Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/Shvetsov_ASh-82> ?p ?o }
- Shvetsov_ASh-82 abstract "The Shvetsov ASh-82 (M-82) is a 14-cylinder, two-row, air-cooled radial aircraft engine developed from the Shvetsov M-62. The M-62 was the result of development of the M-25, which was a licensed version of the Wright R-1820 Cyclone.".
- Shvetsov_ASh-82 thumbnail Aircraft_engine_Shvetsov_ASh-82T.JPG?width=300.
- Shvetsov_ASh-82 wikiPageID "1899060".
- Shvetsov_ASh-82 wikiPageLength "14766".
- Shvetsov_ASh-82 wikiPageOutDegree "66".
- Shvetsov_ASh-82 wikiPageRevisionID "699173846".
- Shvetsov_ASh-82 wikiPageWikiLink Aircraft_engine.
- Shvetsov_ASh-82 wikiPageWikiLink Amtorg_KM-2.
- Shvetsov_ASh-82 wikiPageWikiLink Arkadiy_Shvetsov.
- Shvetsov_ASh-82 wikiPageWikiLink BMW_801.
- Shvetsov_ASh-82 wikiPageWikiLink Bristol_Hercules.
- Shvetsov_ASh-82 wikiPageWikiLink Category:Aircraft_air-cooled_radial_piston_engines.
- Shvetsov_ASh-82 wikiPageWikiLink Category:Aircraft_piston_engines_1940–1949.
- Shvetsov_ASh-82 wikiPageWikiLink Category:Shvetsov_aircraft_engines.
- Shvetsov_ASh-82 wikiPageWikiLink Consolidated_PBY_Catalina.
- Shvetsov_ASh-82 wikiPageWikiLink Douglas_DC-3.
- Shvetsov_ASh-82 wikiPageWikiLink Fiat_A.74.
- Shvetsov_ASh-82 wikiPageWikiLink Focke-Wulf_Fw_190_operational_history.
- Shvetsov_ASh-82 wikiPageWikiLink Gnome-Rhône_14N.
- Shvetsov_ASh-82 wikiPageWikiLink Gudkov_Gu-82.
- Shvetsov_ASh-82 wikiPageWikiLink Ilyushin_Il-12.
- Shvetsov_ASh-82 wikiPageWikiLink Ilyushin_Il-14.
- Shvetsov_ASh-82 wikiPageWikiLink Ilyushin_Il-2.
- Shvetsov_ASh-82 wikiPageWikiLink Inline_engine_(aeronautics).
- Shvetsov_ASh-82 wikiPageWikiLink Kocherigin_OPB-5.
- Shvetsov_ASh-82 wikiPageWikiLink Lavochkin-Gorbunov-Gudkov_LaGG-3.
- Shvetsov_ASh-82 wikiPageWikiLink Lavochkin_La-11.
- Shvetsov_ASh-82 wikiPageWikiLink Lavochkin_La-5.
- Shvetsov_ASh-82 wikiPageWikiLink Lavochkin_La-7.
- Shvetsov_ASh-82 wikiPageWikiLink Lavochkin_La-9.
- Shvetsov_ASh-82 wikiPageWikiLink List_of_aircraft_engines.
- Shvetsov_ASh-82 wikiPageWikiLink Mikoyan-Gurevich_DIS.
- Shvetsov_ASh-82 wikiPageWikiLink Mikoyan-Gurevich_I-211.
- Shvetsov_ASh-82 wikiPageWikiLink Mikoyan-Gurevich_MiG-9_(1941).
- Shvetsov_ASh-82 wikiPageWikiLink Mil_Mi-4.
- Shvetsov_ASh-82 wikiPageWikiLink Mitsubishi_Kinsei.
- Shvetsov_ASh-82 wikiPageWikiLink Nakajima_Sakae.
- Shvetsov_ASh-82 wikiPageWikiLink Petlyakov_Pe-2.
- Shvetsov_ASh-82 wikiPageWikiLink Petlyakov_Pe-8.
- Shvetsov_ASh-82 wikiPageWikiLink Polikarpov_I-185.
- Shvetsov_ASh-82 wikiPageWikiLink Prague_Aviation_Museum,_Kbely.
- Shvetsov_ASh-82 wikiPageWikiLink Pratt_&_Whitney_R-1830_Twin_Wasp.
- Shvetsov_ASh-82 wikiPageWikiLink Pratt_&_Whitney_R-4360_Wasp_Major.
- Shvetsov_ASh-82 wikiPageWikiLink Radial_engine.
- Shvetsov_ASh-82 wikiPageWikiLink Shvetsov.
- Shvetsov_ASh-82 wikiPageWikiLink Shvetsov_ASh-21.
- Shvetsov_ASh-82 wikiPageWikiLink Shvetsov_ASh-62.
- Shvetsov_ASh-82 wikiPageWikiLink Soviet_Union.
- Shvetsov_ASh-82 wikiPageWikiLink Stroke_(engine).
- Shvetsov_ASh-82 wikiPageWikiLink Sukhoi_Su-12.
- Shvetsov_ASh-82 wikiPageWikiLink Sukhoi_Su-2.
- Shvetsov_ASh-82 wikiPageWikiLink Sukhoi_Su-6.
- Shvetsov_ASh-82 wikiPageWikiLink Time_between_overhaul.
- Shvetsov_ASh-82 wikiPageWikiLink Tupolev_Tu-2.
- Shvetsov_ASh-82 wikiPageWikiLink Wright_R-1820.
- Shvetsov_ASh-82 wikiPageWikiLink Wright_R-2600.
