Redacted - RTL-001-CALC-ST-0101 Rev 0, RT-100 Weight and Center of Gravity Calculation. ·...

CALCULATION CONTROL SHEET

CALC. NO. RTL- 001-CALC-ST-0101

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Table of Contents

Calculation Cover Sheet ............................................................................................................................... 1 Calculation Revision Status Sheet ................................................................................................................ 2 Calculation Design Verification Plan and Summary Sheet ........................................................................... 3 Calculation Design Verification Checklist ...................................................................................................... 4 Table of Contents .......................................................................................................................................... 5 1.0 Purpose and Scope ........................................................................................................................... 6 2.0 Summary of Results and Conclusions .............................................................................................. 7 3.0 References ........................................................................................................................................ 9 4.0 Assumptions .................................................................................................................................... 10 5.0 Design Inputs .................................................................................................................................. 10 6.0 Methodology .................................................................................................................................... 10 7.0 Calculations ..................................................................................................................................... 11 Appendix A – Emails .................................................................................................................................. A1 Appendix B – ANSYS Output ..................................................................................................................... B1 Appendix C – ANSYS Input ....................................................................................................................... C1



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1.0 Purpose and Scope

Robatel Technologies is designing the RT-100 transport cask to transport radioactive waste in the form of dewatered resins and filters. The RT-100 transport cask is required to meet the requirements of 10CFR Part 71 (Ref. 3.1). The purpose of this calculation is to determine the detailed cask component and assembly weights and to derive the location of the center of gravity locations for the components and assemblies of the RT-100 transport cask. Weights and center of gravity locations will be determined for fully assembled unloaded and loaded conditions.

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2.0 Summary of Results and Conclusions

Table 2.1 gives the weights and center of gravity locations for the itemized components. Weightsand center of gravity locationswere determined using the ANSYS computer program (See AppendixB for output). The center of gravity locations are based on a coordinate system located at thebottom, center of the lower impact limiter, with (+y) as vertical up and (x) and (z) in perpendicularhorizontal directions. See Section 7.0 for example center of gravity location calculation.

Table 2.2 gives the weights and center of gravity locations for the itemized assemblies, including thefully assembled cask. Weightsand center of gravity locations for the assemblies and unloaded fullyassembled cask were determined using the ANSYS computer program (See AppendixB for output).The center of gravity location for the loaded, fully assembled cask is calculated in Section 7.0. Thecenter of gravity locations are based on a coordinate system located at the bottom, center of thelower impact limiter, with (+y) as vertical up and (x) and (z) in perpendicular horizontal directions.

Table 2.1 - Component Weights and Center of Gravity Locations

Proprietary Information

Table Withheld Under 10 CFR 2.390

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Typewritten Text



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Table 2.2 - Assembly Weights and Center of Gravity Locations

Assembly ANSYS Component

Name Weight

(kg) Center of Gravity,

y-dir (m) Center of Gravity,

x, z-dir (m)

Lower Impact Limiter BIL 2401 0.5161 0

Cask Body CASK 24472 1.4458 0

Primary Lid w/ bolts

PLID 3668 2.7161 0

Secondary Lid w/ bolts

SLID 865 2.7365 0

Upper Impact Limiter TIL 2458 2.8119 0

Total Assembly, empty

TOTAL 33864 1.6494 0

Total Assembly, with payload

N/A 40924 (1.6123, 1.6800)1 (+/-)0.02982

1) Determined using payload center of gravity at 10% of cask interior height

below or above the cask interior geometric centerline, respectively; see Section 7.0 for calculation

2) Determined using payload center of gravity at (+/-)10% of cask interior width away from the cask interior geometric centerline in horizontal directions; see Section 7.0 for calculation



