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The Turbomeca Turmo is a French turboshaft engine developed for helicopter use. A descendant of Turbomeca's pioneering Artouste design, later versions delivered around 1,200 kW (1,610 shp). A turboprop version was developed for use with the Breguet 941 transport aircraft. Current versions are built in partnership with Rolls-Royce, and the engine is produced under license by the Chinese Changzhou Lan Xiang Machinery Works as the WZ-6 and Romanian Turbomecanica Bucharest as the Turmo IV-CA ==Variants== ;Turmo IIIC:A turboshaft powering the Sud-Aviation Frelon prototypes. ;Turmo IIIC2: Developed from the IIIC delivering maximum output ;Turmo IIIC3: Maximum rating at 33,500 rpm for production Super Frelon helicopters ;Turmo IIIC4: ;Turmo IIIC5: ;Turmo IIIC6: ;Turmo IIIC7: ;Turmo IIID:Turboprop for the proposed Breguet Br 942 STOL transport, maximum rating . ;Turmo IIID2: at 22,460 free turbine rpm ;Turmo IIID3: at 33,500 rpm ;Turmo IVB: ;Turmo IVC: ;Turmo IV-CA:Licence production in Romania ;Turmo VI:Turboprop engine with two axial stages, one centrifugal compressor stage and two free power turbine stages, rated at at 32,000 rpm. ;WZ-6:Licence production at the Changzhou Lan Xiang Machinery Works in the Peoples Republic of China. 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Turbomeca Turmo」の詳細全文を読む スポンサード リンク
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