Zaporozhye - 2020
ENGINESENGINESOF THE THIRD MILLENNIUMOF THE THIRD MILLENNIUM
ENGINESENGINESOF THE THIRD MILLENNIUMOF THE THIRD MILLENNIUM
ZAPOROZHYEZAPOROZHYE
MACHINE-BUILDING DESIGN BUREAU PROGRESS STATE ENTERPRISEMACHINE-BUILDING DESIGN BUREAU PROGRESS STATE ENTERPRISE
NAMED AFTER ACADEMICIAN A.G. IVCHENKONAMED AFTER ACADEMICIAN A.G. IVCHENKO
ZAPOROZHYE
MACHINE-BUILDING DESIGN BUREAU PROGRESS STATE ENTERPRISE
NAMED AFTER ACADEMICIAN A.G. IVCHENKO
Ukrainian Defence Industry
®
®
Ukrainian Defence Industry
Foundation date: May 5, 1945
ZAPOROZHYE MACHINE-BUILDING DESIGN
BUREAU PROGRESS STATE ENTERPRISE
NAMED AFTER ACADEMICIAN A.G. IVCHENKO
(IVCHENKO-PROGRESS SE)
FORM OF PROPERTY: - IVCHENKO-PROGRESS SE integrated in the State Concern «UKROBORONPROM»
SPHERE OF ACTIVITIES: - design, manufacture, certification, putting into series production, overhaul, test of aircraft and industrial gas turbine engines
CO-OPERATION: - more than 230 associated enterprises and suppliers
QUANTITYPRODUCTION: - Motor Sich JSC, Zaporozhye, Ukraine - Povazske Strojarne JSC, Povazska Bystrica, Slovak Republic
OPERATION: - 64 types of aircraft powered by engines and APUs of IVCHENKO-PROGRESS SE design are operated in more than 100 countries. - More than 80 thousand piston and gas turbine engines have been manufactured by series production plants. - Total operating time of the gas turbine engines in service is over 300 million hours.
HISTORY
c IVCHENKO-PROGRESS SE, 2020c
2
THE BASIC SPHERES OF ACTIVITIES
DESIGN MANUFACTURE
TEST, DEVELOPMENT AND CERTIFICATIONPUTTING IN SERIES PRODUCTION AND IMPROVEMENT
OF CONSUMER'S CHARACTERISTICS
OVERHAUL
®
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IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
RECOGNITION
OF CERTIFICATION AUTHORITIES
®
State aviation administrationof Ukraine
Certificates No. UA.21J.0004, No. UA.145.0073,No. and others
UKRAINE
Interstate Aviation CommitteeAviation Register (ARMAK)
Certificates No. СПР-15, No. R-69and others
Bureau Veritas (France)
Certificates DSTY ISO 9001:2015, ISO 9001:2015 No. UА228430,BS EN 9001:2015, EN 9100:2016 No. UK 562016-01
European Aviation Safety Agency (Germany)
Certificate No. 216/2008,No. 1702/2003 Part 21A.23(b)2
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IVCHENKO-PROGRESS SE, 2020
1 8 2 8
BUREAU VERITASCertification
UA
ER
UB
V ERI T
AS
АРСД ТУ ВС ЕНОГ НЫЖЕ Й
М
ИОЦ ННА ЫИВ Й
А
ИТМ ЕО ТК
IN ET EE TIRS MT MA OTE C A NV IOIAT
MORE THAN 60 CERTIFICATES OF VARIOUS TYPES
Ukrainian Defence Industry
®
TECHNICAL PRIORITIES
АI-20АI-25
D-36The 1- st in the USSR bypass engine
for regional aircraft, m›1The 1- st in the USSR three-shaft turbofan engine
with high bypass ratio for short-haul aircraft
The 1- st in the USSR turboprop engine with longservice life achived (over 20 000 hours)
D-18ТD-136
D-27Тhe most powerful in the world turboshaft engine
for heavy-lift helicoptersThe world first series-producen propfan
engine for medium tactical transport aircraft
The 1- st in the USSR turbofan with a thrustexceeding 20 tons for long-haul heavy transports
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IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
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Ukrainian Defence Industry
PISTON AND TURBOSHAFT ENGINES FOR LIGHTHELICOPTERS AND ULTRAHEAVY MILITARY
TRANSPORT HELICOPTERS
* - year of project launch- series production- manufacture, testing, final development, certification- design
Мi-1
Ка-15
Ка-18
Ка-26
G-4
B-5
B-10,-11
Мi-26Т
Мi-26
D-136 1971*
Yak-100
Ка-226
AI-450 1994*
АI-26/GR/GRF 1945*
АI-14V 1951*
AI-450M/M1 2006*
Мi-26/26Т
AI-136T2010*
Helicoptersof take off weight
up to 15 t.
