dbo:abstract |
The Lotarev D-136 is a turboshaft engine from the ZMKB Progress Design Bureau. The engine powers the Mil Mi-26 "Halo" helicopter. Development of the engine had begun in about 1972.. The D-136 first flew on a production Mi-26 helicopter in 1980. (en) Le D-136 est un turbomoteur de très forte puissance employé exclusivement par l'hélicoptère russe de transport lourd Mi-26 Halo. Dépassant les 11 000 chevaux de puissance, il a été conçu par l'OKB Ivtchenko-Progress, puis fabriqué par Motor Sich, en Ukraine. (fr) Д-136 — авиационный турбовальный двигатель, разработанный в конце 1970-х годов в ГП "Ивченко-Прогресс" на базе ТРДД Д-36. Серийно выпускается с 1982 года на ЗПО «Моторостроитель», ныне АО «Мотор Сич». (ru) Д-136 — турбовальний двигун призначений для установки на транспортний вертоліт Мі-26. (uk) |
dbo:thumbnail |
wiki-commons:Special:FilePath/D136_engine_maks2009.jpg?width=300 |
dbo:wikiPageExternalLink |
http://www.rusaviainsider.com/ukraine-starts-testing-improved-engine-for-heavy-helicopters/ https://ivchenko-progress.com/%3Fportfolio=d136&lang=en https://archive.org/details/MilHeavyHelicopters/page/n76 https://archive.org/details/MilHeavyHelicopters/page/n79 https://archive.org/details/MilHeavyHelicopters/page/n90 https://archive.org/details/MilHeavyHelicopters/page/n91 https://archive.aviationweek.com/issue/19810615/%23!&pid=28 http://www.motorsich.com/eng/products/aircraft/turboshaft/d-136/ http://www.motorsich.com/eng/products/aircraft/turboshaft/d136_2/ https://ivchenko-progress.com/%3Fportfolio=%D0%B4-136-2&lang=en |
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dbr:Progress_D-236 dbr:List_of_aircraft_engines dbr:Motor_Sich dbr:Lotarev_D-36 dbc:Ivchenko-Progress_aircraft_engines dbr:Aviadvigatel_PD-14 dbr:Aviation_Week_&_Space_Technology dbr:Allison_T701 dbr:Turbofan dbr:Ivchenko-Progress dbc:1980s_turboshaft_engines dbr:Soviet_Union dbr:Mil_Mi-26 dbr:MAKS_Air_Show dbr:Turboshaft |
dbp:combustion |
Annular combustion chamber, 24 fuel nozzles, 2 igniters (en) |
dbp:compression |
18.300000 (xsd:double) |
dbp:compressor |
7 (xsd:integer) |
dbp:developedFrom |
dbr:Lotarev_D-36 |
dbp:developedInto |
dbr:Progress_D-236 |
dbp:length |
*Width: *Height: (en) |
dbp:lists |
* List of aircraft engines (en) |
dbp:majorApplications |
dbr:Mil_Mi-26 |
dbp:manufacturer |
dbr:Motor_Sich dbr:Ivchenko-Progress |
dbp:nationalOrigin |
dbr:Soviet_Union |
dbp:power |
Takeoff: ; Contingency: ; Sustained: (en) |
dbp:ref |
Mil's heavylift helicopters, pages 90-91 (en) |
dbp:related |
*Lotarev D-36 *Progress D-236 (en) |
dbp:similarEngines |
*Allison T701 *Aviadvigatel PD-12V (en) |
dbp:specfuelcon |
Takeoff: ; Cruise: (en) |
dbp:turbine |
1 (xsd:integer) |
dbp:turbinetemp |
Takeoff: ; Maximum: (en) |
dbp:type |
3 (xsd:integer) dbr:Turboshaft |
dbp:wikiPageUsesTemplate |
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dcterms:subject |
dbc:Ivchenko-Progress_aircraft_engines dbc:1980s_turboshaft_engines |
rdfs:comment |
The Lotarev D-136 is a turboshaft engine from the ZMKB Progress Design Bureau. The engine powers the Mil Mi-26 "Halo" helicopter. Development of the engine had begun in about 1972.. The D-136 first flew on a production Mi-26 helicopter in 1980. (en) Le D-136 est un turbomoteur de très forte puissance employé exclusivement par l'hélicoptère russe de transport lourd Mi-26 Halo. Dépassant les 11 000 chevaux de puissance, il a été conçu par l'OKB Ivtchenko-Progress, puis fabriqué par Motor Sich, en Ukraine. (fr) Д-136 — авиационный турбовальный двигатель, разработанный в конце 1970-х годов в ГП "Ивченко-Прогресс" на базе ТРДД Д-36. Серийно выпускается с 1982 года на ЗПО «Моторостроитель», ныне АО «Мотор Сич». (ru) Д-136 — турбовальний двигун призначений для установки на транспортний вертоліт Мі-26. (uk) |
rdfs:label |
Ivtchenko-Progress D-136 (fr) Lotarev D-136 (en) Д-136 (ru) Д-136 (uk) |
owl:sameAs |
wikidata:Lotarev D-136 dbpedia-fr:Lotarev D-136 dbpedia-ru:Lotarev D-136 dbpedia-uk:Lotarev D-136 dbpedia-vi:Lotarev D-136 https://global.dbpedia.org/id/3rCGm |
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wikipedia-en:Lotarev_D-136?oldid=1089808365&ns=0 |
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