+ All Categories
Home > Documents > THRUST MEASUREMENT SYSTEM - ISRO

THRUST MEASUREMENT SYSTEM - ISRO

Date post: 25-Mar-2022
Category:
Upload: others
View: 4 times
Download: 0 times
Share this document with a friend
46
Page 1 of 21 Annexure-1 THRUST MEASUREMENT SYSTEM A new test facility is being established at ISRO Propulsion Complex, Mahendragiri, Tirunelveli, Tamil Nadu for static testing of high thrust rocket engines. To physically measure the thrust developed by rocket engine during static testing, a Thrust Measurement System (TMS) is planned in the facility. This tender is meant for Supply and Site installation of Thrust Measurement System as per technical specification and conditions detailed hereunder. 1. Scope of Work The scope of Bidder in brief includes: 1.1. Procurement of raw material and bought out items. 1.2. Precision fabrication of parts as per tolerances, machining & stress relieving requirements given in drawings. 1.3. Trial assembly of TMS structure and qualification load testing at Manufacturer’s shop. 1.4. Painting, Packing, Transportation of TMS parts to site and safe unloading of items at site. 1.5. Site installation of TMS. 1.6. Final acceptance load testing at site. 1.7. Stage wise inspection of TMS parts from raw material procurement to final load testing at site along with reputed Third Party Inspection agency (to be engaged by Bidder). 2. System Description Thrust Measurement System is an assembly of structural elements and load cells specifically designed to transfer thrust load from rocket engine to the ground structure called Engine Bay Loading Frame and thereby accurately measure the thrust load generated by Engine. Loading Frame is the main load carrying steel structure realized by Department at site. It is a 16m tall steel structure with four inclined columns supporting top deck structure of size 10mx10m with circular opening of Ø3.5m in the center. Loading Frame Structure weighs about 350 ton made up of BIS 2062 E250 Grade B Plates. It is supported by a massive concrete foundation which houses the open J type flame deflector pit of depth 30 m from ground level. Three tensile type load cells each of capacity 100 ton is used in TMS for measuring the engine thrust. These load cells will be given as Free Issue Material by Department at site at the time of site installation.
Transcript

Page 1 of 21

Annexure-1

THRUST MEASUREMENT SYSTEM

A new test facility is being established at ISRO Propulsion Complex, Mahendragiri,

Tirunelveli, Tamil Nadu for static testing of high thrust rocket engines. To physically measure

the thrust developed by rocket engine during static testing, a Thrust Measurement System

(TMS) is planned in the facility. This tender is meant for Supply and Site installation of Thrust

Measurement System as per technical specification and conditions detailed hereunder.

1. Scope of Work

The scope of Bidder in brief includes:

1.1. Procurement of raw material and bought out items.

1.2. Precision fabrication of parts as per tolerances, machining & stress relieving requirements

given in drawings.

1.3. Trial assembly of TMS structure and qualification load testing at Manufacturer’s shop.

1.4. Painting, Packing, Transportation of TMS parts to site and safe unloading of items at site.

1.5. Site installation of TMS.

1.6. Final acceptance load testing at site.

1.7. Stage wise inspection of TMS parts from raw material procurement to final load testing at site

along with reputed Third Party Inspection agency (to be engaged by Bidder).

2. System Description

Thrust Measurement System is an assembly of structural elements and load cells specifically

designed to transfer thrust load from rocket engine to the ground structure called Engine Bay

Loading Frame and thereby accurately measure the thrust load generated by Engine.

Loading Frame is the main load carrying steel structure realized by Department at site. It is a

16m tall steel structure with four inclined columns supporting top deck structure of size

10mx10m with circular opening of Ø3.5m in the center. Loading Frame Structure weighs about

350 ton made up of BIS 2062 E250 Grade B Plates. It is supported by a massive concrete

foundation which houses the open J type flame deflector pit of depth 30 m from ground level.

Three tensile type load cells each of capacity 100 ton is used in TMS for measuring the engine

thrust. These load cells will be given as Free Issue Material by Department at site at the time of

site installation.

Page 2 of 21

Bidder shall have a complete understanding of items indented, its functional & manufacturing

requirements specified in drawings for ensuring satisfactory realization and installation of TMS

at site. The major subsystems in Thrust Measurement System are as follows:

Sl.

No.

Subsystem/

Component

Description

1. Fixed Frame

and interface

plate

Fixed Frame interfaces between Loading Frame and Thrust Frame. The top ring

of the Fixed Frame is connected through bolts with the Loading Frame. The

bottom ring of Fixed Frame is connected to the Thrust Frame through

Measurement Link Assembly. This structure transfers the total thrust load to

Loading Frame.

An Interface Plate is provided between the Loading Frame and top ring of Fixed

Frame. It is provided with tapped holes to attach Fixed Frame. Interface plate

has to be welded with the Loading Frame at site.

2. Thrust Frame Thrust Frame interfaces between Spacer Frame and Fixed Frame. The top ring

of Thrust Frame is interfaced to the bottom ring of Fixed Frame through

Measurement Link Assembly. The bottom ring of Thrust Frame is connected to

Spacer Frame. This is a floating member that transfers load generated by Engine

to the Fixed Frame through Measurement Link Assembly which measures the

thrust force developed by Engine.

3. Spacer Frame Spacer Frame interfaces Engine with Thrust Frame. It is attached to the bottom

ring of Thrust Frame by bolting arrangement.

4. Measurement

Links

Measurement Link interfaces between the Fixed Frame and Thrust Frame. It

connects the top ring of Thrust Frame with bottom ring of Fixed Frame. It

consists of Load Cells and adaptors. It measures the thrust load developed by

Engine.

5. Calibration

Frame and

interface plate

Calibration Frame interfaces between the Loading Frame and 1000T Hydraulic

Jack. The top ring of Calibration Frame is connected to Hydraulic Jack while its

bottom ring is connected to Engine Loading Frame. The purpose of this frame is

to transfer the load generated by hydraulic jack to Engine Loading Frame

during insitu calibration of TMS.

An Interface Plate is provided between the Engine Bay Loading Frame and

Calibration Frame. It is provided with tapped holes to attach Calibration Frame.

Interface plate has to be welded with the Engine Bay Loading Frame at site.

Page 3 of 21

6. Calibration

Link

Calibration Link interfaces between 1000T Hydraulic Jack and Calibration

Plate. It consists of Load Cells and adaptors. It measures the load generated by

the Hydraulic Jack during in-situ Calibration and transfers this load to the

Calibration Plate

7. Calibration

Plate

Calibration Plate interfaces between Calibration Link and Spacer Frame. It

transfers the load from Calibration Link to Spacer Frame during in-situ

calibration of TMS.

8. Preload Frame Preload setup is used during testing process. The preload frame is attached to

the Engine Bay Loading Frame and it supports dead weight with a Pulley Block

assembly. It is meant for keeping load cells always in tension. The Preload

frame is bolted to the Calibration Interface Plate.

9. Pulley block The pulley Block assembly is used to suspend the preload weight and transfer

the load of dead weight suspended to Load Cells.

10. Preload plates The preload Plates of mass 16 tonnes are used to ensure that Load Cells are

always in tension mode for better accuracy in measurement.

11. Side load links The side Load Links are used to ensure that forces and moments in lateral

directions are transferred from Thrust Frame to Fixed Frame. These are

interfaced with Fixed Frame through Bearings and Side Frames.

12. Side Frame Side Frames interface between Side Load Links and the Fixed Frames.

13. Load Test

Fixture

This fixture will be used to carry out load test of the TMS at shop in assembled

condition using the 1000T Hydraulic Jack. During load test, top ring of the

frame interfaces with Calibration Frame while the bottom ring will interface

with Fixed Frame.

14. Stage Bay

Interface Plate

This interface plate is a separate structure similar to interface plate of TMS.

Stage Bay interface plate has to be fabricated and installed at the Stage Bay

Loading Frame.

3. Applicable codes and specifications

3.1. The items realized shall strictly comply with specifications, dimensions, tolerances given in

fabrication drawings of TMS issued by Department. Raw material requirements, fabrication &

inspection procedures and general tolerances shall be as per following standards / codes. All

Page 4 of 21

standards, specifications and codes of practices referred to herein shall be the latest editions

including all applicable official amendments and revisions.

BIS : 814 Covered Electrodes for Manual Metal Arc Welding of Carbon and Carbon

Manganese Steel

BIS: 1363 Hexagon Head Bolts, Screws and Nuts of product (Parts 1 to 3) Grade C

(Size range M5 to M64)

BIS: 1367 Technical Supply Conditions for Threaded Fasteners (All Parts)

BIS: 1852 Specification for rolling & cutting tolerance for hot rolled steel

products.

BIS: 2102 Part I - Tolerances for linear and angular dimensions without

individual tolerance indications.

Part II - Geometrical tolerances for features without individual

tolerance indications.

BIS: 2062 Steel for General Structural Purposes

BIS: 2004 Forgings for General Structural Purposes

BIS: 4367 EN 24 or equivalent 40Ni6Cr4Mo3

BIS: 9595 Recommendations for metal arc welding of carbon & carbon

manganese steel.

ASTM A106/A106M Standard Specification for Seamless Carbon Steel Pipe for High-

Temperature Service

BIS : 800 Code of Practice for General Construction in Steel

BIS : 816 Code of Practice for use of Metal Arc Welding for General construction in

Mild Steel

BIS : 822 Code of Procedure for Inspection of Welds

BIS : 3658 Code of Practice for Liquid Penetrant Flaw Detection

BIS : 7215 Tolerances for Fabrication of Steel Structures

A 388/A 388M Standard Practice for Ultrasonic Examination of Steel Forgings

Page 5 of 21

ASME BPVC Section V

Article 2

Radiographic Examination

ASME BPVC Section V

Article 4

Ultrasonic Examination

ASME BPVC Section VIII

Div.1

Post Weld Heat Treatment

4. Items

The following lists covers major items to be realized by Bidder. Detailed list shall be as per TMS

drawings listed below and Annexures.

• IPRC-SIET-TMS-01/A1-2 Sheets

• IPRC-SIET-TMS-02/A1-1 Sheet

• IPRC-SIET-TMS-03/A1-1 Sheet

• IPRC-SIET-TMS-04/A1-1 Sheet

• IPRC-SIET-TMS-05/A1-1 Sheet

• IPRC-SIET-TMS-06/A1-1 Sheet

• IPRC-SIET-TMS-07/A1-1 Sheet

• IPRC-SIET-TMS-08/A1-1 Sheet

• IPRC-SIET-TMS-09/A1-1 Sheet

• IPRC-SIET-TMS-10/A1-1 Sheet

• IPRC-SIET-TMS-11/A1-1 Sheet

• Annexure-A : List of Fasteners

• Annexure-B : List of bought out items

S.NO DESCRIPTION MATERIAL QTY W.T (Kg)

1. SPACER FRAME IS : 2062

E250 1 1550

2. FIXED FRAME

IS 2062:E250,

IS 2004:20C8,

ASTM A106 GR.B

1 8315

3. THRUST FRAME

IS 2062:E250,

IS 2004:20C8,

ASTM A106 GR.B

1 7050

Page 6 of 21

4. AXIAL LINK ASSEMBLY EN 24

CONDITION-T 3 886

5. ATMS INTERFACE PLATE E250

IS : 2062 1 3495

6. SIDE FRAME-1 IS : 2062

E450 2 360

7. SIDE FRAME-2 IS : 2062

E450 1 150

8. PITCH FORCE/YAW FORCE LINK EN 24

CONDITION-T 2 20

9. ROLL LINK ASSEMBLY EN 24

CONDITION-T 1 18

10. ATTACHMENT BLOCK EN 24 1 10

11. ATTACHMENT BLOCK TWIN EYE EN 24 1 36

12. LATERAL SAFETY STOPPER IS : 2062

E250 3 162

13. SIDE FORCE CALIBRATION LINK

ASSEMBLY

IS : 2062

E450 1 305

14. ALIGNMENT JACKS EN 24 8 40

15. PLATE FOR PRE LOAD SUSPENSION IS : 2062

E250 1 895

16. CALIBRATION INTERFACE PLATE IS : 2062

E250 1 2800

17. PRE LOAD FRAME IS : 2062

E250 1 7620

18. PRE LOAD SUSPENSION ASSEMBLY IS : 2062

E250 4 16800

19. PULLEY BRACKET ASSEMBLY IS : 2062

E250 4 740

Page 7 of 21

20. CALIBRATION FRAME IS : 2062

E250 1 7175

21. 1000T HYDRAULIC JACK …….. 1 ……..

22. HYDRAULIC JACK ADAPTOR EN24 1 510

23. SPHERICAL BEARING &

BEARING HOUSING EN24 1 110

24. IN-SITU CALIBRATION LINK EN24 1 290

25. DUMMY LOAD CELLS EN 24

CONDITION-T 1 250

26. IN-SITU TIE ROD IS : 2062

E250 1 1280

27. WORKING PLATFORM IS : 2062

E250 1 830

28. CALIBRATION PLATE IS : 2062

E250/EN24 1 2865

29. SS 304L Cover IS : 2062

E250 1 1000

30. FASTENERS As per Annexure A LOT LOT

31. BOUGHTOUT ITEMS As per Annexure B LOT LOT

32. COMPONENTS FOR LOAD TESTING IS : 2062

E250 1 15550

33. STAGE BAY INTERFACE PLATE IS : 2062

E250 1 5500

5. Materials

All the materials shall comply with the specifications given in drawings. All materials used

shall be new, unused and free from any defect.

6. Fabrication

6.1. All workmanship and finish shall be of best quality and shall conform to the best method of

fabrication. All materials shall be finished straight and shall be machined/ground smooth true

Page 8 of 21

and square where so specified. All holes and edges shall be free of burrs. Shearing and chipping

shall be neatly and accurately done and all portions of work exposed to view shall be neatly

finished. Material at the shops shall be kept clean and protected from weather.

6.2. All materials shall be straight and, if necessary, before being worked shall be straightened

and/or flattened by pressure and shall be free from twists. Heating or forging shall not be

resorted to without the prior approval of the Department.

6.3. Welding procedure shall be submitted to Department for approval. Welding shall be entrusted

to only qualified and experienced welders who shall be periodically tested and graded as per

BIS 817, BIS: 7310 (Part 1) and BIS: 7318(Part 1). Welder Qualification Reports shall be

submitted to Department for approval. Approval of the welding procedure by the Department

shall not relieve the Bidder of his responsibility for correct and sound welding without undue

distortion in the finished structure.

6.4. Welding electrodes shall be kept in electric oven during welding process. Base metal shall be

preheated to the temperature as per relevant BIS codes.

6.5. Welding process shall be Shielded Metal Arc Welding or Flux Cored Arc Welding. Electrodes

shall be E7018 for IS2062 Materials. In case of welding in EN 24 material, suitable weld

electrodes are to be used. Special electrodes to be used for welding dissimilar materials after

obtaining approval from Department and the details of the same shall be incorporated in

Quality Assurance Plan (QAP).

6.6. The correction of defective welds shall be carried out as directed by the Department without

damaging the parent metal. When a crack in the weld is removed, magnetic particle inspection

or any other equally positive means as prescribed by the Department shall be used to ensure

that the whole of the crack and material up to 25 mm beyond each end of the crack has been

removed. Cost of all such tests and operations incidental to correction shall be to the Bidder's

account.

7. Stress Relieving:

7.1. Stress Relieving is to be done for the parts wherever heavy machining or heavy welding is

involved as indicated in Table-A. The Thrust Frame and Fixed Frame have to be stress relieved

individually as a whole part in a single heat treatment process. IPRC team will witness the

Stress Relieving process.

7.2. Heat Treatment shall be done using electric heater coils with complete thermal insulation in

place. Adequate number of temperature measurements shall be provided to monitor uniform

heating of structure throughout the process.

Page 9 of 21

7.3. The procedure for heat treatment, schematic drawing of heating arrangement, location of

temperature measurements planned, thermal insulation covering, etc. shall be submitted in

advance to IPRC for review and clearance. Before attempting heat treatment, a coupon level

test has to be carried out and process has to be verified.