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3.0 References

3.1 Nuclear Regulatory Commission, 10CFR Part 71, “Packaging and Transportation of Radioactive Material”

3.2 Drawings A. ROBATEL Industries Drawing RT100 PE 1001-1 Rev. D, “ROBATEL TRANSPORT PACKAGE RT100 GENERAL ASSY SHEET 1/2” B. ROBATEL Industries Drawing RT100 PE 1001-2 Rev. D, “ROBATEL TRANSPORT PACKAGE RT100 GENERAL ASSY SHEET 2/2” C. ROBATEL Industries Drawing 102885 PD 1012 Rev. B, “ROBATEL TRANSPORT PACKAGE RT100 S/E EMBALLAGE DETAILS COUVERCLE PRIMAIRE” D. ROBATEL Industries Drawing 102885 PD 1013 Rev. B, “ROBATEL TRANSPORT PACKAGE RT100 S/E EMBALLAGE DETAILS COUVERCLE SECONDAIRE” E. ROBATEL Industries Drawing 102885 PD 1031 Rev. B, “ROBATEL TRANSPORT PACKAGE RT100 S/E EMBALLAGE DETAILS CAPOT INFERIEUR” F. ROBATEL Industries Drawing 102885 PD 1032 Rev. B, “ROBATEL TRANSPORT PACKAGE RT100 S/E EMBALLAGE DETAILS CAPOT SUPERIEUR”

3.3 ANSYS – Mechanical, Version 14, ANSYS, Inc., Canonsbury, PA 15137 (See note) 3.4 NRC Memorandum “Summary of June 26-27, 2012, Meeting with ROBATEL Technologies,

LLC,” (Non-Proprietary Version), ADAMS Ascension No. ML12200A018 3.5 Fundamentals of Heat and Mass Transfer, Frank P. Incorpera, David P. DeWitt, 2002, 5th ed.,

John Wiley & Sons, Inc. 3.6 Design Guide, “LAST-A-FOAM FR-3700 Crash & Fire Protection of Radioactive Material

Shipping Containers,” dated 02/23/2012, General Plastic Manufacturing Company

Note: ANSYS is a commercially available computer software that is procured and maintained under the Enercon Services QA program.

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4.0 Assumptions

There are no unverified assumptions in this calculation. Other design assumptions used, ifany, willbe noted and referenced as needed in the body of the calculation.

5.0 Design Inputs

5.1

52 Proprietary InformationText Withheld Under 10 CFR 2.390

6.0 Methodology

The RT-100 transport cask will be a safety-related structure in accordance with 10CFR Part 71(Ref. 3.1). The cask consists of a stainless steel containment structure with a lead shielding panelbetween the inner and outer cask wall, ductile stainless steel and foam upper and lower impactlimiters, a pair of concentric, removable stainless steel cask lids, a pair of removable stainless steellifting pockets on opposite sides of the cask body and a pair of stainless steel tie-down arms onopposite sides of the cask body (Ref. 3.2).

Components of the RT-100 cask will be created in the ANSYS computer program. (Ref. 3.3).Geometric features and material types of all components will be confirmed against the drawings(Ref. 3.2). However, for simplification of the model, intricate cask details such as chamfered edgeswere not modeled. This leads to a maximum of 5% difference in weight between the model and thedrawings. This has an insignificant effect on the center of gravity locations for the fully assembledunloaded and loaded cask and is therefore acceptable.

The ANSYS command VSUM will be used to obtain the weight and center of gravity locations of thecomponents and assemblies. However, weights calculated in the ANSYS computer program aredoubled as only half of the cask is modeled (see Appendix Bfor cask image).

The center of gravity locations are based on a coordinate system located at the bottom, center ofthe lower impact limiter, with (+y)as vertical up and (x) and (z) in perpendicular horizontal directions.In order to determine the center of gravity locations for components and assemblies based on thebottom, center of the lower impact limiter, the ANSYS coordinate system must be adjusted in thevertical direction (see Section 7.0 for example calculation).