TV3-117VMA-SBM1Vseries 5 (AI-130)
АI-450-2 2016*
Helicoptersof take offweight up
to 4 t.
Heavy-lifthelicopters
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IVCHENKO-PROGRESS SE, 2020
2013*
AI-136T-22013*
MSB-2 «Nadiya»
Mi-2М
Mi MSB-2
®
Аn-12
Аn-10
IL-18
IL-20, IL-22
IL-38
Аn-24
Аn-26
Аn-30
АI-20АSeries 1, 2, 3, 4,AI-20M Series 6
1955*
AI-24 Series 2, AI-24T, AI-24VT
1957*
Аn-70
Аn-140
D-27
1985*
TV3-117VMA-SBM1,TV3-117VMA-SBM1I
1996*
АI-450С-2
2010*
TURBOPROP ENGINES FOR REGIONALAND MILITARY TRANSPORT AIRCRAFT,SPECIAL PURPOSE AIRCRAFT AND GA
* - year of project launch- series production- manufacture, testing, final development, certification- design
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IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
UAV «AKINCI»
AI-450С
2011*
DA50-JP7
For GAaircraft type
DART-450
AI-450СP
2014*
UTL-450
AI-450CP-2
2016*
TA-20
®
Yak-40
М-15
АI-25series 2, 2M
1962*
D-18Tseries 1, 3
1972* D-36 series 1, 1А, 2А, 3А, 4А
1967*
D-18T series 3M
2012*
Аn-124,Аn-124-100М-150
Аn-225
Аn-72
Yak-42
Аn-74
Аn-74ТК-300
Аn-124-100
Тu-334
Bе-200ChS
D-436Т1, D-436ТР
1991*
TURBOFAN ENGINES FOR REGIONAL,MILITARY TRANSPORT ANDMULTIPURPOSE AIRCRAFT
D-436-148FM2013*
An-148, -158
Аn-178
Аn-148, -158, -178
AI-282015*
D-436-1482002*
* - year of project launch- series production- manufacture, testing, final development, certification- design
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L-39
Yak-130
АI-25ТL,АI-25ТLK,АI-25ТLSh 1980*
1998*DV-2
AI-222-25,АI-322
1948*1970*
2005*
АI-322F
АI-14
Yak-18
Yak-12
PISTON, TURBOFAN ENGINES, INCLUDINGENGINES WITH AFTERBURNER, FORTRAINERS AND COMBAT TRAINERS
L-15A
* - year of project launch- series production- manufacture, testing, final development, certification- design
L-59(39MS)
Yak-130D
L-15B
L-39М1
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Ukrainian Defence Industry
2014*
АI-322-30
2016*
АI-322-30F
For light combat aircraft
For light trainingaircraft and lightcombat aircraft
JL-8 (K-8W)
®
АI-8
Аn-8
Аn-10
Bе-12
Мi-6
АI-9
Mi-14
Mi-24
Yak-40
М-15
АI-9V,AI-9V series 1,
AI-9V-1
Мi-171
Мi-28
Мi-24 (Мi-35)
Мi-8МТV
Аn-140
АI9-3B
Аn-148
АI-450МS*
AUXILIARY POWER UNIT (APU)
1957*1964*
1971*
1994*
2002*
* - year of project launch- series production- manufacture, testing, final development, certification- design
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IVCHENKO-PROGRESS SE, 2020
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OUR ENGINES ARE OPERATEDIN MORE THAN 100 COUNTRIES OF THE WORLD
®АI-20А series 1, 2, 3, 4, AI-20К series 5, AI-20М series 6
IL-18
АI-20А, AI-20К series 5,AI-20М series 6
Аn-10
АI-20А, AI-20К series 5
IL-22
АI-20М series 6
IL-38
АI-20А, АI-20К series 5, АI-20М series 6I
Output shaft power, ehp ........ 4,000 ............ 4,250Equivalent specific fuel
, kg/h/ehp .......... 0.270 ............ 0.239consumption
АI-20K АI-20М
Takeoff, (S/L static; ISA)
Аn-12
АI-20К series 5, AI-20М series 6
IL-20
АI-20К series 5
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Ukrainian Defence Industry
®
Аn-32
Bе-12
АI-20D series 4, 5, 5Е
АI-20D series 4
АI-20D series 5, 5Е
Output shaft power, ehp ................................... 5,180 ..................... 5,180Equivalent specific fuel
, kg/h/ehp ..................................... 0.227 ..................... 0.227consumption
АI-20D
series 5, 5E
АI-20D
s eries 4 Takeoff, (S/L static; ISA)
Аn-8
