Propulsion assembly for aircraft with sliding nacelle

Details Propulsion assembly for aircraft with sliding nacelle Propulsion assembly for aircraft with sliding nacelle

B - Operations, Transporting

64

D

B64D 29/08 (2006.01) B64D 33/04 (2006.01) F02K 1/72 (2006.01)

Patent

CA 2689111

The invention relates to a propulsion assembly (1) for an aircraft including a turbojet engine (2), a turbojet fixation mast (4) and a nacelle (3) mounted on the fixation mast and surrounding the turbojet engine. According to the invention, the nacelle includes at least one mobile nacelle portion (40) defining a single-piece envelope about a section of the turbojet engine, said mobile nacelle portion (40) being mounted so as to slide on the fixation mast and to be moved from the front to the rear and conversely.

L'invention se rapporte à un ensemble moteur (1) pour aéronef comprenant un turboréacteur (2), un mât d'accrochage (4) du turboréacteur, ainsi qu'une nacelle (3) montée sur le mât d'accrochage et entourant le turboréacteur. Selon l'invention, la nacelle comporte au moins une portion de nacelle mobile (40) formant enveloppe d'un seul tenant tout autour d'une section du turboréacteur, cette portion de nacelle mobile (40) étant montée coulissante sur le mât d'accrochage de manière a pouvoir être déplacée de l'avant vers l'arrière, et inversement.

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