A maximum payload of 7,060 kg will be applied to the fully assembled cask in order to determine theweightand center of gravity locations for the loaded, fully assembled cask (see Section 7.0). PerReference 3.4, the caskucontents shallbe placedsuch that the CG of thepackage is atapproximately the same location as the geometric centerof thepackage - approximately the samelocation being definedas havinga ±10% difference in distance of the cavityinside dimensions fromthegeometric centerof thepackageinanydirection" All other horizontal center of gravity locationsare assumed to be located at the geometric center of components and assemblies.



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7.0 Calculations

Adjusting ANSYS Coordinate System ycg = distance from base of lower impact limiter to ANSYS coordinate system (+) component/assembly

center of gravity based on ANSYS coordinate system Example (center of gravity location of component BIL_FR3705): ycg = 0.497 + (-)0.318 = 0.179m Center of Gravity Locations of Payload The payload center of gravity located at 10% of the cask interior height below the cask interior geometric centerline was determined as follows: ycg = distance from base of lower impact limiter to base of cask interior (+) distance to center of cask

interior (–)10% of the cask interior height

The payload center of gravity located at 10% of the cask interior height above the cask interior geometric centerline was determined as follows: ycg = distance from base of lower impact limiter to base of cask interior (+) distance to center of cask

interior (+)10% of the cask interior height

The payload center of gravity located at (+/-)10% of the cask interior width away from the cask interior geometric centerline was determined as follows: xcg = zcg = (+/-)10% of the cask interior width xcg = zcg = +/- (1.730 x 0.1) = +/- 0.1730m Center of Gravity Locations of Total Assembly with Payload The center of gravity for the loaded total assembly, using a payload center of gravity 10% of cask interior height below the cask interior geometric centerline, was determined using the following equation:

Where: ycg = distance to center of gravity in y-direction (m) mi = weight of each assembly (kg) yi = center of gravity of each assembly in the y-direction (m)

M = total mass (kg)

mM

ymy

N

iii

cg 6123.140924

)4344.17060()6494.133864(1

mycg 4344.1)1.0956.1(2

956.1652.0

mycg 8256.1)1.0956.1(2

956.1652.0



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The center of gravity for the loaded total assembly, using a payload center of gravity 10% of cask interior height above the cask interior geometric centerline, was determined using the following equation:

Where: ycg = distance to center of gravity in y-direction (m) mi = weight of each assembly (kg) yi = center of gravity of each assembly in the y-direction (m)

M = total mass (kg) The center of gravity for the loaded total assembly, using a payload center of gravity (+/-)10% of cask interior width away from the cask interior geometric centerline in the horizontal directions, was determined using the following equation:

Where: xcg, zcg = distance to center of gravity in perpendicular, horizontal directions (m) mi = weight of each assembly (kg) xi, zi = center of gravity of each assembly in perpendicular, horizontal directions (m)

M = total mass (kg)

Table 7.1 - Weights and Center of Gravity Locations

Assembly ANSYS Component

Name Weight

(kg) Center of Gravity,

y-dir (m) Center of Gravity,

x, z-dir (m)

Payload N/A 70601 (1.4334, 1.8256)2 (+/-)0.17303

Total Assembly, empty

TOTAL 33863 1.6494 0

Total Assembly, with payload

N/A 40634 1.6123, 1.6800 (+/-)0.0298

1) See Section 5.0 for payload weight determination 2) Payload center of gravity is 10% of cask interior height below or above the

cask interior geometric centerline, respectively 3) Payload center of gravity is (+/-)10% of cask interior width away from the

cask interior geometric centerline in horizontal directions

mM

ymy

N

iii

cg 6800.140924

)8256.17060()6494.133864(1

mM

zm

M

xmzx

N

iii

N

iii

cgcg 0298.040924

)1730.07060()033864(11


Appendix A


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Appendix A

Emails


Appendix A


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Appendix B


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Appendix B

ANSYS Output

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Appendix B

Total Cask Assembly


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Proprietary Information

Figure Withheld Under 10 CFR 2.390

CXA5

Typewritten Text


Appendix B


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Lower Impact Limiter (BIL) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 38 (OUT OF 3216 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 1.5368 TOTAL MASS = 1200.5 CENTER OF MASS: XC= 0.0000 YC= 0.19063E-01 ZC=-0.63643 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 730.14 243.45 243.45 IYY = 1281.5 795.22 798.45 IZZ = 730.14 729.70 726.47 IXY = -0.77875E-05 -0.85465E-05 IYZ = 29.470 14.906 IZX = -0.30730E-04 -0.53908E-05 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 0.977 0.212 0.000 -0.212 0.977 (THXY= 0.000 THYZ= 12.233 THZX= 0.000)