АI-20D series 4
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Ukrainian Defence Industry
®
Аn-24
AI-24 series 2, AI-24T, AI-24VT
Аn-26
Аn-30
AI-24 series 2, AI-24T
AI-24VT
AI-24VT
Output shaft power, ehp ..................... 2,550 ................. 2,820 ............... 2,820Equivalent specific fuel
, kg/h/ehp ....................... 0.255 ................. 0.255 ............... 0.255consumption
Takeoff, (S/L static; ISA)
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АI-24TАI-24VTАI-24 series 2
IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
®
АI-25 series 2, 2M
Thrust, kgf ............................................ 1,500, kg/h/kgf ........ 0.56Specific fuel consumption
АI-25
Takeoff, (S/L static; ISA)
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Yak-40М-15
АI-25 series 2М АI-25 series 2
IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
®
L-39
JL-8 (K-8W)
АI-25ТL, АI-25ТLК, АI-25ТLSh
АI-25ТL
АI-25ТLК
АI-25ТLSh
L-39M1
Thrust, kgf ........................................... 1,720 ....................... 1,720 .............................. 1,850, kg/h/kgf ....... 0.58 ......................... 0.58 .................................. 0.6Specific fuel consumption
АI-25TL АI-25TLK АI-25TLSh
Takeoff, (S/L static; ISA)
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Аn-72
Yak-42D
D-36 series 1, 1А, 2А, 3А, 4А
D-36 series 1
D-36 series 1А
Аn-74
D-36 series 2А, 3АThrust, kgf .......................................... 6,500 ............... 6,500S , kg/h/kgf .... 0.365 ............... 0.358pecific fuel consumption
Takeoff, (S/L static; ISA), uninstalled
Аn-74ТК-300
D-36 series 4A
Thrust, kgf .......................................... 1,600 ............... 1,600 , kg/h/kgf ...... 0.65 ................. 0.63Specific fuel consumption
Max cruise, (H = 8 000 m, M = 0.75; ISA)
D-36
series 1, 1A, 2A, 3A
D-36
series 4A
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®
Takeoff, (S/L static; ISA), uninstalled
Аn-225 «Mriya»
D-18Т series 1, 3, 3M
D-18Т series 1
D-18Т series 1, 3, 3M
D-18T series 1, 3, 3M
Max cruise, (H = 11 000 m, M = 0.75; ISA)
Аn-124, Аn-124-100
Thrust, kgf ..................................................................... 23 430,S , kg/h/kgf ..................... 0.345...0.362pecific fuel consumption
Thrust, kgf........................................................................ 4,860, kg/h/kgf ................................. 0.546Specific fuel consumption
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Ukrainian Defence Industry
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D-136, D-136 series 1, AI-136T/T-2
Shaft power, hp .................................... 11,400 ........................ 12,200, kg/h/hp ........ 0.198 ................ 0.198/0.210Specific fuel consumption
D-136,
D-136 series 1
Max takeoff, (S/L static; ISA)
AI-136T/T-2
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Мi-26/26T Heavy-lift helicopters
®
DV-2
L-59
21
Thrust, kgf ................................................... 2 200,, kg/h/kgf ............. 0.595Specific fuel consumption
DV-2
Takeoff, (S/L static; ISA)
IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
®
D-436Т1, D-436ТР, D-436-148
Тu-334-100
D-436Т1
Аn-148
D-436-148B
Bе-200ChS
D-436ТР
Аn-158
D-436-148 D-436-148D
22
Takeoff, (S/L static; ISA), uninstalled
D-436T1 D-436TP D-436-148B D-436-148D
Max cruise, (H = 11 000 m, M = 0.75; ISA)