8. Machining:

8.1. Bidder shall carryout the machining work as specified in the drawings. In general, all the

machining on welded structures shall be carried out after heat treatment / stress relieving and

the dimensions & tolerance specified are to be achieved. All drilled & tapped holes shall be

properly deburred.

8.2. Bidder shall follow proper sequence for welding, drilling & machining in order to achieve

specified dimensions and tolerances mentioned in the drawings. Under no circumstances the

Bidder should resort to welding of parts/improper methods to achieve final

dimensions/tolerances mentioned in assembly drawings.

8.3. Availability of machining allowance shall be checked and confirmed by the manufacturer at

the tack weld stage itself. Manufacturer’s selection of thickness for a member, and depth of

weld shall take the machining allowance into account.

9. Assembly and Load Testing at Shop

Upon completion of fabrication and procurement of bought out items, all the inspection

reports and manufacturer’s test certificates shall be subjected to review of TPI. After TPI’s

clearance, inspection reports shall be submitted to Department. Upon clearance by

Department, trial assembly of TMS shall be made as per drawing IPRC-SIET-TMS-11/A1 with

dummy load cells. Department’s representatives will witness load testing.

All items for assembly shall bear identification mark on non-working surface. All the bought

out items shall be assembled as per supplier’s instructions. Each sub-assembly shall be inspected

and cleared before final assembly of the equipment and the result shall be recorded. Torque

wrenches shall be used for tightening of bolts as per applicable Torque Chart.

Load shall be applied gradually using Hydraulic Jack (to be supplied by Bidder) and the

structure shall be loaded to an extent of maximum 400T. The load shall be retained for

minimum 10 minutes. Deflection in Fixed Frame and Thrust Frame structure under load shall

be measured using dial gauge. Department will bring strain gauges and take measurement

during Load Test. Afterwards, load shall be gradually released. Test Shall be conducted with all

safety measures in place. In case of any abnormal deformation in any of the part during the

loading process, the test shall be aborted. If the abnormal deflection is due to bad workmanship

or use of defective material, Bidder shall be responsible for correcting the same.

Page 10 of 21

After completion of test, TMS assembly shall be dismantled and dimensions of all the

components shall be once again verified. Necessary match marking shall be carried out before

dismantling. Post Load Test inspection reports shall be submitted to Department for review.

Upon clearance by Department, painting works shall be carried out on the structure.

It may be necessary to dismantle sub-assembly or fully assembled item for packing and onward

forwarding to site. In such cases it shall be ensured that minimum numbers of parts are

dismantled and these parts bear match / identification marks to repeat same assembly during

erection.

10. Inspection

10.1. Detailed Quality Assurance Plan (QAP) is to be prepared by Bidder upon award of order clearly

identifying component wise stages of inspection and inspection roles of Bidder, Third Party

Inspector & Department. The QAP shall be submitted to the Department for review and

approval. Approved QAP shall be followed during the course of realization.

10.2. Bidder shall be responsible for inspection and quality control of TMS and related

documentation. In addition, Bidder shall employ a reputed Third Party Inspection (TPI) agency

throughout the work at shop and site. Bidder shall co-ordinate with TPI agency and carryout

inspection. TPI agencies such as Lloyds Register or Bureau Veritas or Det-Norske Veritas or

Technischer Uberwachungs Verein shall only be involved.

10.3. The stage inspections in shop shall include but not limited to the following:

Sl.No. Activity TPI’s role shall include

a. Raw material inspection Taking Sample * and Reviewing

test reports

b. Fit-up inspection Witnessing 100%

c. Root run inspection Witnessing 100%

d. Final welding inspection Witnessing 100%

e. Stress Relieving Witnessing 100%

f. Dimensional inspection Witnessing 100%

g. WPS, PQR and Welders certification as required Witnessing 100%

Page 11 of 21

h. Final dimensional inspection Witnessing 100%

i. Geometrical tolerances checking before unloading from

machine

Witnessing 100%

j. Control assembly and alignment Witnessing 100%

k. Testing to ensure functional requirement Witnessing 100%

l. Grit / Sand blasting and painting Witnessing 100%

* Apart from Manufacturer’s Test Certificate, sample is to be taken from the material to be used

for fabrication at shop in the presence of TPI for every heat number. Samples are to be tested in

a NABL approved laboratory. After ensuring material properties in compliance with standards,

clearance shall be given for shop fabrication. In addition to Physical and Chemical analysis, the

IS 2062 material shall be subjected to impact testing at -20°C.

10.4. The Bidder shall give due notice to the Department in advance of the works getting ready for

inspection.

10.5. No materials shall be painted or dispatched to site without inspection and approval by the

Department unless such inspection is waived in writing.

10.6. The Bidder shall provide all the testing, inspection tools, services and facilities for inspection

by TPI & Department. All the measuring instruments used for inspection and testing shall be

calibrated and appropriate accuracy class of measuring instruments shall be used. Valid

calibration certificate of all measuring instruments, used during inspection and testing shall be

available.

10.7. Ultrasonic Testing shall be done for all forgings before machining.

10.8. Welding Inspection

10.8.1. The Procedure for testing welded joints shall be as per relevant Indian Codes and standards or

other equivalents. All non-destructive tests shall be carried out by qualified operators. All

defects shown shall be repaired and rechecked.

10.8.2. All weld joints and its classification shall be distinctly identified through a numbering system.

Joint numbers shall be engraved on structural members and incorporated in all inspection

reports. The traceability of welds to the radiographs and weld inspection reports shall be

ensured.

Page 12 of 21

10.9. Extent of Testing: In general weld inspection shall be as follows:

• 100% visual inspection for all welds.

• 100% Liquid dye-penetrant inspection test for all joints except gusset & stiffener plate joints.

• 100% Radiography of all butt welds. Wherever radiography is not technically feasible,

Ultrasonic testing shall be carried out with prior approval from Department.

10.10. Visual Inspection

The component shall be checked for conformity with the detailed drawings, dimensional

accuracy, surface finish, fitment & alignment and other related documents/specifications/codes.

Particular attention shall be given to material, fitment & installation, workmanship, cleanliness

and completeness. Following indications are unacceptable:

• Cracks on external surface.

• Undercut on surface, which is more than 1 mm deep.

• Lack of fusion on surface of weldments.

Important note: None of components shall be painted prior to visual/dimension inspection. The

Bidder should protect all components from corrosion by applying oil/grease suitably.

10.11. Bidder shall offer all the welded structure / components for TPI’s inspection at following

stages, before proceeding to next stage. The checks to be carried out at various stages of the

weldments are given below.

10.11.1. Tack weld stage

• Overall sizes of assembly.

• Edge preparation and quality of surface.

• Fitting, alignment and members thickness.

• Measures taken for distortion prevention.

• Groove dimension and root gap.

10.11.2. Welding Completion Stage

• After welding partly/completely, check the size of the weld, quality of weld and finish.

• After welding, assembly shall be checked for dimensional accuracy, bend and local strain

and geometrical distortion.

10.11.3. After Stress Relieving

Page 13 of 21

• Dimensional inspection

• Freeness from heat treatment cracks.

• T-T Curve Chart of Heat Treatment.

10.12. Machining Inspection

All the components shall be machined as per the surface finish indicated in the drawings. Any

deviation on machined component from the drawing shall be brought to the notice of IPRC

immediately. Bidder shall not take any unilateral decision on his own in order to salvage the

item. Dimensional record to be maintained and sketches to be added as required.

After complete inspection of a component, a summary sheet shall be prepared and maintained.

All the necessary tools and instruments shall be arranged by the Bidder.

10.13. Painting and Inspection

10.13.1. TMS shall be painted as per the following scheme.

• Thrust Frame Assembly, Spacer Frame, Preload plates – Golden Yellow

• Fixed Frame Assembly, Preload Frame, Calibration Frame Assembly, Pulley blocks,

Interface frame, Side Frame Assembly-1 (2 nos.), and Side Frame Assembly-2, Calibration

side frame– Phirozi Blue

• All Tie rods, Attachment Blocks, Flexure Seating Plates, Cover plates, Safety Fixtures, Other

Load Test Fixtures - Black

10.13.2. Painting requirements shall be as follows

• Inorganic zinc silicate, DFT-100 microns (min) at shop floor

• Polyurethane, DFT – 100 microns (min) at shop floor

10.13.3. The following brands shall be used.

• GP Bond 141 of Grand Polycoats (Aliphatic polyurethane)

• 2. Bergerthane enamel of Berger (Acrylic polyurethane)

• Apcothane CF674 of Asian paint (Acrylic- Aliphatic polyurethane)

• Pentathane finish paint 4513 of Bombay Paints (Aliphatic isocyanate polyurethane)

10.13.4. Machined interfaces shall not be painted. However, protective coating (IS 158/ Rustex- 3C/

Black Japan) shall be applied immediately after machining to prevent corrosion.

Page 14 of 21

10.13.5. The inspection reports consisting of the following stages shall be submitted to IPRC. No

materials shall be painted without inspection and approval by the Department unless such

inspection is waived.

• Determination of surface preparation.

• Dry film thickness after completion of primer application

• Dry film thickness after completion of final coat of paint

Necessary inspection equipment like paint thickness measuring gauges and other tools required

shall be provided by the Bidder.

11. Inspection Documents

For items being manufactured as per approved QAP, following test certificates and documents,

as applicable for each of the item shall be submitted. All the reports shall be signed with date

clearly indicating role of inspection viz. witness/review/random witness, etc. performed by

each agency

• Physical and chemical test certificates for all materials used in manufacturing of the

equipment.

• Raw material non-destructive test reports.

• Details of stage wise inspection and rectification records for fabricated items, castings,

forgings and machined components.

• Dimension charts with records of alignment, squareness, etc.

• Test certificates for all bought-out items.

• Details of heat treatment and stress relieving charts.

• Non-destructive test reports.

• Static/dynamic balancing certificate for rotating components/machines, as applicable.

• Hardness test report before and after stress relieving.

• Surface preparation and painting inspection reports.

• Catalogues of bought-out items.

12. Site installation

12.1. Bidder shall mobilize required skilled man power, mobile crane, material handling equipment,

welding equipment, electrodes, tools, inspection equipment, Total Work Station, Personnel

Page 15 of 21

Protective Equipment, etc. for installation of TMS at site. Total Work Station shall be used to

measure level variation.

12.2. Upon delivery of required materials at site, Bidder shall commence site installation works. The

interface plates shall be welded to Engine Bay Loading Frame structure after leveling it with

the mating surface to the extent of ±1mm. In case of any mismatch, local grinding shall be done

to mate the surfaces. Welding shall be done by qualified welders in a controlled way. Upon

welding inspection and ensuring of weld quality, installation of TMS shall commence.

12.3. Assembly of TMS shall be made as per drawing IPRC-SIET-TMS-01/A1 (In-situ calibration

setup). All the bought out items shall be assembled as per supplier’s instructions. Each sub-

assembly shall be inspected and cleared before final assembly of the equipment and the result

shall be recorded. Torque wrenches shall be used for tightening of bolts as per standard Torque

Chart. Department will issue actual Load Cells of TMS to Bidder as Free Issue Material for

installation at site. Bidder shall assemble the same with TMS.

12.4. Upon assembly of TMS unit with Loading Frame Structure and clearance by Department,

Bidder shall carryout load testing at site. Load shall be applied gradually using Hydraulic Jack

and the structure shall be loaded to an extent of maximum 220T. The load shall be retained for

minimum 10 minutes. Afterwards, load shall be gradually released. Test shall be conducted

with all safety measures in place.

12.5. After successful load testing, the in-situ calibration setup shall be dismantled and preload set up

shall be assembled.

12.6. Removable type cover made of 5mm thick Stainless Steel 304L plate shall be provided by

Bidder to cover the complete Fixed Frame Structure of TMS after completion of all inspection

works after load testing.

12.7. The Stage Bay Interface Plate shall be welded to Stage Bay Loading Frame structure after

leveling it with the mating surface to the extent of ±1mm. Welding shall be done by qualified

welders in a controlled way. Upon welding inspection and ensuring of weld quality.

12.8. At site, the test stand structure is equipped with an EOT crane of capacity 10t and working

level platforms are available at 11.5m level & 16 m level. Bidder shall arrange any further

temporary structure required for installing / inspecting TMS at site.

12.9. All the site works shall also be monitored and inspected by TPI agency.

13. General Instructions to Bidder

13.1. Bidder shall quote for entire scope of work as per the specific invitation to tender. If any part of

scope is excluded from his offer, the quotation of the Bidder will be liable to get rejected.

Page 16 of 21

13.2. Upon award of Purchase Order, Bidder shall prepare Manufacturing methodology, Execution

schedule & Quality Assurance Plan and submit to Department for review & approval.

Approved procedure shall be followed during the course of realization.

13.3. Manufacturing methodology shall bring out details such as vendor identification for raw

material/bought out items, forging / cutting plan, sequence of fabrication, out sourcing of

works, etc.

13.4. Bidder shall consider in his offer only new structural sections / raw materials for equipment,

fasteners & Bought Out Items. Inspection & testing of Equipment / Bought Out Items shall be

carried out by Bidder/TPI/Department at Bidders/sub-supplier works on the basis of ‘Approved’

drawings & Quality Assurance Plan.

13.5. Bidder shall procure all Bought Out Items only from the suppliers approved by Department.

List of approved make is attached. In case, Bidder propose to procure item from any other

vendor, credentials shall be submitted to the satisfaction of Department. Bidder shall take prior

approval from Department before commencing with procurement process for such case. In case

Bidders proposal is not acceptable, Department’s decision shall be final.

13.6. Bidder shall not off-load the work or part thereof to any sub-contractor without written

permission of Department. In case, sub-letting of any part of the work is permitted by

Department, the fact that such permission has been accorded, neither shall establish any

contractual relationship between Sub-contractor and Department nor shall release the Bidder

from any of his obligations and liabilities under the specific and applicable contract.

Credentials of sub-Contractor and Documentary evidences proving his capability shall be

submitted to the satisfaction of Department. In case, Bidders proposal is not acceptable,

Department’s decision shall be final.

13.7. Approval by Department for various procedures/documents submitted by the Bidder shall not

relieve the Bidder of his responsibilities towards completion of work as defined in the Purchase

Order.

13.8. Bidder shall maintain records of all inspection and testing which shall be made available to the

Department whenever requested for.

13.9. Bidder shall be solely responsible for obtaining necessary clearances, if any, from various

statutory bodies including those of Central & State Government, as applicable, during the

course of manufacture/fabrication, testing, transportation & installation of TMS parts at site.

13.10. After completion of all the works at shop, all the inspection reports shall be consolidated and

submitted to Department for review and dispatch clearance. After obtaining Dispatch

Clearance from Department, the parts of TMS shall be properly packed for arranged for

Page 17 of 21

transportation. Suitable support fixtures are to be used while loading the items in the

transportation trailer to avoid any damage to the system during transportation.

13.11. Bidder shall furnish the supplier’s Installation, Operation and Maintenance Manual for all the

Bought Out Items.

13.12. Location of site:

Mahendragiri is situated in Tirunelveli district, Tamil Nadu state, India. The nearest major

towns are Nagercoil, which is 25 km southward and Valliyur, which is 15 km northward.

IPRC, Mahendragiri is aside of Kanyakumari-Madurai National Highway (NH7) at a distance of

25 km Northward from Kanyakumari. The nearest major railway station is at Nagercoil. The

nearest international airport is at Thiruvananthapuram (Trivandrum, in Kerala state), which is

90 km away in South-West direction.

The installation site in Mahendragiri is about ≈7 km from gate and it is connected with an

approach road of 5.5m wide. The climatic condition at Mahendragiri is tropical and windy with

gusts.

14. Instructions for Unloading, Safe Storage of items and Site installation

14.1. Bidder shall mobilize all the required items and manpower to site with proper permission from

Department and shall maintain proper records.

14.2. Bidder shall make own arrangement for receiving items at site including Crane, slings,

shackles, tools, etc. for unloading items at site. Department will provide open yard for storing

the items. Bidder shall be responsible for safe storage and custody of items.

