Air intake for an aeroplane engine with unducted propellers

Air intake for an aeroplane engine with unducted propellers

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...

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Bibliographische Detailangaben
1. Verfasser: BENSILUM STEPHANE EMMANUEL DANIEL
Format: Patent
Sprache:chi ; eng
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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.