29:
116:
the engine became the first purpose built gas turbine engine for helicopter use by the Soviet Union with previous helicopter turbines being adapted aeroplane powerplants. It was later produced by
509:
460:
123:
The TV2-117 is claimed to be the most popular helicopter powerplant worldwide and has accumulated over 100 million hours in service.
707:
180:
Multi-fuel variant, adapted to run on liquid petroleum gas and other fuels (gasoline or diesel fuel) and for use in cold climates.
712:
502:
363:
431:
495:
404:
215:
World
Encyclopaedia of Aero Engines, World Encyclopaedia of Aero Engines, Aircraft engines of the World 1970
339:
113:
372:
529:
686:
676:
587:
582:
577:
552:
537:
456:
392:
149:
331:
1,300 kW (1,800 hp) at 12,000 rpm (power turbine) at 1,200 m (3,900 ft)
521:
435:
681:
666:
661:
651:
92:
701:
671:
615:
572:
567:
562:
428:
190:
631:
557:
547:
542:
610:
605:
28:
643:
109:
39:
639:
269:
201:
487:
455:(2nd ed.). Cambridge, England: Patrick Stephens Limited. p. 81.
625:
597:
290:
196:
69:
278:
112:
engine intended for helicopter use. Designed in the early 1960s by the
518:
325:
1,500 shp (1,100 kW) at 12,000 rpm (power turbine) de-rated
117:
49:
480:(21st ed.). Washington D.C.: Paul H. Wilkinson. p. 214.
294:
491:
169:
302:
Pressure spray at 50 psi (3.4 bar) with return
283:
Two-stage compressor turbine, two-stage power turbine
638:
624:
596:
528:
503:
252:330 kg (730 lb) (minus accessories)
8:
510:
496:
488:
168:Limited production of engine certified to
446:
444:
424:
422:
420:
368:0.606 lb/(hp⋅h) (0.369 kg/kWh)
193:(intended coupled turboprop application)
416:
16:1960s Soviet turboshaft aircraft engine
18:
7:
453:World Encyclopaedia of Aero Engines
478:Aircraft engines of the World 1970
172:airworthiness standards for Japan.
148:Improved engine with more durable
14:
377:2.06 hp/lb (3.39 kW/kg)
350:8.1 kg/s (1,070 lb/min)
246:0.12 m (1.3 sq ft)
27:
1:
120:, production ending in 1997.
160:Carbon sealed shaft bearings
476:Wilkinson, Paul H. (1970).
429:Klimov TV2-117 product page
729:
359:1,150 K (880 °C)
354:Turbine inlet temperature:
233:2,390 mm (94 in)
108:) is a Soviet gas-turbine
364:Specific fuel consumption
208:Specifications (TV2-117A)
26:
21:
708:1960s turboshaft engines
405:List of aircraft engines
239:400 mm (16 in)
713:Klimov aircraft engines
219:General characteristics
451:Gunston, Bill (1989).
438:Retrieved: 24 May 2012
340:Overall pressure ratio
274:Eight-chamber cannular
373:Power-to-weight ratio
313:Maximum power output:
265:Ten-stage axial flow
114:Isotov Design Bureau
344:6.6:1 at 21,200 rpm
434:2013-03-07 at the
387:Comparable engines
65:Major applications
695:
694:
462:978-1-85260-163-8
393:Rolls-Royce Gnome
150:compressor stator
98:
97:
720:
522:aircraft engines
512:
505:
498:
489:
482:
481:
473:
467:
466:
448:
439:
426:
89:
79:
66:
31:
19:
728:
727:
723:
722:
721:
719:
718:
717:
698:
697:
696:
691:
634:
620:
592:
524:
516:
486:
485:
475:
474:
470:
463:
450:
449:
442:
436:Wayback Machine
427:
418:
413:
384:
329:Altitude power:
323:Take-off power:
315:
309:
259:
240:
221:
210:
187:
129:
87:
77:
64:
17:
12:
11:
5:
726:
724:
716:
715:
710:
700:
699:
693:
692:
690:
689:
684:
679:
674:
669:
664:
659:
654:
648:
646:
636:
635:
630:
628:
622:
621:
619:
618:
613:
608:
602:
600:
594:
593:
591:
590:
585:
580:
575:
570:
565:
560:
555:
550:
545:
540:
534:
532:
530:Piston engines
526:
525:
517:
515:
514:
507:
500:
492:
484:
483:
468:
461:
440:
415:
414:
412:
409:
408:
407:
396:
395:
383:
380:
379:
378:
369:
360:
351:
348:Air mass flow:
345:
335:
334:
333:
332:
326:
317:
316:
308:
305:
304:
303:
297:
284:
275:
266:
258:
255:
254:
253:
247:
241:
234:
228:
220:
217:
209:
206:
205:
204:
199:
194:
186:
183:
182:
181:
178:
174:
173:
166:
162:
161:
158:
154:
153:
146:
142:
141:
138:
132:Source:Klimov.