Thrust, kgf ....................... 7,500 .............. 7,500 ..................... 6,570 ..................... 7 000,Specific fuel
, kg/h/kgf ....... 0.37 ................ 0.37 ..................... 0.351 ..................... 0.351consumption
Thrust, kgf ....................... 1,670 .............. 1,500 ..................... 1,560 ..................... 1,560Specific fuel
, kg/h/kgf ....... 0.61 ................ 0.61 ......................... 0.6 ......................... 0.6consumption
IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
®TV3-117VМА-SBМ1
Аn-140
23
TV3-117VMA-SBM1
Takeoff, (S/L static; ISA)
Max cruise, (H = 6 000 m, M = 0.5; ISA)Output shaft power, ehp .......................................................... 1,750E , kg/h/ehp ....................... 0.193quivalent specific fuel consumption
Output shaft power, ehp .......................................................... 2,500E , kg/h/ehp ....................... 0.206quivalent specific fuel consumption
IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
®D-27
Аn-70
24
Output shaft power, ehp ............................................... 13,240E , kg/h/ehp .............. 0.180quivalent specific fuel consumption
D-27
oTakeoff, (S/L; t = t + 15 C, P = 730 mm Hg)amb ISA amb
IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
®
AI-322
АI-322
Takeoff, (S/L static; ISA)
Thrust, kgf ........................................................ 2,500S , kg/h/kgf .................... 0.64pecific fuel consumption
L-15A
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Ukrainian Defence Industry
Мi-2М
MSB-2 «Nadiya»
AI-450M (M1, M-P, M1-P)
АI-450М (M1, М-P, М1-P)
Takeoff, (S/L static; ISA)Power, hp ............................................. 400 .................. 465S , kg/h/hp .... 0.280 ............... 0.270pecific fuel consumption
AI-450M(M1, M2)
AI-450M-P(M1-P, M2-P)
Mi-2MSB
®
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UAV «AKINCI»
АI-450С (CM, СD, СР)
АI-450C
(CM, СD, СР)
DA50-JP7
DART-450 UTL-450
Propeller shaft power, hp .......................... 400...495S , kg/h/hp ................. 0.277pecific fuel consumption
Takeoff, (S/L static; ISA)
®
Helicopters with takeoff
weight of 3,000...3,300 kg
Power, hp ................................................ 630...800S , kg/h/hp ....... 0.270...260pecific fuel consumption
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Ukrainian Defence Industry
АI-450-2, AI-450С-2 (СР-2)
AI-450-2
АI-450-2 АI-450С-2 (CP-2)
AI-450C-2 (CP-2)
Propeller shaft power, hp ........................... 630...800S , kg/h/hp ......... 0.270...260pecific fuel consumption
Takeoff, (S/L static; ISA)
For UAVs typeFor GA aircraft type
TA-20
Takeoff, (S/L static; ISA)
®TV3-117VМА-SBМ1V series 5, TV3-117VМА-SBМ2, АI-130
ТV3-117VМА-SBМ1V series 5 Мi-8MSB
ТV3-117VМА-SBМ2
Аn-140Т
ТV3-117VМА-SBМ2
ТV3-117VМА-SBМ1V series 5, АI-130
Medium transporthelicopter
Max emergency,(H = 6 000 m, M = 0.5; ISA)Free turbine shaft power, hp .............................. 2,000S , kg/h/hp .................... 0.193pecific fuel consumption
Max emergency, (S/L static; ISA)Power, hp .......................................................... 3,200
Takeoff, (S/L static; ISA)Propeller shaft power, hp .................................... 2,800S , kg/h/hp ..................... 0.210pecific fuel consumption