- Shvetsov_ASh-82 wikiPageWikiLink Yakovlev_Yak-11.
- Shvetsov_ASh-82 wikiPageWikiLink Yakovlev_Yak-24.
- Shvetsov_ASh-82 wikiPageWikiLink File:Aircraft_engine_Shvetsov_ASh-82T.JPG.
- Shvetsov_ASh-82 wikiPageWikiLink File:Shvetsov_family_tree.svg.
- Shvetsov_ASh-82 wikiPageWikiLinkText "ASh-82".
- Shvetsov_ASh-82 wikiPageWikiLinkText "ASh-82FN".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Dongan HS7".
- Shvetsov_ASh-82 wikiPageWikiLinkText "M-82".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Shvetsov AS-82".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Shvetsov ASh-82".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Shvetsov ASh-82/M-82".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Shvetsov ASh-82FN (M-82FN)".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Shvetsov ASh-82FN".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Shvetsov ASh-82T".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Shvetsov ASh-82V".
- Shvetsov_ASh-82 wikiPageWikiLinkText "Shvetsov M-82".
- Shvetsov_ASh-82 bore "155.5".
- Shvetsov_ASh-82 compression "7.05".
- Shvetsov_ASh-82 coolingsystem "Air-cooled. Minimum permissible cylinders temp for operation: 120°C. Maximum permissible cylinders temp: 250°C. Maximum permissible at cruise: 225°C. Normal cylinders temp at cruise: 160 to 180°C".
- Shvetsov_ASh-82 developedFrom Shvetsov_ASh-62.
- Shvetsov_ASh-82 developedInto Shvetsov_ASh-21.
- Shvetsov_ASh-82 diameter "1.26 m".
- Shvetsov_ASh-82 displacement "41.2107".
- Shvetsov_ASh-82 fuelsystem "Carburettors , direct fuel injection with automatic mixture control. Petrol pump: BNK-10KT.".
- Shvetsov_ASh-82 fueltype "90".
- Shvetsov_ASh-82 generators "GDS-6000A 150 Amp".
- Shvetsov_ASh-82 length "2.01 m".
- Shvetsov_ASh-82 lists "*List of aircraft engines".
- Shvetsov_ASh-82 magnetos "Two MB14T-2M".
- Shvetsov_ASh-82 manufacturer "Shvetsov & Evich, OKB-19 in Perm'".
- Shvetsov_ASh-82 numberBuilt "70000".
- Shvetsov_ASh-82 oilsystem "Two pumps: geared rotation pump MSH-6SV and swarm pump PMN-T . Normal oil temp: 40 to 90°C. Limit temp: 115°C. Minimum oil pressure at low gas: 3 kg/cm2 . Minimum oil pressure at cruise: 4.5 kg/cm2 , 5.5 kg/cm2".
- Shvetsov_ASh-82 power "*M-82-111 with carburettors: *1,570 hp at 2,400 RPM for take-off , boost rated at 1.55 Atm *1,540 hp at 2,400 RPM at 6,656 ft *1,330 hp at 2,400 RPM at 17,716 ft , boost rated at 1.29 Atm * 820 hp at 2,400 RPM at 27,887 ft *M-82F with carburettors: *1,650 hp at 2,400 RPM for take-off , boost rated at 1.55 Atm *1,430 hp at 2,400 RPM at 16,404 ft *800 hp at 2,400 RPM at 32,808 ft *M-82FNV and M-82FN with direct fuel injection: *1,850 hp at 2,500 RPM for take-off , boost rated at 1.60 Atm *1,650 hp at 2,400 RPM at 5,413 ft , boost rated at 1.36 Atm *1,450 hp at 2,400 RPM at 15,156 ft , boost rated at 1.36 Atm *810 hp at 2,400 RPM at 34,448 ft *M-82T with two speed supercharger: *1,900 hp at 2,600 RPM for take-off, boost rated at 1.64 Atm *1,630 hp at 2,400 RPM at 6,561 ft , boost rated at 1.34 Atm *1,530 hp at 2,400 RPM at 13,123 ft , boost rated at 1.34 Atm *721 hp at 2,400 RPM at 31,167 ft".
- Shvetsov_ASh-82 weight "1.46".
- Shvetsov_ASh-82 reductionGear "11".
- Shvetsov_ASh-82 similarEngines "*BMW 801 *Bristol Hercules *Fiat A.74 *Gnome-Rhône 14N *Mitsubishi Kinsei *Nakajima Sakae *Pratt & Whitney R-1830 *Wright R-2600".
- Shvetsov_ASh-82 specfuelcon "*M-82F: 355 g/hp•h for take-off, 320 g/hp•hr at nominal power *M-82FNV: 360 g/hp•h for take-off, 325 g/hp•hr at nominal power *M-82T: 350 to 325 g/hp•h for take-off, 260 to 280 g/hp•hr at cruise power".
- Shvetsov_ASh-82 specpower "M-82F: 29.84 kW/L , M-82FNV: 33.48 kW/L".
- Shvetsov_ASh-82 stroke "155.0".
- Shvetsov_ASh-82 supercharger "240000.0".
- Shvetsov_ASh-82 type Radial_engine.
- Shvetsov_ASh-82 type "14".
- Shvetsov_ASh-82 valvetrain "Pushrod, two valves per cylinder with sodium-cooled exhaust valve.".
- Shvetsov_ASh-82 weight "M-82-112 model: 860 kg , M-82FN model: 890 kg , M-82FNV model: 900 kg , M-82T model: 1,020 kg".