37:
506:
Gear-driven two-speed centrifugal type compressor. Gear ratios: 7.78:1 (1st speed) 11.0:1 (2nd speed). Maximum boost for take-off: 965 mm Hg (38.00 MP), subsequent variants had 1,100 or 1,200 mm Hg. Maximum boost at altitude: 920 mm Hg (36.22 MP), subsequent variants had 1,100 mm Hg. Emergency boost
269:
Modification with significantly increased power output at the expense of decreased high-altitude performance. In spite of Klimov's concerns about decreased service life, the engine was pressed into production at the insistence of
280:- (1,300 to 1,360 horsepower (970 to 1,015 kW)) Further increase in power output, which was believed to have exhausted the potential of the M-105 design for greater performance. The "PF2" was installed in the Yak-3 and
212:
of the cylinder banks, with the exhaust system also exiting from the outboard side, with twin sets of "siamesed" exhaust ports adjacent to each other. About 129,000 M-105 and its variants were built.
274:, and further exploitation of "PF" version showed this was the right decision. The "PF" was installed on the most numerous versions of "Yak" fighters - Yak-1B, Yak-7B, Yak-9.
809:
1012:
507:(maximum 2 minutes): 1,100 mm Hg (43.30 MP) at 2,800 RPM. Critical altitude: 2,000 m (6,561 ft) at 1st speed, 4,000 m (13,123 ft) at 2nd speed.
513:
Six K-105 Carburettors (License copy of Solex-Hispano 56SVC self-adjusted carburettor), three on each "outboard" side of cylinder banks
290:- (1,170 horsepower (870 kW)) Engine with 2-stage E-100 turbocharger, experimental high-altitude version, unsuccessful prototype.
766:
747:
98:
1007:
802:
341:
336:
582:
533:
297:
215:
During the war, Klimov's engines were redesignated from "M" (for "motor," engine) to "VK" for the lead designer's initials.
1017:
795:
205:
227:- (1,100 horsepower (820 kW)) First version produced at the end of 1939. Installed on some pre-war fighters.
676:
45:
306:- (1,110 horsepower (830 kW)) M-105PA with decreased propeller reduction gear ratio for bomber aircraft.
714:
Helsinki: Maintenance and spare technical manual of the
Finnish Government. The National Library of Finland.
724:
During the war, the Soviet Air Force used fuel mixtures, including automotive gasoline, without troubles.
597:
249:. Installed on the majority Soviet pre-war fighters - Yak-1, LaGG-1 and several experimental aircraft.
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152:
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266:
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234:
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158:
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1,050 hp (782 kW) at 2,700 RPM at 13,123 ft (4,000 m), boost rated at 1.21 Atm (36.22 MP)
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1,100 hp (820 kW) at 2,700 RPM for take-off, boost rated at 1.27 Atm (38.00 MP)
943:
782:
712:
Hispano-Suiza 12Y-31, M-103, M-105. Rakenneselostus, Käyttö – Ja
Huoltoohjeet
484:
468:
417:
242:
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149:
56:
36:
17:
939:
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165:
300:
ratio for bomber aircraft. Installed on Pe-2, BB-22 (Yak-4) and others.
818:
490:
181:
155:
78:
281:
233:- (1,050 horsepower (780 kW)) First mass production engine (
791:
204:. The M-105 was the first Klimov V-12 engine design to use
493:-filled exhaust valve per cylinder actuated via a single
296:- (1,100 horsepower (820 kW)) Decreased propeller
938:
924:
896:
828:
560:
500 hp (372 kW) at 2,700 RPM at 31,168 ft (9,500 m)
208:, forcing the induction system to be placed on the
742:. Cambridge, England: Patrick Stephens Limited.
497:per bank. Valve lift: 13 mm (intake and exhaust)
803:
180:The M-105, designed in 1940, drew heavily on
8:
255:- (1,200 horsepower (890 kW)) Improved
810:
796:
788:
196:, the M-105 had several improvements like
192:as the M-100). In addition to a two-speed
761:. Marlborough, Wiltshire: Crowood Press.
693:
241:(моторная пушка - motor cannon)-mount
26:
7:
265:- (1,260 horsepower (940 kW))
740:World Encyclopedia of Aero Engines
416:Twelve-cylinder liquid-cooled 60°
25:
710:Valtion Lentokonetehdas (1943).
342:Lavochkin-Gorbunov-Gudkov LaGG-3
337:Lavochkin-Gorbunov-Gudkov LaGG-1
35:
538:1: 0.666 (1: 0.591 for M-105R)
519:94 (minimum grade), 95 or 100
198:two intake valves per cylinder
1:
1013:1930s aircraft piston engines
757:Kotelnikov, Vladimir (2005).