14.3. At site other erection works are also progressing. Bidder has to work in parallel with necessary

safety measures and complete the work.

14.4. Normal working time is between 09:00 Hours to 17:00 Hours on working days. If Bidder has to

work beyond normal working hours or on holidays for completing the work on schedule, prior

permission from Department needs to be obtained by Bidder. The Bidder’s personnel shall not

be permitted to reside inside the Department’s premises after the work.

14.5. Bidder shall make their own arrangement for transportation, accommodation, food, health

care, communication, etc. for their personnel.

14.6. Bidder shall make his own arrangement to safeguard his items. Department will not be

responsible for damage or loss of any items of Bidder.

14.7. Department will issue Load Cells to Bidder as Free Issue Material for installation at site. Bidder

shall be responsible for the safe custody of Load Cells till final acceptance of TMS by

Department.

Page 18 of 21

14.8. Bidder shall be responsible for the safety of persons deployed to site and shall insure all persons

working at site. Department will not be responsible for any type of accident caused to the

Bidder’s personnel.

14.9. During the execution of the work, if Bidder cause any damage to Department property in any

form, necessary charges for repair / replacement of the same will be recovered from Bidder by

Department.

14.10. Bidder shall abide the statutory rules, laws, acts like minimum wages, Labor license,

insurance/ESI, GST, Income Tax, etc. applicable as per Government of India/Government of

Tamil Nadu in force during work execution.

15. Guarantee

Bidder shall submit a Guarantee Certificate for the items supplied for a period of 12 months

from the date of final acceptance of system at our site against fabrication, manufacturing and

workmanship defects. In case any defect develops in the work due to bad material and / or bad

workmanship before the expiry of guarantee period, the Bidder, on notification by

Department, shall rectify or remedy the defect at their own cost and shall make their own

arrangements to provide materials, labour, equipment and any other appliances required in this

regard.

16. Execution Schedule

All the items shall be supplied and installed at site within 7 months from the date of purchase

order. Upon placement of order, Bidder shall submit a detail schedule of all activities involved

to complete the whole work within the delivery period in the form of Gantt chart. The agreed

Gantt chart shall be the basis for progress monitoring and corrective measures during the

execution period. The successful Bidder shall furnish monthly progress reports.

17. Security Deposit

The Bidder shall submit Security Deposit in the form of an unconditional bank guarantee from

any nationalized/scheduled bank approved by RBI for 10% of the Contract value to the

Department within 30 days upon award of contract. This deposit is meant to compensate, the

department, for any loss due to failure of the supplier to complete his obligations as per the

purchase order. The Security Deposit shall be valid for a period of 60 days beyond the date of

final acceptance of the system.

18. Liquidated Damages

Due to reasons not attributable to Department, if the Bidder fails to complete the work or fails

to meet delivery date within the time specified in the Purchase Order or any extension thereof,

the Department will recover liquidated damages (LD) from the Bidder a sum of 0.5% of the

Page 19 of 21

total order value for each calendar week of delay or part thereof. The total value of liquidated

damages shall not exceed 10% of the order value.

19. Force Majeure

Neither party shall bear responsibility for the complete or partial non-performance of any of

his obligations (except for failure to pay any sum which has become due on account of receipt

of goods under the provisions of the order) if the non-performance results from such force

majeure circumstances such as, but not restricted to, flood, fire, earthquake, civil commotion,

sabotage, explosion, epidemic, quarantine restriction, strike, lock-out, freight embargo, acts of

the Government either in its sovereign or Contractual capacity, hostility, acts of public enemy

and other acts of God as well as war or revolution, military operation, blockade, acts or actions

of State authorities or any other circumstance beyond the control of the parties that have

arisen after the conclusion of the order. In such circumstances, the time stipulated for the

performance of an obligation under the order may be proportionately extended.

The party, for whom it has become impossible to meet the obligation under order due to force

majeure condition, will notify the other party in writing not later than twenty-one days from

the date of commencement of the unforeseeable event. Unless otherwise directed by the

department in writing, the Bidder shall continue to perform his obligations under order as far

as is practical and shall seek all reasonable alternative means for performance not prevented by

the force majeure event.

Any certificate issued by the Chamber of Commerce or any other competent authority or

organization of the respective country shall be sufficient proof of commencement and cessation

of the above circumstances.

In case of failure to carry out complete or partial performance of an obligation for more than

sixty days, either party shall reserve the right to terminate the order totally or partially. A prior

written notice of 30 days to the other party will be given informing of the intention to

terminate without any liability. This is exclusive of any reimbursements for the goods received

as provided for in the agreement.

20. Payment

20.1. Bidder shall understand the complete scope of work and quote firm and fixed lump sum price

for executing entire scope of work as per terms & conditions specified in the tender.

20.2. No extra claim shall be entertained from the Bidder, if the actual weight fabricated differ from

those indicated in drawings.

20.3. In case of any additional quantity or work requested by Department to meet any additional

requirement in connection with functional/safety of Thrust Measurement System, Bidder shall

Page 20 of 21

execute the same without holding the work. After completion of entire scope of work,

Department & Bidder shall discuss and mutually arrive at the price for such additional

quantity/work performed.

20.4. Department shall reimburse all taxes as per the prevailing rates at actuals.

20.5. Department is entitled for concessional GST @ 5% (for material supply) as per Ministry of

Finance, Department of Revenue, Notification No. 45/2017-Central Tax (Rate) and 47/2017-

Integrated Tax (Rate) dated 14.11.2017. Department will issue necessary concessional GST

certificate for claiming Concessional GST in favor of Bidder & Vendor only for items directly

consigned to Department. It is the responsibility of Bidder to obtain concessional certificates

from Department by providing necessary details & documents well in advance.

20.6. Department will issue Custom Duty Exemption Certificate for the imported items covered

under Customs Notification No. 5/2018 dated 25.01.2018 and directly consigned to

Department. It is the responsibility of Bidder to obtain concessional certificates from

Department by providing necessary details & documents well in advance.

20.7. Milestone Payment shall be considered as follows:

20.7.1. Upon placement of order and Acceptance of Manufacturing Methodology & Quality Assurance

Plan by Department: 20% of order value shall be paid against bank guarantee (valid for

complete delivery period) and submission of proforma invoice.

20.7.2. Upon completion of delivery of all the items to site: 60% of order value shall be paid against

proforma invoice and delivery documents.

20.7.3. Upon completion of site installation & load testing: 20% of order value shall be paid against

satisfactory completion of site installation of all the TMS unit and successful load testing of

TMS at site and submission of performance bank guarantee for 10% of order value (valid for 12

months from the date of final acceptance of the system by Department) & proforma invoice.

All bank guarantees shall be unconditional and issued by any nationalized/scheduled bank

approved by RBI.

21. Pre-Qualification criteria

The Bidder’s capability will be evaluated based on the following Pre-Qualification (PQ)

criteria. The Bidders shall suitably submit the information solicited and submit as part of the

Techno-Commercial Bid along with supporting documentary evidences. Those Bidders who

fulfil PQ criteria only will be screened-in for opening and evaluation of Price Bid. Any lack of

information or incomplete information or information non-compliant with the PQ criteria

shall be treated as sufficient cause to summarily reject such Bids.

Page 21 of 21

21.1. Average annual financial turnover of Bidder during the last 3 years, ending 31/03/2018, shall be

at least Rs.135 Lakhs. Audited annual turnover document for the last 3 years shall be

submitted.

21.2. The Bidder must have successfully supplied an Equipment or Structure of size minimum 2.5m

in diameter or 2.5mx2.5m in size with parts of minimum thickness 140 mm involving

machining in the last 7 years period ending 31/12/2018. Bidder shall submit the following

documentary evidences:

21.2.1. Purchase order and corresponding acceptance certificate from client

21.2.2. A technical note on brief description of the item highlighting details such as

• Size of the item

• Thickness of the machined parts

• Machining tolerance

• Drawings / sketches / photographs

21.3. The Bidder must have successfully completed supply of items for the following Purchase order

values during the last 5 years ending 31/12/2018. Bidder shall submit purchase order and

corresponding acceptance certificate from client as documentary evidence.

21.3.1. One work of Purchase Order value equal to or more than Rs. 360 Lakhs

Or

21.3.2. Two works each Purchase Order of value equal to or more than Rs. 225 Lakhs

Or

21.3.3. Three works each Purchase Order of value equal to or more than Rs. 180 Lakhs

22. Bid Details

22.1. Bid shall be submitted in Two Parts viz. Techno-Commercial Offer and Price Offer

22.2. Bidder shall not mention or indicate any element of price whatsoever, as sum or percentage, in

the Techno-commercial bid. Such information is to be given in the Price bid only. Bid will be

summarily rejected, if Bidder mention any information on price in Techno-Commercial bid.

22.3. Offer Validity: Offer shall be valid for a minimum period of six months from tender due date.

22.4. Delivery term: The items shall be transported, unloaded at Department’s site in IPRC,

Mahendragiri, Tirunelveli and installed at site.

Annexure- A

LIST OF FASTENERS & WASHERS

(Make of fasteners : Unbrako/PFL)

Sl. no

Description Minimum Thread Length (mm)

Property class

Washer

Type & Thk.

(mm)

Qty (nos.)

Thread

Engagement

(mm)

Drawing Number

&

Component Details

1 M30 X 130 Long Hex. Head Bolt

65 8.8 PLAIN & 5 Thk. 40 59 mm IPRC-SIET-TMS-02/A1 ( SEATING PLATE- COVER

PLATE INTERFACE)

2 M24 X 80 Long Allen Bolt

50 8.8 - 70 44 mm IPRC-SIET-TMS-02/A1 ( SEATING PLATE- TF/FF

INTERFACE)

3 M20 X 45 Long Hex. Head Bolt

30 8.8 PLAIN & 4 Thk. 40 25 mm IPRC-SIET-TMS-05/A1 ( LATERAL STOPPER TO

FIXED FRAME)

4 M20 X 60 Long Hex. Head Bolt

40 8.8 PLAIN & 4 Thk. 50 36 mm IPRC-SIET-TMS-03/A1 ( ENGINE FRAME TO SPACER FRAME)

5 M12 X 40 Long Hex. Head Bolt

20 8.8 PLAIN & 3 Thk. 40 17 mm IPRC-SIET-TMS-03/A1 ( ENGINE FRAME TO SPACER FRAME)

6 M16 X 70 Long Hex. Head Bolt

30 8.8 PLAIN & 3 Thk. 70 22 mm IPRC-SIET-TMS-03/A1 ( THRUST FRAME TO

SPACER FRAME)

7 M36 X 120 Long Hex. Head Bolt

60 8.8 PLAIN PLATE WASHER WITH O.D.

80 MM & 10 Thk.

80 48 mm IPRC-SIET-TMS-04/A1 (FIXED FRAME TO

INTERFACE PLATE)

8 M36 X 110 Long Hex. Head Bolt

65 8.8 PLAIN PLATE WASHER WITH O.D.

80 MM & 10 Thk.

110 60 mm IPRC-SIET-TMS-04/A1 (FIXED FRAME TO SIDE

FRAMES)

9 M20 X 80 Long Hex. Head Bolt

45 8.8 PLAIN & 4 Thk. 40 36 mm IPRC-SIET-TMS-05/A1 ( CALIBRATION INTERFACE PLATE TO THRUST FRAME)

10 M24 X 90 Long Hex. Head Bolt

60 8.8 PLAIN & 4 Thk. 25 46 mm IPRC-SIET-TMS-07/A1 ( SIDE CALIBRATION FRAME

TO JACK BASE PLATE)

11 M24 X 70 Long Hex. Head Bolt

50 8.8 PLAIN & 4 Thk. 35 32 mm IPRC-SIET-TMS-08/A1 ( PULLY BLOCK TO PRELOAD FRAME)

12 M8 X 20 Long ALLEN Bolt

FULL THREAD

8.8 - 35 14 mm IPRC-SIET-TMS-08/A1 ( PULLY HOUSING

ASSEMBLY)

13 M36 X 100 Long Hex. Head Bolt

40 8.8 PLAIN PLATE WASHER WITH O.D.

80 MM & 6 Thk.

70 34 mm IPRC-SIET-TMS-08/A1 (PRELOAD FRAME TO INTERFACE PLATES)

14 M36 X 100 Long Hex. Head Bolt

40 8.8 PLAIN PLATE WASHER WITH O.D.

80 MM & 10 Thk.

70 34 mm IPRC-SIET-TMS-09/A1 (CALIBRATION FRAME TO

INTERFACE PLATES)

15 M16 X 60 Long Hex. Head Bolt

FULL THREAD

8.8 PLAIN & 5 Thk. 70 5 mm IPRC-SIET-TMS-09/A1 (CALIBRATION FRAME TO

WORKING PLATFORM)

16 M 48 X 180 Long Hex. Head Bolt

100

8.8 PLAIN PLATE WASHER WITH O.D.

80 MM & 10 Thk.

20 70 mm IPRC-SIET-TMS-09/A1 (CALIBRATION FRAME TO

1000 T JACK)

17 M20 X 140 Long Hex. Head Bolt

50 8.8 PLAIN & 5 Thk. 35 35 mm IPRC-SIET-TMS-09/A1 ( CALIBRATION PLATE TO

SPACER FRAME)

18 M24 X 80 Long Hex. Head Bolt

50 8.8 PLAIN & 5 Thk. 20 44 mm IPRC-SIET-TMS-09/A1 ( ENGINE SPACER FRAME)

19 M36 X 180 Long Hex. Head Bolt

60 10.9 SPHERICAL WASHER SET & 10

Thk.

25 50 mm IPRC-SIET-TMS-09/A1 (JACK ADAPRTOR TO BEARING HOUSING)

20 M36 X 160 Long Hex. Head Bolt

60 8.8 PLAIN PLATE WASHER WITH O.D.

80 MM & 8 Thk.

60 49 mm IPRC-SIET-TMS-10/A1 (ATMS ON LOAD TEST

SUPPORT STOOL)

21 M36 X 90 Long Hex. Head Bolt

50 8.8 PLAIN PLATE WASHER WITH O.D.

80 MM & 10 Thk.

30 40 mm IPRC-SIET-TMS-10/A1 (SIDE FORCE SIMULATOR)

22 M24 X 130 Long Hex. Head Bolt

70 8.8 PLAIN & 5 Thk 30 55mm IPRC-SIET-TMS-10/A1 (ATTACHMENT BLOCK

INTERFACE)

Page 1 of 9

Annexure-B

LIST OF BOUGHT-OUT ITEMS

Item No: 1

Maintenance-free Rod ends, Make: INA/SKF/FAG/LUK

(Drawing no: IPRC-SIET-TMS-07/A1)

Size Static

Load

Rating

Max.

swiveling

angle

Thread type Quantity

(including

spare)

Φ50 Pin 313 kN 6⁰ Right Hand Thread 4

Φ50 Pin 313 kN 6⁰ Left Hand Thread 4

Φ60 Pin 485 kN 6⁰ Right Hand Thread 4

Φ60 Pin 485 kN 6⁰ Left Hand Thread 4

Φ80 Pin 689 kN 6⁰ Right Hand Thread 2

*Φ35 Pin 159 kN 6⁰ Right Hand Thread 4

*Φ35 Pin 689 kN 6⁰ Left Hand Thread 4

Total 26

* Indicates spare bearings and not shown in drawings and to be supplied with

M36X3 female threads.

(Note: The thread size and other dimensions shall match with the load link as per the

respective drawings provided)

Item No: 2

Maintenance-free Axial Spherical plain bearings, Make: INA/SKF/FAG/LUK (Drawing

no: IPRC-SIET-TMS-09/A1)

� Capacity : 7100 kN (Static load rating)

� Shaft Diameter : 200 mm

� Overall Height : 87 mm

� Shaft Misalignment : ± 80

� Sliding contact surface : Hard chromium/PTFE fabric.

