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- Turbomeca_Turmo abstract "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".
- Turbomeca_Turmo wikiPageExternalLink sous_famille_home.php?sfid=512&mid=615.
- Turbomeca_Turmo wikiPageID "10208655".
- Turbomeca_Turmo wikiPageRevisionID "585022857".
- Turbomeca_Turmo aircon "6.2".
- Turbomeca_Turmo combustion "Annular, reverse-flow".
- Turbomeca_Turmo compression "5.9".
- Turbomeca_Turmo compressor "Single-stage axial, single-stage centrifugal".
- Turbomeca_Turmo developedInto Bristol_Siddeley_Nimbus.
- Turbomeca_Turmo diameter "71.6".
- Turbomeca_Turmo hasPhotoCollection Turbomeca_Turmo.
- Turbomeca_Turmo length "182.0".
- Turbomeca_Turmo lists "*List of aircraft engines".
- Turbomeca_Turmo majorApplications Aérospatiale_Puma.
- Turbomeca_Turmo majorApplications Aérospatiale_Super_Frelon.
- Turbomeca_Turmo manufacturer Turbomeca.
- Turbomeca_Turmo power "1217.0".
- Turbomeca_Turmo weight "3.74".
- Turbomeca_Turmo ref "Flight International.".
- Turbomeca_Turmo turbine "Two-stage compressor turbine, two-stage power turbine".
- Turbomeca_Turmo type Turboprop.
- Turbomeca_Turmo type Turboshaft.
- Turbomeca_Turmo type "Two-shaft turboshaft".
- Turbomeca_Turmo weight "325.0".
- Turbomeca_Turmo subject Category:Turbomeca_aircraft_engines.
- Turbomeca_Turmo subject Category:Turboshaft_engines_1950–1959.
- Turbomeca_Turmo type AircraftEngine102687423.
- Turbomeca_Turmo type Artifact100021939.
- Turbomeca_Turmo type Device103183080.
- Turbomeca_Turmo type Engine103287733.
- Turbomeca_Turmo type Instrumentality103575240.
- Turbomeca_Turmo type Machine103699975.
- Turbomeca_Turmo type Motor103789946.
- Turbomeca_Turmo type Object100002684.
- Turbomeca_Turmo type PhysicalEntity100001930.
- Turbomeca_Turmo type TurbomecaAircraftEngines.
- Turbomeca_Turmo type Whole100003553.
- Turbomeca_Turmo comment "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".
- Turbomeca_Turmo label "Turbomeca Turmo".
- Turbomeca_Turmo label "Turbomeca Turmo".
- Turbomeca_Turmo label "Turbomeca Turmo".
- Turbomeca_Turmo label "チュルボメカ テュルモ".
- Turbomeca_Turmo sameAs Turbomeca_Turmo.
- Turbomeca_Turmo sameAs Turbomeca_Turmo.
- Turbomeca_Turmo sameAs チュルボメカ_テュルモ.
- Turbomeca_Turmo sameAs m.02q586f.
- Turbomeca_Turmo sameAs Q847984.
- Turbomeca_Turmo sameAs Q847984.
- Turbomeca_Turmo sameAs Turbomeca_Turmo.
- Turbomeca_Turmo wasDerivedFrom Turbomeca_Turmo?oldid=585022857.
- Turbomeca_Turmo isPrimaryTopicOf Turbomeca_Turmo.