| 词条 | Turbomeca Piméné | ||||||||||||||
| 释义 |
The Turbomeca Piméné was a small French turbojet engine produced by Turbomeca in the early 1950s.[1] First shown at the 1949 Paris Air Show this engine passed official type tests in 1950.[2] A variant known as the Turbomeca Orédon drove an alternator and was used as an aircraft auxiliary power unit, this name being reused for a later helicopter turboshaft design.[1] Applications
Specifications{{jetspecs||ref=Aircraft engines of the World 1953 [3] |type=Turbojet |length={{cvt|880|mm}} |diameter={{cvt|408|mm}} |weight={{cvt|54|kg}} |compressor=Single stage axial plus single-stage centrifugal |combustion=Single annular combustion chamber |turbine=Single-stage |fueltype=Kerosene |oilsystem=Dry sump with Turbomeca gear pump at {{cvt|43|psi|bar|order=flip}} |power= |thrust= Take-off: {{cvt|240|lbf|kN|order=flip}} at 36,000 rpm / sea level Max Continuous: {{cvt|200|lbf|kN|order=flip}} at 34,000 rpm / sea level Cruising: {{cvt|175|lbf|kN|order=flip}} at 33,000 rpm / sea level |compression=4:1 |aircon={{cvt|2|kg/s|lb/s}} |turbinetemp= Before turbine:{{cvt|850|C|F K}} After turbine:{{cvt|700|C|F K}} |fuelcon= |specfuelcon={{cvt|1.062|lb/lbf/h|kg/kN/h|order=flip}} |power/weight= |thrust/weight={{cvt|2|lbf/lb|kN/kg|order=flip}} }} See also{{Aircontent|related= |similar engines= |lists=
|see also= }} References
1. ^1 Gunston 1989, p. 170. 2. ^Flight - Type test of the Turbomeca Piméné www.flightglobal.com Retrieved: 14 June 2012 3. ^{{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=160-161}}
External links
3 : Turbomeca aircraft engines|Turbojet engines 1940–1949|Mixed-compressor gas turbines |
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