587:328 g/(kW•h) (0.54 lb/(hp•h))
446:35.101 Liters (2,142.2 cu in)
593:11 g/(kW•h) (0.28 oz/(hp•h))
759:Russian Piston Aero Engines
206:reverse-flow cylinder heads
1034:
489:Two intake valves and one
583:Specific fuel consumption
569:23.36 kW/L (0.513 hp/in³)
43:
34:
29:
677:List of aircraft engines
46:Central Air Force Museum
1008:Klimov aircraft engines
602:1.42 kW/kg (0.86 hp/lb)
408:General characteristics
398:Specifications (VK-105)
783:VK-105 on ram.home.com
738:Gunston, Bill (1989).
200:and a counterbalanced
598:Power-to-weight ratio
245:in the "vee" between
44:A VK-105PF engine in
1018:V12 aircraft engines
237:). Able to accept a
184:experience with the
700:Gunston 1989, p. 90
655:Daimler-Benz DB 601
612:Related development
278:VK-105PF2 & PF3
665:Rolls-Royce Merlin
644:Comparable engines
452:2,027 mm (79.8 in)
263:M-105PF (VK-105PF)
94:Major applications
995:
994:
618:Hispano-Suiza 12Z
574:Compression ratio
495:overhead camshaft
473:575 kg (1,266 lb)
464:945 mm (37.20 in)
458:777 mm (30.59 in)
322:Arkhangelsky Ar-2
186:Hispano-Suiza 12Y
142:
141:
16:(Redirected from
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591:Oil consumption:
437:170mm (6.693 in)
428:148mm (5.826 in)
392:Yermolayev Yer-2
239:motornaya pushka
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64:National origin
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387:Yakovlev Yak-9
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382:Yakovlev Yak-7
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377:Yakovlev Yak-4
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372:Yakovlev Yak-3
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367:Yakovlev Yak-2
364:
362:Yakovlev Yak-1
359:
357:Petlyakov Pe-3
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352:Petlyakov Pe-2
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332:P-40 Kittyhawk
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317:P-39 Airacobra
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298:reduction gear
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247:cylinder banks
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140:
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132:Developed from
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115:Yakovlev Yak-3
111:Yakovlev Yak-9
107:Yakovlev Yak-1
103:Petlyakov Pe-2
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768:1-86126-702-9
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671:Related lists
666:
663:
661:
660:Mikulin AM-35
658:
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648:
647:
646:
645:
639:
638:Klimov VK-107
636:
634:
633:Klimov VK-106
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628:Klimov VK-104
626:
624:
623:Klimov VK-103
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549:Power output:
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529:Liquid-cooled
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521:octane rating
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153:liquid-cooled
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18:Klimov M-105P
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732:Bibliography
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511:Fuel system:
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502:Supercharger
500:
483:
467:
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449:
442:Displacement
440:
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422:
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347:Mörkö-Morane
311:Applications
303:
293:
287:
277:
262:
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238:
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224:
214:
209:
194:supercharger
179:
170:World War II
146:Klimov M-105
145:
143:
137:Klimov M-103
122:Number built
69:Soviet Union
944:turboshafts
543:Performance
327:Ikarus S-49
176:Development
126:c. 129,000
1002:Categories
940:Turboprops
683:References
517:Fuel type:
485:Valvetrain
478:Components
469:Dry weight
418:V12 engine
243:autocannon
202:crankshaft
85:First run
926:Turbofans
898:Turbojets
523:gasoline.
403:Data from
48:(Moscow)
607:See also
272:Yakovlev
259:version.
219:Variants
182:Klimov's
166:aircraft
161:used by
987:VK-3000
982:VK-2500
977:VK-1500
967:TV7-117
962:TV3-117
957:TV2-117
952:GTD-350
462:Height:
450:Length:
304:M-105RA
288:M-105PD
253:M-105PA
210:outside
168:during
972:VK-800
916:RD-500
888:VK-150
883:VK-110
878:VK-109
873:VK-108
868:VK-107
863:VK-106
819:Klimov
765:
746:
491:sodium
456:Width:
433:Stroke
294:M-105R
282:Yak-9U
231:M-105P
225:M-105
163:Soviet
156:piston
148:was a
99:LaGG-3
79:Klimov
30:M-105
932:RD-33
906:RD-45
858:M-120
853:M-110
848:M-105
843:M-103
838:M-100
688:Notes
578:7.0:1
414:Type:
88:1938
53:Type
942:and
911:VK-3
763:ISBN
744:ISBN
424:Bore
267:1942
257:1941
235:1940
144:The
150:V12
57:V12
1004::
172:.
811:e
804:t
797:v
771:.
752:.
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284:.
188:(
20:)
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