� Total quantity required : 03

Item No: 3

Double Acting Hydraulic Cylinders of Make: Larzep / Powerteam / Holmatro/ Enerpac/ Europress

(Drawing nos: IPRC-SIET-TMS-09/A1, IPRC-SIET-TMS-07/A1, IPRC-SIET-TMS-05/A1)

Axial calibration link:

� Max. Capacity : 985 t (Pull)

� Stoke length : 150 mm

Page 2 of 9

� Fully closed Height : 735 mm

� Operating pressure : 700 bar (maximum) with safety relief valve

� End fittings for hose : 3/8’’ NPTF and QC/DC as per standard.

� Quantity required : 01

� One spare kit consisting of O-rings & oil seals shall be provided for the jack.

Side force simulation link:

� Capacity : 44 t (pull)

� Stoke length : 330 mm

� Fully closed Height : 517.5 mm

� Operating pressure : 720 bar (Maximum) with built in safety relief valve.

� Thread in Jack Housing : 5 3/4” - 40 mm Long

� Mounting Thread on

Plunger Head

: 2 – 4 1/2”

� End fittings for hose : 3/8’’ NPTF and QC/DC as per standard.

� Total quantity required : 05

� One spare kit consisting of O-rings & oil seals shall be provided for each jack (Total- 3 nos).

Hydraulic hoses:

� Hoses : 10 m length hydraulic hose (700 bar) with QC/DC End

Fittings

� Quantity : 8 nos.

Tilt saddles:

� Make : Power Team

� Part no : 351325

� Quantity : 12 nos.

Pump:

� Make : Power team/ Larzep/ Enerpac/ Holmatro/ Europress

� Description : Manual ( 2 no.) suiting to 44t jack with two way

direction control valve (2 no.) and pressure reducing

valve (4 nos.)

� Type: : Eletrically operated ( 1 no.) suiting to 1000 t jack with

two way direction control valve (1 no.) and pressure

reducing valve (2nos.)

Oil

� Standard hydraulic oil ASTM Grade 215. Quantity : 200 Litres / 1 barrel.

Note:

� The thread size and other dimensions shall match with the load link as per the respective drawings provided

� Suitable handling provision shall be available for all the jacks.

� All the above items are to be procured from authorized distributors only and to be supplied with necessary load test/ warranty certificates.

Page 3 of 9

Item No: 4

Cylindrical bearings for pre-load pulley block, Make: INA/SKF/FAG/LUK (Drawing

no: IPRC-SIET-TMS-08/A1)

� Capacity : 75 kN (Static load rating)

� Shaft Diameter : 30 mm

� Overall Diameter : 72 mm

� Contact surface : Cylindrical rollers.

� Total quantity required : 06 nos.

Item No: 5

12t Capacity two Legged Wire Rope (Conforming to IS 2762: Wire Rope Slings and Sling Legs)

� Wire Rope Make : Usha Martin

� Wire Rope Specification : 6 x 37 steel core (CWR) with grade 1960 (as per IS 2266)

� Wire Rope diameter : 24 mm � Type : Mechanically spliced Two-leg wire rope slings with main ring at one end, ordinary thimbles at other.

� Lifting Capacity : 12 t � Effective Length : 6 m � Ferrule : Conforming to IS 10942 � Master Links (Ring) : Conforming to IS 2760. � Total quantity required : 02 sets.

Item No:6

10t Capacity four Legged Wire Rope (Conforming to IS 2762: Wire Rope Slings and Sling Legs) � Wire Rope Make : Usha Martin � Wire Rope Specification : 6 x 37 steel core (CWR) with grade 1960 (as per IS 2266)

� Wire Rope diameter : 16 mm � Type : Mechanically spliced four-leg wire rope slings with one main ring and two intermediate rings at one end, ordinary thimbles at other.

� Lifting Capacity : 10 t � Effective Length : 6 m � Ferrule : Conforming to IS 10942 � Master Links (Ring) : Conforming to IS 2760. � Total quantity required : 01 set.

Page 4 of 9

Item No: 7

Wire ropes & accessories for pre-load suspension & Turnbuckles:

a Wire rope (16 mm diameter) with ordinary thimbles having effective length of 4280mm long Make: Usha Martin

4 nos.

b Wire rope (16 mm diameter) with ordinary thimbles having effective length of 3100 mm long Make: Usha Martin

4 Nos.

c Turnbuckle – 6.89 t capacity with jaw & jaw type ends having length range 955 mm-1412 mm Make: Crosby, Model No : HG 228, Stock no: 1032894

8 Nos.

d Swivel Head eye bolt with load capacity of 13.75 t (Make : Crosby, Model: HR1000M ,Stock no: 1068389)

6 Nos.

e D-shackles with load capacity of 9.5 t (Make : Crosby Model: G209A Stock no: 1017560)

20 Nos.

f Eye bolt with load capacity of 8.5 t (Make: - Crosby, Model: M279 Stock no: 1046109)

6 Nos.

Item No: 8

SWIVEL EYE BOLTS Sl.no Description Specification Qty

Required

1. Swivel Eye bolt – 1.9 t ( M16 x2)

Make: Crosby Model: HR-1000M Stock no: 1068334

5 Nos.

2. Swivel Eye bolt – 4.2 t ( M24 x3)

Make: Crosby Model: HR-1000M Stock no: 1068361

5 Nos.

3. Swivel Eye bolt – 11 t ( M36 x4)

Make: Crosby Model: HR-1000M Stock no: 1068389

5 Nos.

Item No: 9 Hydraulic Scissor Truck

� Make : VANJAX

� Model No. : VXLT-800/1500 " - 2 nos.

� Capacity : 800 kg

� Min. Height: 445 mm,

� Max. Height: 1500mm,

� Platform size (approx.): 1210 x 610

� Movement: Manual

� Safety feature: Mechanical Lock Wheel

Total quantity required : 02 set

Page 5 of 9

Item No: 10

Total Station

� Make : Sokkia

� Model No. : FX 101

� Total quantity : 01

� Display : Dual Side Colour Display with Touch Screen

� Angle Accuracy : 1”; Angle Resolution: 0.5”

� Reflector less Range : 500m

� Internal Memory : 1 Lac pts

Standard accessories shall include

- Telescopic Tripod

- Circular Prism with Mount and Target

- Telescopic Range Pole with Level

- Mini Prism with 4 Short Poles

Item No: 11 Hydraulic Torque Wrench

� Quantity : 01 set

� Supply shall include Hydraulic Power Unit, Stack sockets, reducers, reaction paddles, extension arms, flexible hoses, quick connect / disconnect couplers and hydraulic oil.

� Make : Torc, USA

� Torque Range : upto 40000 N.m

� Output accuracy : ±3%

� Torque repeatability : 100%

� Material of construction of cylinders and ratchet links : ASTM A 322 4340 Aircraft quality steel

� Sockets : Hexagonal stack sockets and reducers of different sizes to meet nut requirements from 1.5 inch to 3 inch.

� Operation : Electrically operated remote control with 12 feet wire

� Spares shall include hoses, oil for two fillings, etc.

Item No: 12

Tools

SI. NO. DISCRIPTION OF

ITEMS SIZE MAKE/MATERIAL Quantity

1.

DOUBLE END BI-HEXAGONAL

RING SPANNERS,

OFFSET TYPE

i) METRIC SIZE : 6x7, 8x9, 10x11, 12x13, 14x15, 16x17, 18x19, 20x22, 21x23, 24x26, 24x27, 25x28, 27x32, 30x32, 32x36, 36x41, 41x46, 46x50

(1 set= 18 items each 1 no)

Any reputed make Nickel-Chrome plated chrome vanadium steel

3 sets

Page 6 of 9

ii) METRIC SIZE: 34x38, 55x60, 75x80 (1 set= 3 items each 1 no)

3 sets

2. SINGLE END OPEN JAW SPANNER

i) METRIC SIZE : 55mm , 56mm, 58mm, 60mm, 66mm, 70mm, 75mm, 80mm, 120mm, 124mm

(1 set= 10 items each 1 no)

Any reputed make Nickel-Chrome plated chrome vanadium steel

3 sets

ii) METRIC SIZE: 95mm, 105mm (1 set= 2 items each 1 no)

3 sets

3. ADJUSTABLE SPANNERS

Span: 0-13mm length: 100mm Any reputed make

Nickel-Chrome plated chrome vanadium steel

3 Nos.

Span: 0-25 mm Length: 200mm

3 Nos.

Span: 0-36 mm Length: 250mm

3 Nos.

4.

SPANNERS OF ONE END WITH

JAW AND OTHER END WITH RING

i) METRIC SIZE: 10mm, 11mm, 12mm, 13mm, 14mm, 15mm, 16mm, 17mm, 18mm, 19mm, 20mm, 21mm, 22mm, 23mm, 24mm, 25mm, 26mm, 27mm, 28mm, 29mm, 30mm, 32mm, (1 set= 22 items each 1 no)

Any reputed make Nickel-Chrome plated chrome vanadium steel

3 sets

i) METRIC SIZE: 55mm, 60mm, 75mm, 80mm (1 set= 4 items each 1 no)

3 sets

5.

BOX SPANNER WITH

REVERSIBLE RATCHET with ½” square drive and 2 Nos. of ½” F X ¾”

M adapter

METRIC SIZE: 6mm, 7mm, 8mm, 9mm, 10mm, 11mm, 12mm, 13mm, 14mm, 15mm, 16mm, 17mm, 18mm, 19mm, 20mm, 21mm, 22mm, 23mm, 24mm, 25mm, 26mm, 27mm, 28mm, 29mm, 30mm, 31mm, 32mm, 34mm, 36mm,

41mm, 50mm (1 set= 31 items each 1 no)

Any reputed make Manufacturer’s

standard material 3 sets

6.

TORQUE WRENCH WITH ½” square drive

with 2 Nos. of ½” F X ¾” M adapter

RANGE: 14-68 Nm

Any reputed make Manufacturer’s

standard material

3 Nos.

RANGE: 25-135 Nm 3 Nos.

RANGE: 50-220 Nm 3 Nos.

RANGE: 135-540 Nm 3 Nos.

RANGE: 475-1015 Nm 3 Nos.

7.

OPEN ENDS, ROUND

ATTACHEMENT (TO SUIT ABOVE

TORQUE WRENCH)

METRIC SIZE: 10mm, 11mm, 12mm, 13mm, 14mm, 15mm, 16mm, 17mm, 18mm, 19mm, 20mm, 21mm, 22mm, 23mm, 24mm, 25mm, 26mm, 27mm, 28mm, 29mm, 30mm, 31mm, 32mm,

36mm (1 set= 24 items each 1 no)

Any reputed make Drop forged chrome

plated vanadium steel

3 sets

Page 7 of 9

8. HAND HELD ENGRAVING

MACHINE -

Any reputed make Manufacturer’s

standard material 3 Nos.

9.

SLEDGE HAMMER AND

HANDLE

CAPACITY HANDLE LENGTH

Any reputed make Manufacturer’s

standard material

3 Nos. 1 lb 350mm

2 lb 350mm 3 Nos.

3 lb 350mm 3 Nos.

CLAW HAMMER 2 lb 300 mm 3 Nos.

BALL PEEN HAMMERS WITH

WOODEN HANDLE

1 lb 350mm 3 Nos.

2 lb 350mm 3 Nos.

3lb 350mm 3 Nos.

NYLON HAMMER ½ lb 350mm 3 Nos.

10.

LETTER PUNCH: CAPITAL

LETTERS, SET OF 26 ENGLISH

LETTERS

Height of characters: 6mm, 26 letters Any reputed make Heat treated carbon

steel 3 Nos

11. NUMBER PUNCH:

SET OF 10 NUMBERS

Height of characters: 6mm, 10 items Any reputed make Heat treated carbon

steel 3 Nos.

12. CENTER PUNCH Tip dia: 3mm, length: 100mm Any reputed make Chrome Vanadium

Steel 3 Nos.

13. MAGNIFICATION

GLASS Dia: 100mm Any reputed make 5 Nos.

14. DIVIDER 150mm

Any reputed make

3 Nos.

300mm 3 Nos.

15. SPIRIT LEVEL (MAGNETIC

MODEL)

Length: 150mm Any reputed make

Cast aluminium 3 Nos.

Length: 300mm Any reputed make

Cast aluminium 3 Nos.

16. STAR SCREW

DRIVER

Dia: 6mm, Length: 125mm

Any reputed make Blade: Chrome vanadium steel,

Handle: Manufacturer

standard material

5 Nos.

Dia: 8mm, Length: 150mm

Any reputed make Blade: Chrome vanadium steel,

Handle: Manufacturer

standard material

5 Nos.

Dia: 25mm, Length: 265 mm

Any reputed make Blade: Chrome vanadium steel,

Handle: manufacturer

standard material

5 Nos.

17. SCREW DRIVER Dia: 8mm, Length: 250 mm Any reputed make 5 Nos.

Page 8 of 9

Dia: 10mm, Length: 330 mm Blade: Chrome vanadium steel,

Handle: manufacturer

standard material

5 Nos.

Dia:11.5mm, Length: 140mm 5 Nos.

18. HAND HACKSAW

FRAME Suitable for blade length 300mm

Any reputed make Hardened steel

5 Nos.

19. HAND HACKSAW

BLADE Size: 12"X1/2"X24 TPI, Length: 300mm

Any reputed make High strength steel

200 Nos.

20.

VERNIER HEIGHT GAUGE

WITH DIAL GAUGE

Range: 0 to 600mm in increments of 0.02 mm Least count: 0.02

Make : Mitutoyo 5 Nos.

21. DIGITAL VERNIER CALIPER

Range: 0 to 300mm length, accuracy: 0.01 mm

Make : Mitutoyo 5 No.

22. DEPTH GAUGE 0.02 mm, parallax-free vernier scale,

capacity 200mm Make : Mitutoyo 5 No.

23. SCREW PITCH

GAUGE

Metric pitch ranges: 0.35mm to 6.0mm in 22 Leaves:

(0.35mm, 0.4mm, 0.45mm, 0.5mm, 0.55mm, 0.6mm, 0.7mm, 0.75mm,

0.8mm, 1mm, 1.25mm, 1.5mm, 1.75mm, 2mm, 2.5mm, 3mm, 3.5mm, 4mm,

4.5mm, 5mm, 5.5mm, 6mm & 60 Angle gauge )

Any reputed make Tool steel

3 Nos.

24.

TOOLS BOX WITH, FIVE

COMPARTMENTS, LOCK & KEY

(MEDIUM QUALITY)

500mmX400mmX300mm (LXBXH) Any reputed make

steel 6 Nos.

25. ALLEN KEYS

TOOL KIT

A / F DIMENSION (mm): 1, 1.5, 2, 2.5, 3, 4, 5, 6, 8, 10, 12, 14, 17 & 19 (1 set = 14 items each 1 no)

Any reputed make Manufacturer’s

standard material 5 sets

26. STEEL RULE 300mm Any reputed make

Stainless steel

each 5

Nos.

27. MEASURING STEEL TAPE

3m Any reputed make 5 Nos.

5m Any reputed make 5 Nos.

10m Any reputed make 3 Nos.

25m Any reputed make 3 Nos.

28. CHISEL (FLAT AND DIAMOND

POINT) Length: 100mm, section 10mm

Any reputed make Hardened steel

3 Nos.

29.

AUTOMATIC CUT-OUT MANUAL TORQUE WRENCH

SUITABLE FOR OPEN END

HEADS

RANGE: 1-36 Nm

Any reputed make Manufacturer’s

standard material

3 No.

RANGE: 5-60 Nm 3 No.

RANGE: 20-200 Nm 3 No.

RANGE: 50-1000 Nm 3 No.

Page 9 of 9

30.

