Air intake for an aeroplane engine with unducted propellers

Details Air intake for an aeroplane engine with unducted propellers Air intake for an aeroplane engine with unducted propellers

B - Operations, Transporting

64

D

B64D 27/14 (2006.01) B64D 29/04 (2006.01) B64D 33/02 (2006.01)

Patent

CA 2743009

Air intake (113) for an aeroplane engine of the type with unducted propellers, which intake is intended to be connected by a pylon (134) to the fuselage of an aeroplane, the local length of this air intake, measured parallel to the axis (A) of the engine between a point on the leading edge (138) of the air intake and a transverse plane (P) situated at an inlet impeller of the engine compressor, is longer (Lmax) in the region (142) of the air intake connected to the pylon and shorter (Lmin) in the region of the air intake opposite the pylon.

Entrée d'air (113) d'un moteur d'avion du type à hélices propulsives non carénées, destinée à être reliée par un pylône (134) au fuselage d'un avion, la longueur locale de cette entrée d'air, mesurée parallèlement à l'axe (A) du moteur entre un point du bord d'attaque (138) de l'entrée d'air et un plan transversal (P) situé au niveau d'une roue d'entrée du compresseur du moteur, est plus grande (Lmax) dans la zone (142) de l'entrée d'air reliée au pylône et plus faible (Lmin) dans la zone de l'entrée d'air

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