| 词条 | Turbomeca Marboré | ||||||||||||||
| 释义 |
The Turbomeca Marboré is a small turbojet engine that was produced by Turbomeca from the 1950s into the 1970s. The most popular uses of this engine were in the Fouga CM.170 Magister and the Morane-Saulnier MS.760 Paris. It was also licensed for production in the United States as the Teledyne CAE J69.[1] The original Marboré, as well as Marboré III, IV, and V were not produced in significant numbers. A typical weight for this series of engines is {{convert|140|kg|abbr=on}}. Fuel consumption is {{convert|720|L/h|abbr=on}} on the Marboré VI at {{convert|4500|m|abbr=on}}, as compared to {{convert|520|L/h|abbr=on}} on Marboré II engines (same altitude). An increase of 27% fuel consumption and a decrease in cruise range capabilities.[2] Variants
Teledyne CAE J69: Licence production and development in the United States. Applications
See Teledyne CAE J69 Specifications (Marboré II){{jetspecs||ref=FAA TCDS[3], Aircraft engines of the World 1953[4] |type=Turbojet |length={{cvt|1064|mm}} |diameter={{cvt|567|mm}} |weight={{cvt|133|kg}} |compressor=Single-stage centrifugal |combustion=Annular combustion chamber |turbine=Single-stage axial flow |fueltype=Aviation kerosene Air 3405 (JP-1) |oilsystem=Dry sump, Turbomeca gear pump at {{cvt|70|psi|bar|order=flip}} |power= |thrust= Take-off:{{cvt|880|lbf|kN|order=flip}} at 22,600 rpm / sea level Max continuous:{{cvt|705|lbf|kN|order=flip}} at 21,000 rpm / sea level |compression=4:1 |aircon={{cvt|7.6|kg}} |turbinetemp= Before turbine:{{cvt|800|C|F K}} After turbine:{{cvt|610|C|F K}} |fuelcon= |specfuelcon={{cvt|1.08|lb/lbf/h|kg/kN/h|order=flip}} |power/weight= |thrust/weight={{cvt|3.03|lbf/lb|kN/kg|order=flip}} }} See also{{Aircontent|related=
|similar engines= |lists=
|see also= }} References1. ^Gunston 1989, p.169. 2. ^CM-170 Flight Tests, Airplane Cruise Performance Charts, and Aircraft Flight Manuals 3. ^FAA Type Certificate Data Sheet Retrieved: 2 November 2008 4. ^{{cite book |last=Wilkinson |first=Paul H. |title=Aircraft engines of the World 1953 |year=1953 |publisher=Sir Isaac Pitman & Sons Ltd. |location=London |edition=11th |pages=164-165}}
External links{{Commons category}}
3 : Turbomeca aircraft engines|Turbojet engines 1950–1959|Centrifugal-flow turbojet engines |
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