OPEN ENDS, HEAD

ATTACHEMENT (TO SUIT ABOVE

TORQUE WRENCH)

METRIC SIZE: 6mm, 7mm, 8mm, 9mm, 10mm, 11mm, 12mm, 13mm, 14mm, 15mm, 16mm, 17mm, 18mm, 19mm, 20mm, 21mm, 22mm, 23mm, 24mm, 25mm, 26mm, 27mm, 29mm, 30mm,

32mm, 34mm, 36mm, 38mm (1 set= 28 items each 1 no)

Any reputed make Drop forged chrome

plated vanadium steel

3 sets

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEET DRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

STATUS

TENDER PURPOSE

FABRICATION

DISCUSSION / REVIEW

------------------------------

ONLY FOR REVIEW

------------------------------

10

3

5

4

6

7

8

9

2

13

17

15

16

18

11

19

1 12

14

ASSEMBLY SETUP DURING ENGINE TESTING

IS : 2062E250

------

EN24

------

13

2

1197

10

8

6

5

14

3

16

4

20

21

22

23

24

25

26

128

27

ASSEMBLY SETUP DURING IN-SITU CALIBRATION

TEST STAND FORSEMI CRYO INTEGRATED ENGINE TEST FACILITY

(3-D VIEWS OF SUB-SYSTEMS)

1 : 12 IPRC-SIET-TMS-01/A1 21

TOTAL WEIGHT : 80,750 Kgs. (Approx)

REVISIONS SIGNZONE DATE

1 SPACER FRAME 1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

16

17

18

1550

PRE LOAD SUSPENSION ASSEMBLY

PRE LOAD FRAME

CALIBRATION INTERFACE PLATE

PLATE FOR PRE LOAD SUSPENSION

ALIGNMENT JACKS

SIDE FORCE CALIBRATION LINKASSEMBLY

LATERAL SAFETY STOPPER

ATTACHMENT BLOCK TWIN EYE

ATTACHMENT BLOCK

ROLL LINK ASSEMBLY

PITCH FORCE/YAW FORCE LINK

SIDE FRAME-2

SIDE FRAME-1

ATMS INTERFACE PLATE

AXIAL LINK ASSEMBLY

THRUST FRAME

FIXED FRAME

4

1

1

1

8

1

3

1

1

1

2

1

2

1

3

1

1

16800

7620

2800

895

40

305

162

36

10

18

20

150

360

3495

886

7050

8315

CONDITION-T

IS : 2062

IS : 2062

IS : 2062

IS : 2062

IS : 2062

EN 24

20

19

CALIBRATION FRAME

PULLEY BRACKET ASSEMBLY

IS : 2062

IS : 2062

1

4

7175

740

CONDITION-T

CONDITION-T

EN 24

EN 24

EN 24

EN 24

IS 2062:E250,IS 2004:20C8,ASTM A106 GR.B

IS 2062:E250,IS 2004:20C8,ASTM A106 GR.B

IS : 2062E250

E250IS : 2062

IS : 2062E450

IS : 2062E450

E250

E450IS : 2062

EN 24

E250

E250

E250

E250

E250

E250

29

28

27

26

25

24

23

22

21

LOADING FRAME

CALIBRATION PLATE

WORKING PLATFORM

IN-SITU TIE ROD

300T LOAD CELL

IN-SITU CALIBRATION LINK

SPHERICAL BEARING & BEARING HOUSING

HYDRAULIC JACK ADAPTOR

1000T HYDRAULIC JACK

IS : 2062

IS : 2062

IS : 2062

IS : 2062

EN24

E250

E250/EN24

E250

E250

1

1

1

1

1

1

1

1

1

---

2865

830

1280

---

290

110

510

---

32

31

30

ALL HANDLING SYSTEMS

ALL BOUGHTOUT ITEMS

ALL NUTS,BOLTS & WASHERS

------

------

------

LOT

LOT

LOT

---

---

---

REFER ANNEXURE-2

REFER ANNEXURE-3

33 COMPONENTS FOR LOAD TESTING -- 15550

IPRC-SIET-TMS-03

REFER ANNEXURE-1

NOT SHOWN IN THE DRAWING

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-08

IPRC-SIET-TMS-08

IPRC-SIET-TMS-08

IPRC-SIET-TMS-06

IPRC-SIET-TMS-05

IPRC-SIET-TMS-05

IPRC-SIET-TMS-07

IPRC-SIET-TMS-05

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-06

IPRC-SIET-TMS-02

IPRC-SIET-TMS-05

IPRC-SIET-TMS-04

IPRC-SIET-TMS-10

EN24

GENERAL NOTE:

THE SEQUENCE OF FABRICATION/ERECTION OF THE1.INDIVIDUAL COMPONENTS IS LISTED IN THE RESPECTIVEDRAWINGS.THE PART LIST GIVES THE SUMMARY OF ALL THE2.COMPONENTS REQUIRED TO COMPLETE THE ASSEMBLY.AS SEVERAL ITEMS ARE BOUGHT-OUT, THE ACTUALQUATITIES (INCLUDING SPARES) IS LISTED IN ANNEXURE-2. THE SUPPLY OF THE ITEMS SHALL BE AS PER THE LISTGIVEN IN ANNEXURE-2ALL THE FASTENERS, BOLTS & WASHERS ARE LISTED IN3.ANNEXURE-1. LENGTH OF THE FASTENERS TO BEENSURED AT FABRICATOR SITE DURING TRIAL ASSEMBLYBEFORE SUPPLY.ALL HANDLING& AUXILARY SYSTEMS ARE PROVIDED IN4.ANNEXURE-3.ANY CHANGE IN THE MATERIAL/DIMENSIONS IN ANY OF5.THE COMPONENTS HAS TO BE MADE ONLY AFTER PRIORAPPROVAL FROM THE DESIGNER AS PER REVISEDDRAWING PROVIDED.

NOTE:DRAWINGS TO BE READ IN CONJUCTION WITH1.A) MEC/11/12/10HV/LDF/D/30001-30003 -REV2 (SHEETS- 3 NOS.) FOR INTEGRATED ENGINE TEST

FACILITY LOADING FRAME (ENGINE BAY)B) SE 2000.0500.2000.00.0AD FOR FRAME ASSSEMBLYTHE OUTER DIMENSIONS OF LOADING FRAME IS USED IN THE DRAWINGS FOR REPRESENTATION2.PURPOSE. NOT TO BE CONSIDERED FOR ANY FABRICATION DETAILS. REFERMEC/11/12/10HV/LDF/D/30001-30003 -REV2.ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP TESTING / ULTRASONIC TESTING/ RADIOGRAPHY3.ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY4.ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED5.STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING / WELDING IS6.INVOLVEDCHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHINING7.

TOTAL NO. OF DRAWING SHEETS : 11

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

STATUS

TENDER PURPOSE

FABRICATION

DISCUSSION / REVIEW

------------------------------

ONLY FOR REVIEW

------------------------------

3

2

4 12

11

9

7

68

10

6

8

1

13

(VIEW FROM BOTTOM OF LOADING FRAME)

A

A

19

17

16

20

(VIEW FROM TOP OF LOADING FRAME)

SECTION A-ASCALE 1 : 15

1 3

4

6

8 10

14

15

16

17

18

19

2

5

20

1 A

1 B

AB

15TYP

15TYP

15TYP15TYP

TEST STAND FORSEMI CRYO INTEGRATED ENGINE TEST FACILITY

(OVERALL ASSEMBLY DETAILS)

1 : 20 IPRC-SIET-TMS-01/A1 22

TOTAL WEIGHT : 51250 Kgs. (Approx)

REVISIONS SIGNZONE DATE

IPRC-SIET-TMS-04

IPRC-SIET-TMS-05

IPRC-SIET-TMS-02

IPRC-SIET-TMS-06

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-05

IPRC-SIET-TMS-07

IPRC-SIET-TMS-05

IPRC-SIET-TMS-05

IPRC-SIET-TMS-06

IPRC-SIET-TMS-08

IPRC-SIET-TMS-08

IPRC-SIET-TMS-08E250

E250

E250

E250

E250

EN 24

IS : 2062E450

E250

E450IS : 2062

E450IS : 2062

IS : 2062E250

IS 2062:E250,IS 2004:20C8,ASTM A106 GR.BIS 2062:E250,IS 2004:20C8,ASTM A106 GR.B

EN 24

EN 24

EN 24

EN 24

CONDITION-T

CONDITION-T

7404IS : 2062PULLEY BRACKET ASSEMBLY19

EN 24

IS : 2062

IS : 2062

IS : 2062

IS : 2062

IS : 2062

CONDITION-T

8315

7050

886

3495

360

150

20

18

10

36

162

305

40

895

2800

7620

16800

1

1

3

1

2

1

2

1

1

1

3

1

8

1

1

1

4

FIXED FRAME

THRUST FRAME

AXIAL LINK ASSEMBLY

ATMS INTERFACE PLATE

SIDE FRAME-1

SIDE FRAME-2

PITCH FORCE/YAW FORCE LINK

ROLL LINK ASSEMBLY

ATTACHMENT BLOCK

ATTACHMENT BLOCK TWIN EYE

LATERAL SAFETY STOPPER

SIDE FORCE CALIBRATION LINKASSEMBLY

ALIGNMENT JACKS

PLATE FOR PRE LOAD SUSPENSION

CALIBRATION INTERFACE PLATE

PRE LOAD FRAME

PRE LOAD SUSPENSION ASSEMBLY 18

17

16

15

14

13

12

11

10

9

8

7

6

5

4

3

2

IPRC-SIET-TMS-0315501IS : 2062E250

SPACER FRAME1

SHOWN ONLY FOR REPRESENTATION---1E250

IS : 2062LOADING FRAME20 NOTE:DRAWINGS TO BE READ IN CONJUCTION WITH1.A) MEC/11/12/10HV/LDF/D/30001-30003 -REV2 (SHEETS- 3 NOS.) FOR INTEGRATED ENGINE TESTSFACILITY LOADING FRAME (ENGINE BAY) B) SE 2000.0500.2000.00.0AD FOR FRAME ASSSEMBLYTHE OUTER DIMENSIONS OF LOADING FRAME IS USED IN THE DRAWINGS FOR REPRESENTATION2.PURPOSE. NOT TO BE CONSIDERED FOR ANY FABRICATION DETAILS. REFERMEC/11/12/10HV/LDF/D/30001-30003 -REV2.ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP TESTING / ULTRASONIC TESTING/ RADIOGRAPHY3.ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY4.ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED5.STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING / WELDING IS6.INVOLVEDCHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHINING.7.

SEQUENCE OF ERECTION:THE AXIAL THRUST MEASUREMENT SYSTEM IS CONNECTED TO1.BOTTOM OF LOADING FRAME THROUGH PART-5. THEWELDING OF THE ABOVE 60 Thk PLATE IS TO BE DONE WITHA WELD SIZE OF 15 MM ON BOTH OUTER AND INNERDIAMETERS(4750 AND 3400 MM RESPECTIVELY) AS SHOWN,AFTER OBTAINING CLEARANCE FROM SIET/IPRC.THE CALIBRATION SYSTEM IS CONNECTED TO TOP OF2.LOADING FRAME THROUGH PART-16.THE WELDING OF THEABOVE 60 Thk PLATE IS TO BE DONE WITH A WELD SIZE OF 15MM ON BOTH OUTER AND INNER DIAMETERS(4750 AND 3500MM RESPECTIVELY) AS SHOWN, AFTER OBTAININGCLEARANCE FROM SIET/IPRC.PRIOR TO THE WELDING OF THE PART-5 & PART-16, THE3.FOLLOWING IS TO BE ENSURED:

PLANARITY OF THE TOP & BOTTOM FACES WITH IN 1 MM.•CONCENTRICITY OF BOTH THE PLATES W.R.T LOADING•FRAME WITH IN 1MM.MATCHING OF AXES II-IV & I-III OF PART-5 & 16 WITH 2-4•&1-3 AXES OF LOADING FRAME.

REFERENCE AXIS:X- DIRECTION – ENGINE THRUST AXIS1.Y- DIRECTION – ENGINE II- IV AXIS2.Z- DIRECTION – ENGINE I-III AXIS3.

(THE AXIS MARKING OF I-II-III-IV ARE GIVEN IN PART DRAWINGS OF INDIVIDUAL COMPONENTS. WHEREVER MENTIONED, THESE ARE TO PUNCHED ON THE COMPONENTS DURING FABRICATION)

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PRPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

1

34

5

6

7

8

9

10

1112

13

14

2

AXIAL THRUST MEASURMENT SYSTEM

115

0

605

544

.75

194

2

3250

4750

4500

3100

1700

105

5

R2375 R2250 R

1550

R850

R1200

R625

R900

30°

30°

45°

45°

XX

II

IIII

IV

350

12.

25

1700

1250

3100

2750 PCD

SECTION X-XSCALE 1 : 15

AA

AA

4A

4B

4A

4C

4C

4D

4D

350

225

115

162

194

2

186

2

SECTION AA-AASCALE 1 : 10

225

g6

163.

30

115 R27

.50

R40

135 51.5

BBBB

M90

X4

90

135

5

45°

145

115 R40

850

225

g6

51.5

R27

.50

163.

30

SECTION BB-BBSCALE 1 : 5

5 MM UNDER CUT

PART - 4A

AXIAL LINK ASSEMBLY(QUANTITY - 3 NOS.)

95

111 340

M90 x 4 - 85 Lg

PART-4B(SCALE 1:5)

LOAD CELL SPECIFICATIONS:MAKE : SENSY/ EQUIVALENT

MODEL : 5105CAPACITY :1 MN

(NOTE: 3 NOS. OF DUMMY LOAD CELLS ARE TO BE SUPPLIED AS PER THE DIMENSIONS MENTIONED ABOVE.

MATERIAL : EN-24 CONDITION-T)DDDD

32 HOLES ON 290 PCD - 4 Nos.

30° T

YP

30°

CC

CC

M 30 TAPPED HOLES ON 290 PCD, THROUGH - 4 Nos.

26 HOLES ON 290 PCD WITH 40 COUNTERBORE

24 DEEP - 8 Nos.

350 --0.200.50

290 PCD

170

60

40 24

M24

225 H7

25.

4

SECTION CC-CCSCALE 1 : 5PART - 4C

350

225 H7 290 PCD

20 60

32

SECTION DD-DDSCALE 1 : 5PART - 4D

1 SPACER FRAME 1

2

3

4

AXIAL THRUST MEASURMENT SYTEM &

AXIAL LINK ASSEMBLY DETAILS

1 : 15 IPRC-SIET-TMS-02/A1 11

1550

REVISIONS SIGNZONE DATE

AXIAL LINK ASSEMBLY

THRUST FRAME

FIXED FRAME

3

1

1

886

7050

8315

CONDITION-TEN 24

IS 2062:E250,IS 2004:20C8,ASTM A106 GR.B

IS 2062:E250,IS 2004:20C8,ASTM A106 GR.B

IS : 2062E250

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

4D

4C

4B

4A

FLEXURE COVER PLATE

FLEXURE SEATING PLATE

LOAD CELL

MEASUREMENT FLEXURE

CONDITION-T

CONDITION-T

CONDITION-T

6

6

3

6

222

162

-

502

EN 24

EN 24

MAKE: SENSY/ EQUIVALENT

EN 24

DUMMY LOAD CELL TO BE SUPPLIED

E250IS : 2062E450

E250

E450IS : 2062

E450IS : 2062

IS : 2062

EN 24

EN 24

EN 24

EN 24

CONDITION-T

CONDITION-T

IS : 2062

IS : 2062

3495

360

150

20

18

10

36

162

305

40

1

2

1

2

1

1

1

3

1

8

ATMS INTERFACE PLATE

SIDE FRAME-1

SIDE FRAME-2

PITCH FORCE/YAW FORCE LINK

ROLL LINK

ATTACHMENT BLOCK

ATTACHMENT BLOCK TWIN EYE

LATERAL SAFETY STOPPER

SIDE FORCE CALIBRATION LINKASSEMBLY

ALIGNMENT JACKS14

13

12

11

10

9

8

7

6

5 E250

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED5. CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHNING

ONLY FOR REVIEW

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

3.7

7.5° (TYP)

7.5° (TYP)

X

X

10 THK STIFFENERS (PART-4)- 48 NOS.

10 THK STIFFENERS (PART-3)- 48 NOS.

370

45

45 1800

1700

1420 +0.25

0

7

18

SECTION X-XSCALE 1 : 6

0.2 A

0.2 A

B

A

15 TYP

70 210

70

70

56 112

56 28

57°

57°

1250

1700

R780

R795

PART-2

M20 TAPPED HOLES, 40 DEEP. ON 1560 PCD- 20 NOS.(TO SUIT ENGINE FRAME ASSEMBLY)

UNDER HOLD

M12 TAPPED HOLES, 20 DEEP. ON 1590 PCD- 14 NOS.(TO SUIT ENGINE FRAME ASSEMBLY)

1250 1800

3.7

18 THROUGH HOLES EQUISPACED ON 1710 PCD- 48 NOS.

50

1620

DEVELOPMENT OF PART-5(PLATE SIZE REQUIRED 280x50Thk - 5010Lg)

20 TYP

90

280

40

135

280

1

2

3

3

5

1 1

2

3

4

5

SPACER FRAME

1 : 6 IPRC-SIET-TMS-03/A1 11

440

TOTAL WEIGHT : 1550 Kgs. (Approx)

REVISIONS SIGNZONE DATE

CIRCULAR RING-O.D1620XWIDTH280X50Thk

STIFFENER-280X135X10Thk

STIFFENER-280X90X10Thk

1

45

45

1

540

140

65

365

IS : 2062E250

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

PART-3(THE EXISTING GAP BETWEEN

BOTH ENDS HAS TO BE CHECKED BEFOREWELDINGTHE RIB)

PART-4(THE EXISTING GAP BETWEEN

BOTH ENDS HAS TO BE CHECKED BEFORE WELDING THE RIB)

IVII

I

III

PART-1

BIG END PLATE-O.D1800XI.D1250X45Thk

SMALL END PLATE-O.D1700XI.D1250X45Thk

IS : 2062E250

IS : 2062E250

IS : 2062E250

IS : 2062E250

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED5. CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHNING

ENGINE INTERFACE ON HOLD. CLEARNACE TO BE OBTAINED FROM SIET/IPRC

UNDER HOLD

SEQUENCE OF FABRICATION:PRE-MACHINING OF PART-1 AND PART-21.WELDING OF PART 3, PART-4 AND PART-5 AND FOLLOWED BY STRESS RELIEVING2.FINAL MACHINING OF END FLANGES FOR PLANARITY3.DRILLING & TAPPING OF INTERFACE HOLESIN SINGLE SEETING AS PER GIVEN TOLERANGES4.

