Turbomeca Piméné
(Redirected from Turboméca Piméné)
| Piméné | |
|---|---|
| Type | Turbojet |
| National origin | France |
| Manufacturer | Turbomeca |
| First run | 1948 |
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 similar, but not directly related, smaller turboshaft, known as the Turbomeca Orédon, drove an alternator and was used as an aircraft auxiliary power unit,[3]
Variants
[edit]- TR-011
- small 0.785 kN (176 lbf) turbojet engine, precursor to the Orédon APU.[4][5]
- Piméné
- enlarged 1.079 kN (243 lbf) higher mass flow development of the TR-011 / Orédon.[5]
Applications
[edit]Specifications
[edit]Data from Aircraft engines of the World 1953,[6] Aircraft engines of the World 1950[4]
General characteristics
- Type: turbojet
- Length: 880 mm (35 in) (1,094 mm (43.1 in) with exhaust duct
- Diameter: 408 mm (16.1 in)
- Dry weight: 54 kg (119 lb)
Components
- Compressor: single-stage centrifugal compressor with 14 vanes
- Combustors: single annular combustion chamber
- Turbine: single-stage
- Fuel type: kerosene
- Oil system: dry sump with Turbomeca gear pump at 3.0 bar (43 psi)
Performance
- Maximum thrust:
- Take-off: 1.1 kN (240 lbf) at 36,000 rpm / sea level
- Max continuous: 0.89 kN (200 lbf) at 34,000 rpm / sea level
- Cruising: 0.78 kN (175 lbf) at 33,000 rpm / sea level
- Overall pressure ratio: 4:1
- Air mass flow: 2 kg/s (4.4 lb/s) at 36,000 rpm at sea level
- Turbine inlet temperature:
- Before turbine: 850 °C (1,560 °F; 1,120 K)
- After turbine: 700 °C (1,292 °F; 973 K)
- Specific fuel consumption: 108.3 kg/kN/h (1.062 lb/lbf/h)
- Thrust-to-weight ratio: 2.077 at take-off thrust
See also
[edit]Related lists
References
[edit]- Notes
- ^ Gunston 1989, p. 170.
- ^ Flight - Type test of the Turbomeca Piméné www.flightglobal.com Retrieved: 14 June 2012
- ^ Wilkinson, Paul H. (1950). Aircraft engines of the World 1950 (8th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 37.
- ^ a b Wilkinson, Paul H. (1950). Aircraft engines of the World 1950 (8th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 112–113.
- ^ a b "AAPHT - La naissance de Turbomeca". www.amis-turbomeca.com (in French). Retrieved 16 January 2020.
- ^ Wilkinson, Paul H. (1953). Aircraft engines of the World 1953 (11th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 160–161.
- Bibliography
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Kay, Anthony L. (2007). Turbojet History and Development 1930-1960 Volume 2:USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary (1st ed.). Ramsbury: The Crowood Press. ISBN 978-1861269393.