Max emergency,(H = 6 000 m, M = 0.5; ISA)Propeller shaft power, hp .................................... 2,000S , kg/h/hp ..................... 0.193pecific fuel consumption
Max emergency, (S/L static; ISA)Propeller shaft power, hp ................................... 3,200
30
Takeoff, (S/L static; ISA)Power, hp .......................................................... 2,800S , kg/h/hp .................... 0.212pecific fuel consumption
IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
Мi-17
АI-130
AI-322-40
AI-322-40AI-322-30
AI-322-30
®
AI-322-30, AI-322-40
Light trainers and combat aircraftRegional passenger,
business aircraft
Takeoff, (S/L static; ISA)Thrust, kgf ................... 3,000 ............ 3,755Specific fuel
, kg/h/kgf ..... 0.7 ............ 0.381consumption
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®AI-322F, AI-322-30F
АI-322F
АI-322F
Light combat aircraft
Takeoff,(S/L static; ISA)
Takeoff,(S/L static; ISA)
Fullaugmented
power
Fullaugmented
power
AI-322-30F
Thrust, kgf ................... 2,920 ............... 4,900Specific fuel
, kg/h/kgf ... 0.71 ................. 1.92consumption
Thrust, kgf ................... 2,500 ............... 4,200Specific fuel
, kg/h/kgf ... 0.64 ................... 1.9consumption
AI-322-30F
L-15B
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D-436-148FM
Takeoff / Emergency, (S/L static; ISA)
An-178
D-436-148FM
Max cruise,(H = 11 000 m, M = 0.75; ISA)
Thrust, kgf ......................................... 7,880 / 8,800S , kg/h/kgf ............... 0.371pecific fuel consumption
Trhust, kgf...................................................... 1,700S , kg/h/kgf ............... 0.605pecific fuel consumption
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Аn-148, Аn-158 modifications
The engine is designed forinstallation on regional passenger
and medium transport aircraft
®
®
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SHORT-LIFE TURBOJET ENGINE AI-350
Maximum power rating, (S/L static; ISA; s =1.0)in
Thrust, daN ............................................................................. 350
Specific fuel consumption, kg/(daN·h) .........................................1.16
(Н = 5 000 m; М = 0.8; ISА; s = 1.0)F F in
Thrust, daN ............................................................................. 385
Specific fuel consumption, kg/(daN·h) .........................................1.50
Parameters are presented at the maximum electric power takeoff from the built-in alternator - 5 kVA
The engine is designedfor application within UAV
®
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AI-28
Advancedgeared fan engines
Specific fuel consumption by 15...20% lower thanthat of current engines in this thrust class
Regional passenger
and medium transport aircraft
Max takeoff, (S/L static; ISA)Thrust, kgf ...................................................................................... 10,300Ambient air temperature to which this thrust is
оmaintained invariable, С ................................................................... +30
Takeoff , (S/L static; ISA)Thrust, kgf ................................................................................... 9,400Ambient air temperature to which this thrust is
оmaintained invariable, С ................................................................... +30