ONLY FOR REVIEW

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

X

X

Y Y

IV

I

II

III

-

15TYP

12 TYP

1

2

7

3

5

6

4

8

55°

R 1475

R 1200

R 1981.5

R 1375

R 2250

R 1550

SECTION X-XWELD DETAILS

PART-5(SCALE 1:10)

PART-7(SCALE 1:5)

15 TYP

15 TYP

6 TYP

12 TYP

62.

75

110

00.

2

4500 --0.500.75

SECTION Y-YSCALE 1 : 15

0.2 A0.2 A

A

20°

15° 1

15°

20°

20°

15°

15° 10°

30°

10° 15°

15° 20

°

20°

10°

10°

15°

30°

15°

20°

2950

4500

10°

15°

15°

40 THROUGH HOLES ON 3700 PCD,19 NOS.

40 THROUGH HOLES ON 4300 PCD,19 NOS.

40 THROUGH HOLES ON 4000 PCD,16 NOS.

PART-1(DETAILS OF CONSTRUCTION AND THROUGHHOLES)

I

II

III

IV

TYP

1875 0.5

130

125

260

500 105

50.

5 1550 0.5

115

105

420

230

15°

45°TYP

45° 45°

PART-1(DETAILS OF TAPPED HOLES FOR SIDE FRAMES

AND ALIGNMENT JACKS)

II

I

IV

III

M90X4 TAPPED HOLES, THROUGH, EQUISPACED ON 3140 PCD, 8 NOS.

M36X4 TAPPED HOLES, THROUGH, 12 NOS. ( AT 6 LOCATIONS AS SHOWN)

M36X4 TAPPED HOLES, THROUGH, 11 NOS.(AT 2 LOCATIONS AS SHOWN)

6°TYP 6°TYP

120°

120°

120°

30°

30° Z

ZM20 TAPPED HOLES, 30 DEEP,

ON 2450 PCD, 9 NOS. (ON BOTH SIDES)

150 THROUGH HOLES EQUISPACED ON 2750 PCD,3 NOS.

PART-2PART-8

(SCALE 1:5)

3100

2400

180

82.50

100

100

125°

SECTION Z-Z

520

1055

84.25

° 310

R80

160

96.

5

80

PART-4(THE EXISTING GAP BETWEEN THE

PIPES HAS TO BE CHECKED BEFOREWELDINGTHE PLATE)

140

55°

1115

300

700

100

150

50

350

R120

0

R155

0 150

30°

30°

M24 TAPPED HOLES, 48 DEEP, ON 290 PCD, 8 NOS.

(TO BE DRILLED AFTER WELDING) 85

205

115

25

100 200

80 25

1 BIG END PLATE 1

2

3

4

5

6

7

8

FIXED FRAME

1 : 15 IPRC-SIET-TMS-04/A1 11

4350

TOTAL WEIGHT : 8350 Kgs. (Approx)

REVISIONS SIGNZONE DATE

STIFFENER-200x100x16Thk

STIFFENER-205x85x16Thk

STIFFENER-1115x140x16Thk

BASE PLATE- 40 Thk

STIFFENER-1055x520x20Thk

PIPE-O.D 168.28x21.95Thk1115Lg (Approx.)

SMALL END RING

6

6

6

3

3

6

1

12

12

64

217

195

530

2970IS : 200420C8

ASTM A106GR.B

IS : 2062E250

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

PART-6(THE EXISTING GAP BETWEEN

BOTH ENDS HAS TO BE CHECKED BEFOREWELDINGTHE RIB)

XXS SCHEDULE

IS : 2062E250

IS : 2062E250

IS : 2062E250

IS : 2062E250

IS : 2062E250

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY.2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY.3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED.5. CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHNING.

SEQUENCE OF FABRICATION:PREPARATION OF PART-1 BY WELDING FROM TWO PLATE1.SEGMENTS AS PER DRAWING. APPROVAL IS TO BEOBATIANED FROM DESIGNER IN CASE OF NON-AVAILABITYOF REQUIRED PLATE SIZES ALONG WITH PROPOSEDSEGMENT SIZES.PRE-MACHINING OF PART-1 AND PART-2.2.WELDING OF PART 3, PART-4 AND PART-5 AFTER3.ENSURING GAPS BETWEEN PIPES, FOLLOWED BY STRESSRELIEVING.FINAL MACHINING OF PART-1 AND PART-5 END FACES FOR4.PLANARITY.DRILLING & TAPPING OF ALL INTERFACE HOLES ON END5.FACES AS PER TOLERANCE SPECIFICATIONS IN A SINGLESETTING.

ONLY FOR REVIEW

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

1

5

3

4A

2

4B

120

° TYP

15°

30° 30°

30°

30°

30° 30°

45° TYP

30°

30°

X

X

150 THROUGH HOLE ON 2750 PCD EQUISPACED ,3 NOS. 68 HOLE, 5 mm DEEP

ON 3140 PCD EQUISPACED ,8 NOS.

M 48 TAPPED THROUGH HOLE, ON 2400 PCD , 9 NOS.

III

IV

I

II0.1 B

0.1 B

0.1 B

3250 2250

3140 PCD

M48

150 68

5

150

175

150

175

65

150°

SECTION X-XSCALE 1 : 15PART-1

45° TYP

7.5°

15° TYP 3.75°

7.5° TYP

120

YY

III

IV

I

M 16 TAPPED HOLE, 30 DEEP ON 1710 PCD , EQUISPACED ,48 NOS.

M 56 TAPPED HOLE, 60 DEEP RADIALLY , EQUISPACED ,8 NOS.

M 20 TAPPED HOLE, 40 DEEP ON 1330 PCD ,EQUISPACED ,24 NOS.

0.1 B

0.1 B

0.1 B

1420

1800

1260

5

185

95

30°

46.35 M 20

M 16

SECTION Y-YSCALE 1 : 10

95 120

45

180

5

R16

25

R112

5

20°

30°

30°

R1375

30°

ZZ

M 24 TAPPED HOLE, 48 DEEP ON 290 PCD,8 NOS.

(TO BE DRILLED AFTER WELDING)

150

5

37 350

++

0.500.20

SECTION Z-ZSCALE 1 : 10

1190

1190 237.5

554.5

SCALE 1:10PART-4A

(THE EXISTING GAP BETWEEN THEPIPES HAS TO BE CHECKED BEFOREWELDINGTHE PLATE)

15°

30° TYP

30°

30°

N

N

P

P

II

III

IV

I

68 HOLE, 5 mm DEEP ON 3140 PCD EQUISPACED ,8 NOS.

M 24 TAPPED HOLE, 48 DEEP ON 190 PCD,8 NOS.

10 TYP

15 TYP

127

5.50

1260

1420

1800

95

185

150

37

5

60°

3250

2250

68

5

1560 PCD

2750 PCD

119

0

SECTION N-NSCALE 1 : 15

0.2 A

A

15 TYP

15 TYP

M 5

6 X

5.5

50

+ -0.10

0.10

2750 PCD

185

95

1420 --0.150.30

5

CSECTION P-PSCALE 1 : 15

0.2 A0.2 B

0.2 B

BA

15 TYP

350 +0.25

0

5

68

5

150

3

7

65

DETAIL CSCALE 1 : 5

0.2 B0.2 A 15 TYP

1410

15° TYP

7.5°

QQ

38 THROUGH HOLE ON 1330 PCD EQUISPACED ,24NOS.

36 THROUGH HOLE ON 1100 PCD EQUISPACED , 4 NOS.

1410 4

0 1100 PCD

SECTION Q-QSCALE 1 : 10

PART-6

250

300

1900

2400

2500

15°

6° T

T

22 THROUGH HOLE ON 2450 PCD , 3NOS.

12 TYP

16

16

180

24 24

212

22

22SECTION T-TSCALE 1 : 5PART-7

12 TYP

30

Tilt Saddle

Mechanical Jack

Mechanical JackSeating Block

M 90 X4 Thin Lock NutWITH A/F 140, 30 THK

R

R

140

657

50 155

30

62.75

SECTION R-RSCALE 1 : 5

PART-8

M 6

4 SQ

THR

EAD

500

525

595

32.5

36 T

HRO

UGH

HOLE

S

45°

5

140

39.3

50

MECHANICAL JACK

160

45°

5

M 90 X4

100

155

M 64 SQ THREAD

MECHANICAL JACKSEATING BLOCK

1190

237.50

1190

42.5

R50

168.5 554.5

142.5

SCALE 1:10

PART-4B(THE EXISTING GAP BETWEEN THE

PIPES HAS TO BE CHECKED BEFOREWELDINGTHE PLATE)

1 BIG END RING 1

2

3

4A

5

THRUST FRAME

1 : 15 IPRC-SIET-TMS-05/A1 11

TOTAL WEIGHT : 8050 kg. (Approx)

REVISIONS SIGNZONE DATE

STIFFENER-1

PIPE O.D168.28X21.95Thk-1190Lg

SMALL END RING

3

3

12

1

IS : 200420C8

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

II

E250

E250

20C8

IS : 2062

IS : 2062

ASTM A 106Gr. B

IS : 2004

BASE PLATE

(WELD DETAILS: PART NO. 5 TO PART NO. 1)

(WELD DETAILS: PART NO. 4 TO THRUST FRAME)

PART-2

PART-5

6 PRELOADING INTERFACE PLATEE250

IS : 20621

7 LATERAL SAFETY FIXTURE IS : 2062E250 3

8 ALINGNMENT JACK ASSEMBLYE250

IS : 20628

1400

4000

1130

238

390

475

162

40

TILT SADDLE MAKE:POWERTEAM/ EQUIVALENT 8 159 PART NO: 351325

SEQUENCE OF FABRICATION:PREPARATION OF PART-1 AND PART-2 BY FORGING (100% RT).1.PRE-MACHINING OF PART-1 AND PART-22.WELDING OF PART 3, PART-4 AND PART-5 AFTER ENSURING3.GAPS BETWEEN PIPES, FOLLOWED BY STRESS RELIEVINGFINAL MACHINING OF PART-1 AND PART-5 END FACES FOR4.PLANARITYDRILLING & TAPPING OF ALL INTERFACE HOLES ON END FACES5.AND IN RADIAL DIRECTION AS PER TOLERANCE SPECIFICATIONSIN A SINGLE SETTING

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED5. CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHNING

ONLY FOR REVIEW

XXS SCHEDULE

2003IS : 2062E250

STIFFENER-24B

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

7.5°

TYP

YY

IV

II

M36 TAPPED HOLES, THROUGHON 4300 PCD,24 NOS.

M36 TAPPED HOLES, THROUGHON 3700 PCD,24 NOS.

TYP

20°

15°

20°

15° 1

20°

20°

15°

15° 20°

15°

15° 20

°

20°

20°

15°

30°

30°

10°

10°

50°

XX

I

M36 TAPPED HOLES, THROUGHON 4300 PCD,19 NOS.

M36 TAPPED HOLES, THROUGHON 4000 PCD,16 NOS.

M36 TAPPED HOLES, THROUGHON 3700 PCD,19 NOS.

TYP

60

3400

4750

10

4500 ++

0.750.50

SECTION X-XSCALE 1 : 10

4500 ++

0.750.50

60

3500

4750

22.

50

SECTION Y-YSCALE 1 : 10

1 1

2

INTERFACE PLATES

1 : 10 IPRC-SIET-TMS-06/A1 11

3500

TOTAL WEIGHT : 6300 kg. (Approx)

REVISIONS SIGNZONE DATE

1 2800

IS : 2062E250

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

IV

II

I III

PART-1 PART-2

FIXED FRAME INTERFACE PLATE

CALIBRATION INTERFACE PLATE IS : 2062E250

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED5. CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHNING

III

SEQUENCE OF FABRICATION:PREPARATION OF PART-1 AND PART -2 BY WELDING FROM MULTIPLE PLATES AS1.PER DRAWING, FOLLOWED BY STRESS RELIEVINGAPPROVAL IS TO BE OBATIANED FROM DESIGNER IN CASE OF NON-AVAILABITY OF2.REQUIRED PLATE SIZES ALONG WITH PROPOSED SEGMENT SIZES.FINAL MACHINING OF PART-1 AND PART-2 END FACES FOR PLANARITY3.DRILLING & TAPPING OF ALL INTERFACE HOLES ON END FACES AS PER TOLERANCE4.SPECIFICATIONS IN A SINGLE SETTING

ONLY FOR REVIEW

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

(MEASUREMENT AND CALIBRATION) ISRO PROPULSION COMPLEX

MAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

675

515

45

R25

M52 x 3.0 - 80 Lg (RH THREAD)

M52 x 3.0 - 80 Lg (LH THREAD)

PART-2( SIDE FORCE LINKTO BE SUPPLIED

WITH M 52X 3 THIN NUT-2 NOS. )

175

M52 x 3.0 - 70 Lg

PART-3ROD END BEARING SPECIFICATIONS:

MAKE : INA/ EQUIVALENTMODEL : GI R 60 UK-2 RS ( 1 No.)

GIL 60 UK -2RS ( 1 No.)( FOR EACH LINK)

BASIC LOAD RATING : 485 kN

1330

M45 x 3.0 - 75 Lg(RH THREAD)

M45 x 3.0 - 75 Lg(LH THREAD)

PART-8( ROLL LINK TO BE SUPPLIED

WITH M 45X 3 THIN NUT-2 NOS. )

160

M45 x 3.0 - 68 Lg

PART-9ROD END BEARING SPECIFICATIONS:

MAKE : INA/ EQUIVALENTMODEL : GIR 50UK-2 RS ( 1 No.)