128:
125:
106:Isotov TV2-117
102:Klimov TV2-117
96:
95:
93:Klimov TV3-117
90:
88:Developed into
84:
83:
80:
74:
73:
67:
61:
60:
57:
53:
52:
47:
43:
42:
37:
33:
32:
24:
23:
15:
13:
10:
9:
6:
4:
3:
2:
725:
714:
711:
709:
706:
705:
703:
688:
685:
683:
680:
678:
675:
673:
670:
668:
665:
663:
660:
658:
655:
653:
650:
649:
647:
645:
641:
637:
633:
629:
627:
623:
617:
614:
612:
609:
607:
604:
603:
601:
599:
595:
589:
586:
584:
581:
579:
576:
574:
571:
569:
566:
564:
561:
559:
556:
554:
551:
549:
546:
544:
541:
539:
536:
535:
533:
531:
527:
523:
520:
513:
508:
506:
501:
499:
494:
493:
490:
479:
472:
469:
464:
458:
454:
447:
445:
441:
437:
433:
430:
425:
423:
421:
417:
410:
406:
403:
402:
401:
400:
399:Related lists
394:
391:
390:
389:
388:
381:
376:
374:
370:
367:
365:
361:
358:
355:
352:
349:
346:
343:
341:
337:
336:
330:
327:
324:
321:
320:
319:
318:
314:
311:
310:
306:
301:
298:
296:
292:
288:
285:
282:
280:
276:
273:
271:
267:
264:
261:
260:
256:
251:
248:
245:
244:Frontal area:
242:
238:
235:
232:
229:
226:
223:
222:
218:
216:
214:
207:
203:
200:
198:
195:
192:
191:Antonov An-24
189:
188:
184:
179:
176:
175:
171:
167:
164:
163:
159:
156:
155:
151:
147:
144:
143:
140:Base variant.
139:
136:
135:
134:
133:
126:
124:
121:
119:
115:
111:
107:
103:
94:
91:
86:
85:
81:
76:
75:
71:
68:
63:
62:
58:
55:
54:
51:
48:
46:Manufacturer
45:
44:
41:
38:
35:
34:
30:
25:
20:
656:
477:
471:
452:
398:
397:
386:
385:
371:
362:
356:
353:
347:
338:
328:
322:
312:
299:
286:
277:
268:
262:
249:
243:
236:
230:
224:
212:
211:
185:Applications
131:
130:
122:
105:
101:
99:
78:Number built
644:turboshafts
307:Performance
300:Oil system:
263:Compressor:
250:Dry weight:
104:(initially
702:Categories
640:Turboprops
411:References
287:Fuel type:
270:Combustors
257:Components
227:Turboshaft
110:turboshaft
56:First run
40:Turboshaft
626:Turbofans
598:Turbojets
289:Aviation
237:Diameter:
213:Data from
202:Mil Mi-14
177:TV2-117TG
157:TV2-117AG
432:Archived
382:See also
293:such as
291:Kerosene
197:Mil Mi-8
165:TV2-117F
145:TV2-117A
127:Variants
70:Mil Mi-8
22:TV2-117
687:VK-3000
682:VK-2500
677:VK-1500
667:TV7-117
662:TV3-117
657:TV2-117
652:GTD-350
279:Turbine
231:Length:
152:blades.
137:TV2-117
82:23,000
672:VK-800
616:RD-500
588:VK-150
583:VK-110
578:VK-109
573:VK-108
568:VK-107
563:VK-106
519:Klimov
459:
118:Klimov
50:Klimov
632:RD-33
606:RD-45
558:M-120
553:M-110
548:M-105
543:M-103
538:M-100
225:Type:
59:1962
36:Type
642:and
611:VK-3
457:ISBN
295:JP-4
100:The
357:TIT
170:FAA
704::
443:^
419:^
72:.
511:e
504:t
497:v
465:.
375::
366::
342::
281::
272::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