Appendix B


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Foam FR3705, Lower Impact Limiter (BIL_FR3705) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 2 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.24895 TOTAL MASS = 19.916 CENTER OF MASS: XC= 0.0000 YC=-0.31800 ZC=-0.76220 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 16.521 2.9369 2.9369 IYY = 28.607 17.037 17.037 IZZ = 16.521 14.507 14.507 IXY = 0.22284E-09 -0.23130E-12 IYZ = -4.8271 -0.59801E-23 IZX = 0.23553E-09 -0.29913E-09 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 1.000 0.000 0.000 0.000 1.000 (THXY= 0.000 THYZ= 0.000 THZX= 0.000)


Appendix B


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Foam FR3720, Lower Impact Limiter (BIL_FR3720) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 2 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.40862 TOTAL MASS = 130.76 CENTER OF MASS: XC= 0.0000 YC=-0.30927 ZC=-0.57665 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 68.460 12.472 12.472 IYY = 109.26 65.781 65.784 IZZ = 68.460 55.953 55.950 IXY = -0.66402E-08 0.28472E-08 IYZ = -23.481 -0.16147 IZX = -0.95710E-08 0.81187E-08 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 1.000 -0.016 0.000 0.016 1.000 (THXY= 0.000 THYZ= -0.941 THZX= 0.000)


Appendix B


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Foam FR3740, Lower Impact Limiter (BIL_FR3740) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 8 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.81229 TOTAL MASS = 520.68 CENTER OF MASS: XC= 0.0000 YC= 0.10532 ZC=-0.66025 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 321.78 89.023 89.023 IYY = 593.63 366.65 367.81 IZZ = 321.78 316.01 314.85 IXY = 0.19873E-07 -0.25629E-07 IYZ = 43.954 7.7456 IZX = 0.30296E-06 0.58820E-06 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 0.989 0.148 0.000 -0.148 0.989 (THXY= 0.000 THYZ= 8.504 THZX= 0.000)


Appendix B


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Cask Body (CASK) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 1960 (OUT OF 3216 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 1.2874 TOTAL MASS = 12236. CENTER OF MASS: XC=-0.43398E-01 YC= 0.94875 ZC=-0.55080 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 21293. 6567.4 6598.6 IYY = 10181. 6445.6 6391.7 IZZ = 21889. 10852. 10875. IXY = 580.67 76.868 IYZ = 6708.9 314.71 IZX = -259.86 32.621 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 0.921 0.389 -0.036 -0.390 0.919 -0.062 0.009 0.071 0.997 (THXY= 23.031 THYZ= -3.552 THZX= 2.057)


Appendix B


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Lead, Cask Body (CASK_PB) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 190 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.63505 TOTAL MASS = 7201.4 CENTER OF MASS: XC= 0.0000 YC= 0.90160 ZC=-0.56628 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 11772. 3609.2 3609.2 IYY = 5857.5 3548.2 3532.3 IZZ = 11772. 5918.5 5934.4 IXY = 0.13098E-02 -0.78857E-03 IYZ = 3871.8 195.07 IZX = -0.11225E-02 0.19545E-03 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 0.997 -0.081 0.000 0.081 0.997 (THXY= -0.001 THYZ= -4.673 THZX= 0.000)