GIL 50 UK -2RS ( 1 No.)( FOR EACH LINK)

BASIC LOAD RATING : 485 kN

60

30

260

PART-5( CUSTOMISED M60 HEXAGONAL HEAD BOLT TO BE SUPPLIED WITH NUT OF 30 MM HEIGHT & 8 MM

THK WASHERS)

M60 x 4 - 70 Lg

50

235

30

PART-11( CUSTOMISED M48 HEXAGONAL HEAD

BOLT TO BE SUPPLIED WITH NUT OF 30 MM HEIGHT & 8 MM THK WASHER)

M48 x 3 - 65 Lg

80

100

10 10 185

5 THROUGH HOLE

PART-20(SUITABLE COTTER PIN TO BE SIPPLIED

WITH PIN)

230

PART-18ROD END BEARING SPECIFICATIONS:

MAKE : INA/ EQUIVALENTMODEL : GIR 80UK-2 RS ( 1 No.)BASIC LOAD RATING : 689 kN

M64 x 4.0 - 85 Lg

260

88.5

69

PART-17LOAD CELL SPECIFICATIONS:MAKE : SENSY/ EQUIVALENT

MODEL : 5105CAPACITY :500 kN

M64 x 4 - 65 Lg

M64 x 4 - 65 Lg

100

100

2-412 "-8 x 40 MM Lg

M64 x 4 - 65 Lg

PART-16( SEE PART-14 FOR MATING DETAILS)

534-12 THROUGH

THREAD TO SUIT PART-14

PART-15(40 THK)

25 HOLES ON 100 PCD - 8 Nos.

1

532

3

6

4

SIDE FRAME -1 ASSEMBLY (QTY.-02 NOS.)

30

240

60

PART-6( CUSTOMISED M60 HEXAGONAL HEAD BOLT TO BE SUPPLIED WITH NUT OF 30 MM HEIGHT & 8 MM

THK WASHERS)

M60 x 4 - 60 Lg

M 56 X 5.5

140

87

R15

40

100

60

125

130

60

140 90 55

175

220

PART-04( ATTACHMENT BLOCK TO BE SUPPLIED

WITH THIN NUT OF M 56 SIZE)

8 TYP

M 56 X 5.5

87

R15

180

40

125

2

20 130

R90

100

60

140

180 9

0

25 60

17.5 17.5

8 TYP

605

+ -0.5

0.5

690

40

25

460

24

25

20

16

108 125

105 105

250

40 TYP

600

390

210

95

180 105

X

XPART-1

( SIDE FRAME-1)

12TYP12 TYP

8 TYP

600

350

16

98

125 108

130

1

30

45

50 125 125 125 125

10

40 THROUGH HOLES,12 NOS.

6TYP

605

+ -0.5

0.5

185 150 100 65

60

100

100 350

25

150

4

5

75

25

SECTION X-XSCALE 1 : 5

8TYP

12 TYP

12 TYP

78

9

9

11

SIDE FRAME -2 ASSEMBLY 10

12

180

90 2

4

470

605

+ -0.5

0.5

690

150

25

25 330

40

250

85

500

85 40

12

96 105

90

Y

Y

PART-7( SIDE FRAME-2)

12TYP 12 TYP

8 TYP

605

+ -0.5

0.5

50 90 50

80 130 154

25

24

310 2

5

75 25

150

SECTION Y-YSCALE 1 : 5

8TYP

12 TYP

12 TYP

310

500

40 105 105 105 105

40

115

1

15

12

86

10

105 96 6TYP

M 56 X 5.5 330

190

150

1

30

80

46

25

25

86

110

150

60

50 90

PART-10( TWIN EYE ATTACHMENT BLOCK TO BE SUPPLIED WITH THIN NUT OF M 56 SIZE)

8 TYP

M 56 X 5.5

110

150

1

30

130 90 50 8 TYP

330

130

190

25

45°

95

30

50

220

PART-12( CUSTOMISED M48 HEXAGONAL HEAD

BOLT TO BE SUPPLIED WITH NUT OF 30 MM HEIGHT & 8 MM THK WASHER)

M48 x 3 - 70 Lg

CALIBRATION SIDE FRAME ASSEMBLY

15

16

17

18

19

20

1314

250

50 40 40

310

3

2

605

+ -0.5

0.5

390

40

25 25

100

350

45° TYP

N

N

M 24 TAPPED HOLES, THROUGH, 7 NOS.

692

4

0

600

50 310

3

2

340

145

45

25

150

45

75

105

230

16 108

105

Z

Z

PART-13( CALIBRATION SIDE FRAME)

SECTION Z-ZSCALE 1 : 5

12TYP

15TYP

12 TYP

12TYP

350

600

45 130 130

50

125

1

25

125

1

25

16

10

98

125

1

08

125

390

50

25

25

40 THROUGH HOLES,12 NOS.

15 TYP

12 TYP

SECTION N-NSCALE 1 : 5

12 TYP

15TYP

12 TYP

12 TYP

M56 X 5.5

200

150

50

80

150

R100 PART-19( ATTACHMENT BLOCK TO BE SUPPLIED

WITH THIN NUT OF M 56 SIZE)

M56 X 5.5 130

95 R15

60 80 130 170

80

150

250

50

130

200

100

65

80

150

25

20 8TYP

PART-14HYDRAULIC JACK SPECIFICATIONS:MAKE : POWER TEAM/ EQUIVALENT

MODEL : RD8013CAPACITY : 44 tons (Pull)

100 tons (Push)

1 SIDE FRAME-1 2

2

3

4

5

6

7

8

SIDE FRAMES & LINKS

1 : 5 IPRC-SIET-TMS-07/A1 11

360

TOTAL WEIGHT : 1135 kg. (Approx)

REVISIONS SIGNZONE DATE

ATTACHMENT BLOCK-1

ROD END BEARING - 60 MM

PITCH/YAW FORCE LINK

2

4

2

20

20

IS : 2062E450

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

MAKE : INA/EQUIVALENT

EN 24

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.TESTING / ULTRASONIC TESTING / RADIOGRAPHY.ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY.2.ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED.3.STRESS RELIEVING IS TO BE DONE FOR ALL THE4.PARTS WHEREVER HEAVY MACHNING /WELDING ISINVOLVED.CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION5./ MACHNING.SUITABLE BREATHING HOLES TO BE PROVIDED FOR CLOSED6.SECTIONS & SAME TO BE PLUGED AFTER FINAL FABRICATION.

EN 24CONDITION-T

60 PIN -SIDE FRAME SIDE EN 24 2

2 5

5

13

12

11

10

9

CALIBRATION SIDE FRAME 1

15

14

JACK BODY PLATE- 40Thk

HYDRAULIC JACK - 44T

EN 24 2

2

17

16

LOAD CELL- 50T

JACK ADAPTOR 2

POWER TEAM MAKE:RD 8013

18 - 2

-

18

10.5

-

20

19 ATTACHMENT BLOCK-2

EN 24

EN 24

2

2

16

60

SEQUENCE OF FABRICATION FOR SIDE FRAMES:THE BASE PLATES OF THE SIDE FRAMES ARE MADE OF1.SINGLE PLATE WITH 25 MM SLOTS FOR INSERTING THEVERTICAL PLATES. REFER INDIVIDUAL DRAWINGS FOR LENGTHDETAILS.PREPARATION OF BASE PLATES AND INDIVIDUAL PARTS TO2.MATCH THE OVERALL DIMENSIONS.EDGE-PREPARATION AND WELDING OF PLATES AS SHOWN IN3.DRAWING, FOLLOWED BY STRESS RELIEVING.FINAL MACHINING OF BASE PLATE BOTTOM FACE FOR4.PLANARITYDRILLING & TAPPING OF ALL HOLES ON BASE PLATE AND5.FACE PLATES BY MAINTAINING THE PERPENDICULARITY ASPER TOLERANCE SPECIFICATIONS IN A SINGLE SETTING.

- -

60 PIN -THRUST FRAME SIDE EN 24

EN 2450 PIN -THRUST FRAME SIDE

--

4

42

2EN 2450 PIN -SIDE FRAME SIDE

EN 24CONDITION-T

EN 24

MAKE : INA/EQUIVALENT

36

36

2

4

1

ROLL LINK

ROD END BEARING - 50 MM

TWIN-EYE ATTACHMENT BLOCK

3002IS : 2062E450SIDE FRAME-2

IS : 2062E450

-

EN 24

DUMMY LOAD CELL TO BE SUPPLIED

-2

ROD END BEARING - 80 MM MAKE : INA/EQUIVALENT

80 PIN -THRUST FRAME SIDE

ONLY FOR REVIEW

240

EN 24CONDITION-T

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

2

1

3

7.5°

15°

4500

2950

40 THROUGH HOLES EQUISPACED

ON 3700 PCD, 24 NOS.

40 THROUGH HOLES EQUISPACED

ON 4300 PCD, 24 NOS.

M90 TAPPED HOLES, THROUGH, EQUISPACEDON 3150 PCD, 12 NOS.

15°

3800

R50 100

1150

175

254

687.50

127

R

550

120 THROUGH HOLES, EQUISPACED

ON 3150 PCD, 12 NOS.

M24 TAPPED HOLES,THROUGH, 4 NOS.

X

X

ASTM PIPES 12 Nos.(8 PIPES WELDED WITH RIBS)

IV

III

II

I

592

500

4500 --0.500.15

3800

2950

1100

60

32

3400 PCD

SECTION X-XSCALE 1 : 20

6 TYP

10TYP

700

500

150

750

60

150

0 2

00

160

80

75

30

50

125

M36 TAPPED HOLE

M80 TAPPED HOLE

M80 TAPPED HOLE

80 ROD WITH M 80 THREAD (1675 mm Lg.)

26 THROUGH HOLES WITH 50 COUNTER BORE 30 DEEP,

ON 500PCD-4 NOS12

5

6

NOTE FOR PART-6:OUT OF 32 NOS. OF1.PLATES FOR EACH PRELOADASSEMBLY. THE WEIGHT FOR24 NOS. CAN BE MADEFROM A SINGLE BLOCK BYCASTING (IS1030 GR230/450W)ALL THE PLATES SHALL BE2.COATED WITH TEFLON/PVCTO PREVENT CORROSION.10

120

R60

750

M24 TAPPED HOLES, THROUGH ON 500 PCD - 3 NOS.

8

9

7

8 TYP

Y

YSECTION Y-YSCALE 1 : 2

1112

1314

15

16

17

325

175

254

250

PART-8(SCALE 1:5)

25 HOLES,THROUGH, 4 NOS.

90

32

32

113 113

6TYP

780

890

47

300 R100

400

32

150

512.50

250

9

8

6TYP

65

200 Z

Z

72

R8

10°

20

20

150 65

47

10

14°

3

3

80

120

100 PCD

3

R1

26

9

10

SECTION Z-ZSCALE 1 : 1.5

M8 TAPPED HOLES, 16 DEEP ON 100 PCD - 4 NOS.

10 MM GROOVE (WITH 14 ) FOR FELT SEAL

30

140

100

20 6

3.50

47

M30 x 45 Lg

PART-12(SCALE 1:2)

120

10

80

75

6 3

A

A

100 PCD 65

65

10

3

3

47

14°

SECTION A-ASCALE 1 : 1.5

9 HOLES THROUGH, WITH 14 COUNTER BORE 4 DEEP, 4 NOS.

10 MM GROOVE (WITH 14 ) FOR

FELT SEAL

72

30

47

30

47.50

80 30

B

B

PART-16(SCALE 1:1)

26

16

47

SECTION B-BSCALE 1 : 1

152

5

120

75

120 ROD WITH M90

THREAD- 75 Lg

M90 STUD- 1525 Lg

M24 TAPPED HOLE- 36 Lg.

325

150

175

700

PART-9(SCALE 1:5)

400

R100

512.50

24

63

250

300

858

700

PART-7(SCALE 1:5)

1370

20

PART-10(SCALE 1:10)

M20 X 100Lg M20 X 100Lg

1 BIG END PLATE-60Thk 1

2

3

4

5

6

7

8

PRELOAD AND SAFETY FIXTURE

----- IPRC-SIET-TMS-08/A1 11

4175

TOTAL WEIGHT : 26000 kg. (Approx)

REVISIONS SIGNZONE DATE

STIFFENER-700x500x10Thk

PIPE-O.D 168.28x21.95Thk500Lg

SMALL END PLATE-32 Thk

8

12

1

298

475

2495

ASTM A106GR.B

IS : 2062E250

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

PART-2

XXS SCHEDULE

IS : 2062E250

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED5. CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHNING

PART-1

IV

I III

II

PART-4(SCALE 1:15)

IS : 2062E250

PRELOAD HOLDER IS : 2062E250 4

PART-4 - ASSEMBLY(SCALE 1:10)

PART-5(SCALE 1:10)

PRELOAD PLATE (122 KG. EACH) IS : 2062E250 128 15616

1184

SIDE PLATE-32Thk IS : 2062E250

IS : 2062E250 4

8

PART-7 WITH WELD DETAILS(SCALE 1:5)

13

12

11

10

9

CYLINDRICAL ROLLER BEARING

SHAFT

PULLEY

STIFFENER-325x700X24Thk

IS : 2062E250

IS : 2062E250

IS : 2062E250

IS : 2062E250

4

4

4

4

4

15

14

SLEEVE-1

CLOSING PLATE

IS : 2062E250

IS : 2062E250

4

4

17

16

M30 NUT

SLEEVE-2

IS : 2062E250

IS : 2062E250

4

4

PART-14(SCALE 1:10)

PART-11(SCALE 1:1.5)

PART-13(SCALE 1:1)

PART-15(SCALE 1:1)

PART-18(SCALE 1 :10)

536

BASE PLATE-250x325x32Thk 78

140

15TIEROD O.D 20X1370 Lg WITH M20 NUTS (2 NOS.)

44

12

SKF MAKE:NU2306ECP--

SAFETY STUD-1525 Lg18 IS : 2062E250 16

3

2

2

1

940

ONLY FOR REVIEW

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

30° TYP

7.5° 15° TYP 15°

30° TYP

700

700

XX

42 THROUGH HOLEEQUISPACED ON 4300PCD 24 NOS.42 THROUGH HOLE

EQUISPACED ON 3700 PCD 24 NOS.

20 THROUGH HOLEEQUISPACED ON 4000 PCD 12 NOS.

M 48 TAPPED HOLES,80 DEEP - 4 NOS.

10 TYP

60°

1790

590

65

150

4500 --0.500.75

3500

241

8

50

146.40

30°

265

8.6

90°

168.28

21.95

1350 PCD

3960 PCD

2610

SECTION X-XSCALE 1 : 15

0.2 A

A

15 TYP

15 TYP

1

3

4

2 CALIBRATION FRAME

865

188

261

5

261

5

PART-04(12 Thk.)

56

7

8

9

10

CALIBRATION PLATE

112

TYP

70 TYP

30° TYP

R830

R740

20° TYP

12°

TYP

32

R780 57°

57°

YY

22 THROUGH HOLEON 1560 PCD -12 NOS.

M250X 4 250

500

1800

80

560

80

800

700 15

20

SECTION Y-YSCALE 1 : 15

15 TYP

15 TYP

10 TYP

8 TYP

8 TYP

45° TYP 32

16° TYP

M 24 TAPPED HOLES,ON 600 PCD,48 DEEP - 8 NOS.

45° TYP

ZZ

M 24 TAPPED HOLES,ON 600 PCD,48 DEEP - 8 NOS.

M250X 4 500

480

250

80

800 700

15

SECTION Z-ZSCALE 1 : 15

PART-06

400

350

130

20

PART-07

32

400

500

20

80

PART-08

32

80

R740

R830

112 12°

22

R780

PART-10SCALE 1:5

20

70

20°

R830

R740

22

R780

PART-9SCALE 1:5

20

N

N

M 36 TAPPED HOLES,ON 440 PCD,55 DEEP,EQUISPACED-12 NOS.