Max cruise, (H =11 000 m, М = 0.8, ISA)Thrust, kgf ........................................................................................ 1,860Specific fuel consumption, kg/h/kgf ................................................. 0.545Ambient air temperature to which this thrust is
оmaintained invariable, С ................................................................... +10
An-178 modification
®AI-9500F
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Tactical fighter
Takeoff
(S/L static; ISA; )s = 1,0in
Full augmented power
(S/L static; ISA; )s = 1,0in
Thrust, kgf ............................................................ 9,500 ...................................... 6,400S , kg/h/kgf ........................ 1.74 ........................................ 0.84pecific fuel consumption
®
Аn-8
Ве-12
Мі-6
Мі-6ААn-10
Мі-10
AI-8
AI-8
Generator terminals power, kW ........ 60
Fuel consumption, kg/h ................... 120
S/L static; ISA
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Ка-52
Bleed airflow, kg/s ............... 0.38
Bleed air pressure, total, MPa, min ..................... 0.24
oBleed air temperature, С ..... 130
АІ-9
Yak-40
Ка-29
Ка-27
Ка-32
Ка-50
Ка-60
Мі-14
Мі-24
М-15
S/L static; ISA
AI-9
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АІ-9V, AI-9V series 1,
AI-9V-1
Мі-8МТ (Мі-8АМТ)
Мі-172
Мі-8МТV
Мi-24 (Мi-35)
Мi-171
Мi-28
AI-9V, AI-9V series 1, AI-9V-1
S/L static; ISA
Aircraft electric system DC power, kW ........ 3
Bleed airflow, kg/s .................................... 0.4
Bleed air pressure, total, MPa, min ........ 0.29
Bleed air temperature, К .......................... 433
Мі-8 (Мі-17)
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S/L static; ISA
Generator terminals power, kW ....................................... 40
Bleed airflow, kg/s, not less .......................................... 0.72
Bleed airflow pressure, absolute, МPa, not less ......... 0.368oBleed airflow temperature, С, not more ........................ 215
Fuel consumption, kg/h, not more .................................. 115
AI-450МS*
* Design is jointly developed by Motor Sich JSCand IVCHENKO-PROGRESS SE
APUs
Аn-140
AI9-3B
Аn-148
S/L static; ISA
Aircraft electric system AC power, kVA ........... 16
Bleed airflow, kg/s .......................................... 0.4
Bleed air pressure, total, MPa, not less ....... 0.32oBleed air temperature, С .............................. 260
АІ9-3B АI-450МS*
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®
GAS-PUMPING UNIT (GPU)
АІ-336-2-8
Gas-pumping unit (GPU)
АI-336-1/2-10
АI-312
Rated power, kW ............... 4,200 .................. 6,300 ................... 6,300 ................ 8,000 .............. 10,000 ............. 10,000 .............. 12,000оflat rated up to t , C .......... + 35 .................... + 15 ..................... + 25 .................. + 15 .................. + 15 ................. + 15 .................. + 15amb
Free turbine rpm ................ 8,200 .................. 8,200 ................... 8,200 ................ 8,200 ................ 4,800 ............... 6,500 ................ 6,500Efficiency ............................. 26.5 ....................... 31 ........................ 31 .................. 31.8 ..................... 34 ..................... 34 .................... 37
D-336-1/2 АI-336-2-8 АI-336-1-10 АI-336-2-10
Developed on the basis of basic GTD variants with parameters, equipment, systems for power, gas and other industrial applications required for a Customer.
