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214:("VMA" stands for "high altitude, modernized, model A") – for Ka-50 helicopters. It is currently installed on Ka-27, Ka-29, Ka-31, Mi-24, Mi-28A/N and Ka-32 machines. This engine was awarded type certificates by the IAC Aviation Registry and by Transport Canada. Mass production started in 1986. Export models are equipped with TV3-117VMAR engines (the extra "R" stands for "power") whose rated power and cruising power are similar to those of the TV3-117VKR engine
197:("VK" stands for "high altitude, Kamov") – a model similar to the TV3-117V engine but adapted to Ka-27, Ka-29 and Ka-32 helicopters. Mass production began in 1985. Export helicopter models were equipped with TV3-117VKR engines featuring a higher rated and cruising power ("VKR" stands for "high altitude, Kamov, power"); they were originally designed for Ka-28 machines
207:
helicopters and later installed also on Mi-8MT/Mi-17 models. This engine features an automatic switch to emergency power. It was awarded type certificates by the IAC Aviation
Registry, India, the Republic of China and the People's Republic of China. Mass-produced since
220:– a version of TV3-117VM for Mi-8MT/Mi-17 civil helicopters. Type certificates for this engine were awarded by the IAC Aviation Register, India, the Republic of China and the People's Republic of China. Mass production started in 1993
226:– a version of TV3-117VMA for Ka-32 civil helicopters. Type certificates for this engine were awarded by the IAC Aviation Register, Transport Canada and Switzerland. Mass production started in 1993
139:
engine was developed in 1974. Later the Klimov TV3-117 was installed on 95% of all helicopters designed by Mil and Kamov
Engineering Centre. The engine has been produced in many variants.
527:
586:
191:("V" stands for "high altitude") – for Mi-24 helicopters operated in the mountains (particularly in Afghanistan). Mass production started in 1980
528:
https://www.researchgate.net/figure/TV3-117-A-two-stage-turbine-driving-a-compressor-and-a-free-turbine-driving-a-rotor-and_fig1_363405659
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16 turbines. 12 as compressor and 4 as free turbine for drive rotor and compressors. all axial.
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helicopters and their variants. Mass production started in 1977
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Brassey's World
Aircraft & Systems Directory 1999/2000
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designed by the Mil and Kamov design bureaus. The TV3-117
539:
Brassey's World
Aircraft & Systems Directory 1999/2000
131:. It is used in most medium lift, utility, and attack
203:("VM" stands for "high altitude, modernized") – for
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171:("MT" stands for "modernized, transport") – for
252:highly modified TV3-117 2700 hp also for
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515:"SOV - Klimov TV3-117 : Turbovrtulové"
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181:("KM" stands for "Kamov, marine") – for
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429:920–990 C (Turbine entry temperature)
7:
328:Specifications (TV3-117VMA Series 2)
25:
438:0.308 kg/kW/hr (0.507 lb/shp/hr)
161:("M" stands for "marine") – for
35:
408:1,640 kW (2,200 shp) (take-off)
380:12 stage axial, no centrifugal.
1:
64:, MMP chernyshev Salyut UMPO
806:
541:. London:Brassey's, 1999.
427:Turbine inlet temperature:
423:8.7 kg/s (19 lb/s) minimum
395:basically Russian Jet Fuel
434:Specific fuel consumption
361:728 mm (28.7 in) (height)
240:aircraft produced by the
34:
29:
785:1970s turboshaft engines
475:List of aircraft engines
790:Klimov aircraft engines
348:Free-turbine turboshaft
339:General characteristics
537:Taylor, Michael J. H.
413:Overall pressure ratio
443:Power-to-weight ratio
406:Maximum power output:
223:TV3-117VMA series 02
493:Brasseys 1999 p.670
217:TV3-117VM Series 02
457:Comparable engines
355:2,055 mm (80.9 in)
78:Major applications
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16:(Redirected from
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599:aircraft engines
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232:a 2000 hp
229:TV3-117VMA-SBM1
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18:Isotov TV3-117
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261:Applications
254:hot and high
236:version for
173:Mi-8MT/Mi-17
124:is a Soviet
121:
119:
110:Number built
721:turboshafts
400:Performance
378:Compressor:
365:Dry weight:
287:Kamov Ka-50
282:Kamov Ka-32
277:Kamov Ka-29
272:Kamov Ka-27
185:helicopters
133:helicopters
129:aero engine
126:gas turbine
114:>25,000
83:Kamov Ka-27
779:Categories
717:Turboprops
481:References
447:5.58 kW/kg
393:Fuel type:
372:Components
211:TV3-117VMA
137:turboshaft
69:First run
58:Motor Sich
48:Turboshaft
703:Turbofans
675:Turbojets
359:Diameter:
333:Data from
317:Mil Mi-35
312:Mil Mi-28
307:Mil Mi-24
302:Mil Mi-17
297:Mil Mi-14
234:Turboprop
200:TV3-117VM
194:TV3-117VK
178:TV3-117KM
168:TV3-117MT
452:See also
292:Mil Mi-8
188:TV3-117V
158:TV3-117M
143:Variants
103:TAI T925
87:Mil Mi-8
30:TV3-117
764:VK-3000
759:VK-2500
754:VK-1500
744:TV7-117
739:TV3-117
734:TV2-117
729:GTD-350
385:Turbine
353:Length:
248:VK-2500
244:Company
242:Antonov
148:TV3-117
749:VK-800
693:RD-500
665:VK-150
660:VK-110
655:VK-109
650:VK-108
645:VK-107
640:VK-106
596:Klimov
545:
238:An-140
155:(1972)
153:Mi-24A
62:Klimov
709:RD-33
683:RD-45
635:M-120
630:M-110
625:M-105
620:M-103
615:M-100
417:9.4:1
345:Type:
205:Mi-28
183:Ka-27
163:Mi-14
95:Mi-28
91:Mi-24
72:1974
44:Type
719:and
688:VK-3
543:ISBN
208:1986
151:for
120:The
781::
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588:e
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574:v
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20:)
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