JACK ADAPTOR(PART-11)

540

M 3

50 X

4

500

440

PC

D

SECTION N-NSCALE 1 : 10

10 X 45 CHAMFER

P

P

BEARING HOUSING(PART-12)

40 THROUGH HOLES, ON 440 PCD,36 DEEP, EQUISPACED-12 NOS.

54

0

120

340

+0.0

40

440

PC

D

259

40

SECTION P-PSCALE 1 : 10

265

Q

Q

INSITU CALIBRATION LINK(PART-13)

100

1175

M 1

25 X

4

150

265

200

- -0.05

0.07

SECTION Q-QSCALE 1 : 10 5 X 45 CHAMFER

190

R

R

300T LOAD CELL(PART-14)

LOAD CELL SPECIFICATIONS:MAKE : SENSY/ EQUIVALENT

MODEL : 5105CAPACITY :3 MN

M 1

25 X

4- 1

35 L

M 1

25 X

4 -1

35 L

440 140 160

190

SECTION R-RSCALE 1 : 10

250

T

T

3375 150

250

270

M 2

50 X

4

M12

5 X4

SECTION T-TSCALE 1 : 10INSITU CALIBRATION TIE ROD

(PART-15)

M350 X 4

350

100

680

335

(SCALE 1 : 15)

(PART-16)HYDRAULIC JACK SPECIFICATIONS:

MAKE :LARZEP/ EQUIVALENTMODEL : TD100015/C ( 1 No.)

CAPACITY : 985 t (PULL)STROKE : 150 MM

1000T HYDAULIC JACK (AT MID STROKE)

900

900

700

700

R100

B

B

AXIAL SPHERICAL PLAIN BEARING(PART-17)

ROD END BEARING SPECIFICATIONS:MAKE : INA/ EQUIVALENT

MODEL : GE 200 AW ( 1 No.)BASIC LOAD RATING : 7100 kN

87 60

200

246

SECTION B-BSCALE 1 : 10

6

4500

400

7.5° 15° TYP

30° TYP

15° TYP

SS

42 THROUGH HOLEEQUISPACED ON 3700 PCD 24 NOS.

M 16 TAPPED THROUGH HOLEEQUISPACED ON 4000 PCD 12 NOS.

42 THROUGH HOLEEQUISPACED ON 4300PCD 24 NOS.

6 MM Thk RIBS,24 NOS.

3 TYP

6

50

100

1530

400

4500

SECTION S-SSCALE 1 : 20

WORKING PLATFORM(PART-18)

6 MM THK CHQ PLATE

1 1

2

CALIBRATION SYSTEM

1 : 15 IPRC-SIET-TMS-09/A1 11

2425

REVISIONS SIGNZONE DATE

1 1900

IS : 2062E250

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

BIG END PLATE

SMALL END RING IS : 200420C8

TOTAL WEIGHT : 13115 kg. (Approx)

17

16

15

14

13

12

11

10

9

8

7

6

5

4

3

AXIAL SPHERICAL PLAIN BEARING

1000 T HYDAULIC JACK

INSITU CALIBRATION TIE ROD

LOAD CELL - 3 MN

INSITU CALIBRATION LINK

BEARING HOUSING

JACK ADAPTOR

PAD-2

PAD-1

STIFFENER -400X350X32Thk

END BLOCK

PLATE- O.D 1800 X 80 Thk.

STIFFENER-2615X 865X16Thk.

PIPE O.D 168.28X21.95ThK.2610-Lg.

IS : 2062E250

EN 24CONDITION-T

EN 24

EN 24

EN 24

EN 24

IS : 2062E250

IS : 2062E250

IS : 2062E250

EN 24(ANNEALED)

IS : 2062E250

ASTM A 106GR. B

1

1

1

1

1

1

1

4

2

22

12

1

1

3

12

35

1920

1275

-

290

135

510

11

10

130

300

908

1450

375

2475 XXS SCHEDULE

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED5. CHECK FOR THE STATUS OF DRAWING BEFOREFABRICATION/MACHNING

STIFFENER -500X80X32Thk

EN 24

MAKE:LARZEP / EQUIVALENT

MAKE:INA / EQUIVALENT

ONLY FOR REVIEW

SEQUENCE OF FABRICATION FOR CALIBRATION FRAME:PREPARATION OF PART-1 BY WELDING FROM MULTIPLE PLATES. PART-02 IS FORGED.1.PRE-MACHINING OF PART-1 AND PART-22.WELDING OF PART 3, PART-4 AFTER ENSURING GAPS BETWEEN PIPES, FOLLOWED BY3.STRESS RELIEVINGFINAL MACHINING OF PART-1 AND PART-4 END FACES FOR PLANARITY4.DRILLING & TAPPING OF ALL INTERFACE HOLES ON END FACES AS PER TOLERANCE5.SPECIFICATIONS IN A SINGLE SETTING.

DUMMY LOAD CELL TO BE SUPPLIED

8651WORKING PLATFORM18 IS : 2062E250

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETDRG. NO.SCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

1

3

4

2

INTERFACE FRAME

A

A

PIPE - OD 168.28 WITH 21.95 THK & STINFFENER WELDED (15 MM Thk FILLET WELD) AT 6 LOCATIONS, EQUISPACED

ON 3962 PCD

3500

3400

4500

4500

4750

4750

60

60

750

20

SECTION A-ASCALE 1 : 20

0.2 A

A

12 TYP

12TYP

6 TYP

5 7

6

8

9

250

0

40

40

130

0

NOTE: PART-8 TO BE MADE FROM MULTIPLE PLATE SEGMENTS1.

(PREFERABLY 2 NOS.) BY WELDING.2. PART-7 IS WELDED BETWEEN PART-6 BY BENDING INTO CIRCULAR ARC OF RADIUS 2000 MM. WELD SIZE IS 6 MM.

27.5°

45°

27.5°

45°

17.5

° 17.5°

57.

32.5° 32.5°

57.5°

21°

18°

21°

18°

21° 21°

R22

50

R1750

7.5° TYP

R50

(TYP

)

140

1

20

IV

III

II

I

40 THROUGH HOLES ON 4300 PCD - 12 NOS

40 THROUGH HOLES ON 3700 PCD - 12 NOS

40 THROUGH HOLES ON 4000 PCD - 12 NOS

125

TYP

130 TYP

4500

2500

45° TYP

IV

III

II

I

M36 TAPPED HOLES, THROUGH (12 NOS) AS SHOWN, 8 SETS EQUISPACED ON 3100 PCD

240

5

250

M125 TAPPED HOLE- 140 Lg.

M250 x4 THREAD- 270 Lg

350

PART-10 - 48 THK(SCALE 1:5)

M56 x 5.5 TAPPED HOLE,THROUGH -1 NO.

25 HOLES EQUISPACED ON 280 PCD, THROUGH - 8 NOS.

SIDE LOAD SIMULATION FRAME(SCALE 1:5)

15

16

1718

1920

11

12

13

14ENGINE SPACER FRAME

(SCALE 1:10)

738

90

150

50

700

26 HOLES EQUISPACED ON 600 PCD, THROUGH - 8 NOS.

PART-14 - 32 THK(SCALE 1:5)

II

III

IV

I

C

C

M24 TAPPEDHOLES EQUISPACED ON 600 PCD,

THROUGH - 8 NOS.

I

II

III

IV

350

20

508

80

70

SECTION C-CSCALE 1 : 5

190

340

PART-19 ( 25 THK)

50

282

1

50

150

50

250

310

M24 TAPPED HOLES EQUISPACED ON 200 PCD,

THROUGH - 7 NOS.

PART-17 ( 50 THK)

50

250

250

50

PART-9 ( 16 THK)

900

70

M64

x4.0

90

PART- 22(SCALE 1 :10)

2-412 -40 Lg

1 FIXED FRAME INTERFACE PLATE 1

2

3

4

5

6

7

8

INTERFACE FRAME AND LOAD TEST FIXTURES

1 : 20 IPRC-SIET-TMS-10/A1 11

3500

TOTAL WEIGHT : 15750 kg. (Approx)

REVISIONS SIGNZONE DATE

STIFFENER-750x525x20Thk

PIPE-O.D 168.28x21.95Thk750Lg

CALIBRATION INTERFACE PLATE

6

12

1

742

712

2800

ASTM A106GR.B

IS : 2062E250

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

XXS SCHEDULE

IS : 2062E250

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED5. CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHNING

IV

I III

II

PART-13(SCALE 1:5)

IS : 2062E250

SUPPORT PLATES - 6 Nos. IS : 2062E250 1 SET

PART-8(SCALE 1:20)

ISMC 400, 2500Long (BOX SECTION)

IS : 2062E250 6 1500

635

BASE PLATE-40Thk

IS : 4923Yst 310

IS : 2062E250

1

SUPPORT STOOL

PART-5(LOCATION DETAILS OF ISMC 400 WITH SUPPORT PLATES)

13

12

11

10

9

STIFFENER-738x90x16Thk

PIPE OD-508MMX50.1Thk -658MM Lg

TOP PLATE-80Thk

ASTM A 106

IS : 2062E250

IS : 2062E250

IS : 2062E250

8

1

1

1

1

15

14

BOTTOM PLATE-40Thk

BOTTOM PLATE-32Thk

IS : 2062E250

IS : 2062E250

1

1

17

16

FACING PLATE-50Thk

STIFFENER

IS : 2062E250

IS : 2062E250

1

8

PART- 21(SCALE 1 :10)

3400

35BLOCK PLATE-48Thk

110

360

SIDE PLATE18 IS : 2062E250 2

95

REFER IPRC/SIET/TMS-06/A1-PART2

REFER IPRC/SIET/TMS-06/A1-PART1

STIFFENER-250x250x16Thk

LOAD TEST TIEROD-1

PART-11 NOTE:ALL THE PARTS 15,16,18 &20 AND WELDING1.SCHEME IS IDENTICAL TO CALIBRATION SIDEFRAME(REFER IPRC/SIET/TMS-07 FORDETAILS). AFTER WELDING THE CENTREHEIGHT OF THE HYDRAULIC JACK WILL BE350 MM INSTEAD OF 605 MM.

SHS 200x200x6Thk-12500LONG

48 78

20

19

CLOSING PLATE

PLATE-340x190x25Thk

IS : 2062E250

IS : 2062E250

1

2

21 1IS : 2062E250 906

740

NOTE:PART-12 ISCOCENTICALLY WELDED WITH PART 14.1.WELD SIZE IS 15 MM.PART 11 IS WELDED ON THE TOP OF PART 12 ON2.THE PERIPHERY AS AN EDGE JOINT. WELD SIZE IS15 MM.PART-13 IS WELDED AS LENGTHWISE STIFFENER WITH3.PART 11 AND PART 12. WELD SIZE IS 6 MM.

IS : 2062E250 82

185REFER IPRC/SIET/TMS-07/A1-PART13 FOR COMPLETE DETAILS

441EN 24LOAD TEST TIEROD-222

A

B

C

D

E

REF. DRG. NO.

COM. FILE NO.

F

8 7 6 5

S.NO

< 0.025

1.6 - 8

0.025 - 1.6

ASK IF IN DOUBT

ALL DIMENSIONS ARE IN MILLIMETERS

UNLESS OTHERWISE SHOWN

DO NOT SCALE THE DRAWING

8 - 25

MACHINING FINISH IN MICRONS :-

CHAMFER 1 M.M. X 45°

REMOVE SHARP EDGES & BURRS

120-400 + 0°-10 4000 & ABOVE +3.0 _SIGN. DATE

LENGTH IN M.M. OFSHORTER SIDE OF

ANGLE UPTO & INCL.

DEVIATION FOR NON TOLERANCED DIMENSIONS

30-120 + 0°-20

1- 6 + 1°-00

6- 30 + 0°-30

DIAMETERS & LENGTHS

6 - 30 +0.2

120 - 315 +0.5 315 - 1000 +0.8 1000 - 2000 +1.2 2000 - 4000 +2.0

30 - 120 +0.3

UPTO & INCL.

(IS -2102)

6 +0.1

DESIGNED

SMP&ETFSDSC

DES.CHKD

APPROVED

DRG.CHKD_

_

_DRAWN,

,

,

,

REMARKS

PROJECTION

SHEETSCALE

OF

ISRO PROPULSION COMPLEXMAHENDRAGIRI

TITLE

DESCRIPTION QTYMATERIAL W.T(Kg)

A

B

C

4 3 2

D

E

1

F

28

29

30 262724

5

2

3

1

12

13

14

15

16

17

18

19

21

22

20

XX

9

11

5

30

23

3

10

12

SECTION X-XSCALE 1 : 15

1

2

3

4

5

6

8

10

12

13

14

16

17

18

19

20

21

22

23

24

26

25

27

28

30

29

15

LOAD TEST SETUP

1 : 15 IPRC-SIET-TMS-11/A1 11

REVISIONS SIGNZONE DATE

DISCUSSION / REVIEW

FABRICATION

TENDER PURPOSE

STATUS

NOTE:ALL CRITICAL WELDS ARE TO BE QUALIFIED WITH DP1.

TESTING / ULTRASONIC TESTING / RADIOGRAPHY2. ALL SHARP CORNERS ARE TO BE CHAFERED SUITABLY3. ALL WELDS ARE 6 mm UNLESS OTHERWISE SPECIFIED4. STRESS RELIEVING IS TO BE DONE FOR ALL THE PARTS WHEREVER HEAVY MACHNING /WELDING IS INVOLVED5. CHECK FOR THE STATUS OF DRAWING BEFORE FABRICATION / MACHNING

ONLY FOR REVIEW

------

EN24

------

EN24

IPRC-SIET-TMS-04

IPRC-SIET-TMS-05

IPRC-SIET-TMS-02

IPRC-SIET-TMS-10

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-07

IPRC-SIET-TMS-05

IPRC-SIET-TMS-07

IPRC-SIET-TMS-05

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-10

IPRC-SIET-TMS-09

IPRC-SIET-TMS-09

IPRC-SIET-TMS-03

44T CALIBRATION JACK WITH LOADCELL AND ADAPTOR

ENGINE SPACER FRAME

SLS SPACER PLATE

LOAD TEST TIE ROD-2

30

---

510

110

290

---

906

830

2865

1

1

1

1

1

1

1

1

E250

E250

E250/EN24

EN24

IS : 2062

IS : 2062

IS : 2062

1000T HYDRAULIC JACK

HYDRAULIC JACK ADAPTOR

SPHERICAL BEARING & BEARING HOUSING

IN-SITU CALIBRATION LINK

300T LOAD CELL

LOAD TEST TIE ROD

WORKING PLATFORM

CALIBRATION PLATE

21

22

23

24

25

26

27

28

29

E250

EN 24

IS : 2062E450

E250

E450IS : 2062

E450IS : 2062

IS : 2062E250

E250IS : 2062

IS 2062:E250,IS 2004:20C8,ASTM A106 GR.BIS 2062:E250,IS 2004:20C8,ASTM A106 GR.B

EN 24

EN 24

EN 24

EN 24

CONDITION-T

CONDITION-T

CALIBRATION FRAME

19

20

EN 24

IS : 2062

IS : 2062

CONDITION-T

8315

7050

886

360

150

20

18

10

36

162

305

40

7175

1

1

3

1

2

1

2

1

1

1

3

1

8

1

FIXED FRAME

THRUST FRAME

AXIAL LINK ASSEMBLY

INTERFACE FRAME

SIDE FRAME-1

SIDE FRAME-2

PITCH FORCE/YAW FORCE LINK

ROLL LINK ASSEMBLY

ATTACHMENT BLOCK

ATTACHMENT BLOCK TWIN EYE

LATERAL SAFETY STOPPER

SIDE FORCE CALIBRATION LINKASSEMBLY

ALIGNMENT JACKS

1550

18

17

16

15

14

13

12

11

10

9

8

7

6

5

4

3

2

1SPACER FRAME1

ATTACHMENT BLOCK-2

SIDE LOAD SIMULATION FRAME

SUPPORT STOOL

1ASTM A 106 IPRC-SIET-TMS-10650

EN24

EN24

EN24

IS : 2062E450

------

E250IS : 2062

IPRC-SIET-TMS-10

IPRC-SIET-TMS-07

IPRC-SIET-TMS-10

IPRC-SIET-TMS-10

IPRC-SIET-TMS-07

IPRC-SIET-TMS-1035

30

1

1

1

1

1

1

44

183

---

6300


Recommended