B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 29/06 (2006.01) B64C 7/02 (2006.01)
Patent
CA 2657402
The invention relates to an engine unit for aircraft, comprising an engine, an engine mounting device (4), a cowling enclosing the engine, provided with an air intake (32) and fan shrouds, the unit comprising a support cradle (40) for the fan shrouds fixed to the mounting device or to an assembly comprising a fan housing and the air intake, fixed to said housing. According to the invention, the engine unit has more than one aerodynamic coupling fairing (33) with first mounting means fixed to the cradle (40) and second mounting means fixed to other of the elements on the mounting device (4) and said unit.
La présente invention se rapporte à un ensemble moteur pour aéronef comprenant un moteur, un dispositif d'accrochage du moteur (4) ainsi qu'une nacelle entourant le moteur et pourvue d'une entrée d'air (32) et de capots de soufflante, cet ensemble comprenant un berceau (40) de support des capots de soufflante, monté fixement sur le dispositif d'accrochage ou bien sur une entité comportant un carter de soufflante et l'entrée d'air fixée sur ce carter. Selon l'invention, l'ensemble moteur dispose de plus d'un capotage aérodynamique de jonction (33) équipé de premiers moyens d' accrochage montés sur le berceau (40), et également équipé de seconds moyens d'accrochage montés sur l'autre des éléments parmi le dispositif d'accrochage (4) et ladite entité.
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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