B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 33/08 (2006.01) B64D 33/10 (2006.01) F02C 7/14 (2006.01) F02C 7/18 (2006.01)
Patent
CA 2226424
The invention concerns a turboprop engine comprising an oil cooler (5) which is disposed in the engine pod (1) and upon which cooling air acts. The oil cooler (5) is disposed in a flow duct (6) which at the rear opens into the environment and at the front can be connected alternately to an air-inlet opening (7) or to the feed duct (11) of the compressor (2) of the aircraft gas turbine.
L'invention concerne un turbo-propulseur présentant un refroidisseur d'huile (5), sur lequel agit de l'air de refroidissement, et disposé dans une nacelle (1). Ce refroidisseur d'huile est disposé dans un canal de flux (6), lequel, à l'arrière, débouche dans l'environnement et, à l'avant, peut être relié soit à un orifice d'admission d'air (7), soit au canal d'admission de flux (11) du compresseur (2) de la turbine à gaz de l'aéronef.
Bmw Rolls-Royce Gmbh
Goudreau Gage Dubuc
Rolls-Royce Deutschland Ltd & Co Kg
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