Appendix B


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Primary Lid (PLID) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 832 (OUT OF 3216 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.23213 TOTAL MASS = 1833.8 CENTER OF MASS: XC= 0.0000 YC= 2.2191 ZC=-0.45964 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 9537.6 119.69 119.69 IYY = 1001.7 614.23 614.32 IZZ = 9537.6 507.12 507.02 IXY = -0.46055E-02 0.34533E-03 IYZ = 1873.7 3.1763 IZX = 0.64747E-03 -0.37800E-03 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 1.000 0.030 0.000 -0.030 1.000 (THXY= 0.000 THYZ= 1.697 THZX= 0.000)


Appendix B


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Secondary Lid (SLID) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 346 (OUT OF 3216 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.49659E-01 TOTAL MASS = 432.25 CENTER OF MASS: XC= 0.0000 YC= 2.2395 ZC=-0.18504 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 2189.9 7.1909 7.1909 IYY = 41.975 27.174 27.213 IZZ = 2189.9 21.993 21.954 IXY = 0.61977E-04 0.46561E-05 IYZ = 179.58 0.45042 IZX = 0.25711E-04 0.30447E-04 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 0.996 0.086 0.000 -0.086 0.996 (THXY= 0.000 THYZ= 4.932 THZX= 0.000)


Appendix B


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Lead, Secondary Lid (SLID_PB) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 2 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.11612E-01 TOTAL MASS = 131.68 CENTER OF MASS: XC= 0.0000 YC= 2.1888 ZC=-0.14898 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 634.98 1.1732 1.1732 IYY = 8.1125 5.1899 5.1899 IZZ = 634.98 4.0957 4.0957 IXY = 0.76308E-03 0.38647E-05 IYZ = 42.940 0.24442E-05 IZX = -0.44472E-04 0.72025E-05 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 1.000 0.000 0.000 0.000 1.000 (THXY= 0.000 THYZ= 0.000 THZX= 0.000)


Appendix B


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Upper Impact Limiter (TIL) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 40 (OUT OF 3216 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 1.5405 TOTAL MASS = 1229.1 CENTER OF MASS: XC= 0.0000 YC= 2.3149 ZC=-0.62912 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 7328.0 254.76 254.76 IYY = 1289.7 803.26 808.84 IZZ = 7328.0 741.23 735.65 IXY = 0.31099E-02 0.62222E-05 IYZ = 1770.6 -19.422 IZX = -0.81071E-03 0.32755E-04 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 0.961 -0.276 0.000 0.276 0.961 (THXY= 0.000 THYZ= -16.026 THZX= 0.000)


Appendix B


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Foam FR3705, Upper Impact Limiter (TIL_FR3705) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 2 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.24896 TOTAL MASS = 19.916 CENTER OF MASS: XC= 0.0000 YC= 2.6400 ZC=-0.76221 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 153.32 2.9371 2.9371 IYY = 28.609 17.038 17.038 IZZ = 153.32 14.508 14.508 IXY = -0.17028E-04 0.20528E-11 IYZ = 40.077 0.87326E-18 IZX = 0.30871E-08 -0.49132E-05 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 1.000 0.000 0.000 0.000 1.000 (THXY= 0.000 THYZ= 0.000 THZX= 0.000)


Appendix B


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Foam FR3720, Upper Impact Limiter (TIL_FR3720) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 2 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.40864 TOTAL MASS = 130.77 CENTER OF MASS: XC= 0.0000 YC= 2.6313 ZC=-0.57666 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 961.33 12.473 12.473 IYY = 109.27 65.787 65.790 IZZ = 961.33 55.958 55.955 IXY = 0.50065E-04 -0.74037E-06 IYZ = 198.58 0.16148 IZX = 0.61166E-06 0.11746E-04 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 1.000 0.016 0.000 -0.016 1.000 (THXY= 0.000 THYZ= 0.941 THZX= 0.000)


