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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.

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rdfs:label
  • Ivtchenko-Progress D-136 (fr)
  • Lotarev D-136 (en)
  • Д-136 (ru)
  • Д-136 (uk)
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)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/D136_engine_maks2009.jpg
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Link from a Wikipage to an external page
sameAs
similar engines
  • *Allison T701 *Aviadvigatel PD-12V (en)
specfuelcon
  • Takeoff: ; Cruise: (en)
turbine
turbinetemp
  • Takeoff: ; Maximum: (en)
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thumbnail
national origin
length
  • *Width: *Height: (en)
manufacturer
power
  • Takeoff: ; Contingency: ; Sustained: (en)
ref
  • Mil's heavylift helicopters, pages 90-91 (en)
related
  • *Lotarev D-36 *Progress D-236 (en)
type
has 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)
combustion
  • Annular combustion chamber, 24 fuel nozzles, 2 igniters (en)
compression
compressor
developed from
developed into
lists
  • * List of aircraft engines (en)
major applications
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