D-336-1/2-4 D-336-1T/2Т AI-312
D-336-1/2
D-336-1/2-4
D-336-1Т/2Т
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GTD АІ-2500,
GTD АІ-3000
Rated power, kVA ................................... 4,000 ....................... 6,000Voltage, V .................................... 6,300/10,500 ........... 6,300/10,500Current frequency, Hz .............................. 50/60 ...................... 50/60Current ...................................................................... AC three-phase
POWER STATIONS
Modular
gas turbine
power station
Gas turbine power station
GTD АI-336E-1-4,
GTD АІ-336Е-1-6
GTPS АІ-2500, GTPS АІ-3000
MGTPS АI-4000,
MGTPS АI-6000
Rated power, kVA ..................................... 2,500 ........................ 3,000Voltage, V ..................................... 6,300/10,500 ............ 6,300/10,500Current frequency, Hz .............................. 50/60 ........................ 50/60Current ........................................................................ AC three-phase
AI-2500 AI-3000oup to t +15 Camb
AI-4000 AI-6000oup to t +15 Camb
oup to t +35 Camb
oup to t +15 Camb
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IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
®LOW-EMISSION COMBUSTIONCHAMBERS
D-336, АI-336 GAS TURBINE DRIVES
OF ALL MODIFIED VERSION S WITH LOW-EMISSION
COMBUSTION CHAMBERS
LOW-EMISSION COMBUSTION CHAMBERS
FOR INDUSTRIAL GAS TURBINE UNITS
OF VARIOUS POWER LEVELS BOTH NEW
AND TO BE UPDATED
Nitrogen oxide concentration
3NOx Ј 50 mg/Nm
Carbon monoxide concentration
3CO Ј 100 mg/Nm
under all power ratings without water supply
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IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
®
3 GPU capacity, thousand,Nm /24h ........ 420...2603Volumetric fuel gas flow rate, m /s .................. 0.2
Inlet pressure range, MPa (abs) ........... 0.4 ... 2.1Outlet pressure range, MPa (abs) ........ 3.1 ... 4.5
oInlet gas temperature, С ...................... -20 ...+40oOutlet gas temperature, C, not more .............. 80
3Volumetric gas-and-steam mixture flow rate, m /h ......... 15,000Gas-and-steam mixture oxygen content, % ......................... Ј 2
oGas-and-steam mixture temperature, С ............................. 100Fuel (kerosene) consumption, kg/h ..................................... 320
oWater flow rate at mixture cooling to 100 C, kg/h ............ 6,500
AI-45
Unit type Automotive unit with extensible arm-like pipeline and turntableTurntable rotation speed, rpm ............... Ј 1.5Arm-pipeline lifting (lowering)speed, m/sec ......................................... Ј 0.5Maximum arm-pipeline length, m .............. 16
AI-19GIG-А
SPECIAL EQUIPMENT
АІ-9VP
GAS-PUMPING UNIT
GPU-C-0,7/45-5 АI-45
АI-19GIG
INERT GAS GENERATOR
GAS TURBINE DRIVE (GTD)
АИ-25В-0,8, SUPERCHARGER
GPU-С-0,7/45-5 АI-45
Supercharger
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IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry
AI-19GIG
AI-19GIG-А
MOBILE UNIT
2 Gas operating pressure, kg/cm ............ up to 30 ..... up to 12
FGPU gas pressure drop 2ratio, kg/cm less than 0.5 ..... less than 0.5 .............................
Purification grade:
- from solid particles larger than 40 µ ........... full ..... full
- from liquid fractions .................................... full ..... full
Gas flow rate, kg/h up to 2,500 ..... up to 1,200 ..........................
®
SPECIAL EQUIPMENT
FILTER SEDIMENT
TRAP
FREE TURBINE
MODULE
МSТ-198
CONTAINERIZED VARIANTCONTAINERIZED VARIANT
FILTER SEDIMENTTRAP
Free turbine power, MW ....................................... 20.0
Free turbine rotational speed, rpm ..................... 3,000
Turbine inlet gas temperature, K ........................... 9082Turbine inlet gas pressure, kg/cm 2.83.......................
Turbine inlet air flow, kg/s ..................................... 96.4
Turbine expansion ratio ........................................ 2.63
Efficiency .............................................................. 0.91
МSТ-198
Pressure ratio, max ................................................... 63Compressor power, m /h .................................. 50,000
Pressure ratio, not less .................................................... 103Steam flow rate, m /h (kg/s) .......................... 210,000 (0.16)
ТМ50
ТМ210
COMPRESSORS
OF ТМ50, ТМ210
UNITS
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IVCHENKO-PROGRESS SE, 2020
Ukrainian Defence Industry