Aircraft propulsion system

Details Aircraft propulsion system Aircraft propulsion system

B - Operations, Transporting

64

D

B64D 27/26 (2006.01) B64D 29/00 (2006.01)

Patent

CA 2728743

Aircraft propulsion system (10) comprising a bypass turbojet engine which is surrounded by a nacelle, and means (80) of attaching the engine to a pylon (16) of an aircraft, the nacelle (12) comprising an internal structure exhibiting symmetry of revolution with a rigid framework formed of an upstream annular frame (50) attached to an intermediate casing (38) of the engine, of a downstream annular frame (52) supporting the exhaust casing (40) of the engine, and of longitudinal arms (54, 56, 58, 60) connecting these frames (50, 52), the downstream annular frame (52) being fixed to the pylon (16) by resilient or articulated suspension means.

Système propulsif d'aéronef (10), comprenant un moteur à turboréacteur à double flux entouré par une nacelle, et des moyens (80) d'accrochage du moteur à un mât (16) d'un aéronef, la nacelle (12) comprenant une structure interne de révolution à ossature rigide formée d'un cadre annulaire amont (50) fixé à un carter intermédiaire (38) du moteur, d'un cadre annulaire aval (52) supportant le carter d'échappement (40) du moteur, et de bras longitudinaux (54, 56, 58, 60) de liaison de ces cadres (50, 52), le cadre annulaire aval (52) étant fixé au mât (16) par des moyens de suspension souple ou articulée.

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