Appendix B


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Foam FR3740, Upper Impact Limiter (TIL_FR3740) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 8 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 0.81232 TOTAL MASS = 520.70 CENTER OF MASS: XC= 0.0000 YC= 2.2167 ZC=-0.66027 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 2874.6 89.028 89.028 IYY = 593.68 366.68 367.84 IZZ = 2874.6 316.03 314.87 IXY = 0.63606E-03 -0.83709E-04 IYZ = 754.35 -7.7462 IZX = 0.14628E-05 0.21586E-03 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.000 0.000 0.000 0.989 -0.148 0.000 0.148 0.989 (THXY= 0.000 THYZ= -8.504 THZX= 0.000)


Appendix B


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Total Assembly, Empty (TOTAL) PRINT MASS PROPERTIES ASSOCIATED WITH THE CURRENTLY SELECTED VOLUMES TOTAL NUMBER OF VOLUMES SELECTED = 3208 (OUT OF 3208 DEFINED) *********************************************** SUMMATION OF ALL SELECTED VOLUMES TOTAL VOLUME = 4.6349 TOTAL MASS = 16787. CENTER OF MASS: XC= 0.99687E-03 YC= 1.1577 ZC=-0.55168 *** MOMENTS OF INERTIA *** ABOUT ORIGIN ABOUT CENTER OF MASS PRINCIPAL IXX = 41169. 13559. 13560. IYY = 13558. 8448.7 8448.3 IZZ = 41344. 18844. 18844. IXY = 9.2990 28.673 IYZ = 10676. -45.766 IZX = 11.088 1.8561 PRINCIPAL ORIENTATION VECTORS (X,Y,Z): 1.000 0.006 0.000 -0.006 1.000 0.004 0.000 -0.004 1.000 (THXY= 0.322 THYZ= 0.252 THZX= 0.017)


Appendix B


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Appendix C

ANSYS Input


Appendix B


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The following ANSYS files are used in this calculation: Volume in drive M has no label. Volume Serial Number is 164B-772E Directory of M:\Projects\ROBATEL\ROBATEL002 - RT-100 Calculations\3.0 Calculations\Civil\ST0101 Wgt n CG RT100\ANSYSFILES 08/28/2012 01:26 PM <DIR> . 08/28/2012 01:26 PM <DIR> .. 08/28/2012 01:21 PM <DIR> Archives 08/28/2012 01:24 PM <DIR> Backup 08/28/2012 08:18 AM 988 BIL.txt 08/28/2012 08:18 AM 988 BIL_FR3705.txt 08/28/2012 08:18 AM 988 BIL_FR3720.txt 08/28/2012 08:18 AM 988 BIL_FR3740.txt 08/28/2012 08:18 AM 988 CASK.txt 08/28/2012 08:18 AM 988 CASK_PB.txt 08/28/2012 01:26 PM 0 filelist.txt 08/28/2012 08:18 AM 988 PLID.txt 08/28/2012 08:18 AM 988 SLID.txt 08/28/2012 08:18 AM 988 SLID_PB.txt 08/28/2012 08:18 AM 988 TIL.txt 08/28/2012 08:18 AM 988 TIL_FR3705.txt 08/28/2012 08:18 AM 988 TIL_FR3720.txt 08/28/2012 08:18 AM 988 TIL_FR3740.txt 08/28/2012 08:18 AM 988 TOTAL.OUT 08/28/2012 09:03 AM 117,637,120 WGTCG.db 08/28/2012 08:18 AM 117,571,584 WGTCG.dbb 08/28/2012 09:03 AM 956 WGTCG.err 08/26/2012 02:16 PM 2,214 WGTCG.inp 08/28/2012 09:03 AM 2,682 WGTCG.log 08/28/2012 08:13 AM 51,519 WGTCG000.png 08/28/2012 08:14 AM 51,515 WGTCG001.png 22 File(s) 235,331,422 bytes 4 Dir(s) 1,622,861,828,096 bytes free These files are archived in the ENERCON project files and provided to the client in electronic format.

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Redacted - RTL-001-CALC-ST-0101 Rev 0, RT-100 Weight and Center of Gravity Calculation. ·...

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