Lotarev D-136 (original) (raw)

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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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dbo:wikiPageLength 5582 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID 1089808365 (xsd:integer)
dbo:wikiPageWikiLink 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 dbt:Cite_magazine dbt:Cite_news dbt:Cite_web dbt:Commons_category dbt:Cvt dbt:Portal dbt:R dbt:Refimprove dbt:Reflist dbt:Short_description dbt:Ivchenko_aeroengines dbt:Jetspecs dbt:Aircontent dbt:Infobox_aircraft_engine
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)
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