F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/70 (2006.01)
Patent
CA 2612117
The invention concerns a pod (1) for an aircraft comprising a cowling (5), an engine (6) housed in the inner volume of the cowling, an annular channel (9) circulating a secondary thrust flow arranged between the engine and the cowling, and at least one thrust reverser (2) for forming a reverse flow from the secondary thrust flow circulating in the annular channel. The thrust reverser comprising a plurality of doors (10) provided in the rear part (7) of the cowling, so as to form a trailing edge of the cowling. The thrust reverser can comprise means for actuating the doors such that at least one actuating means actuates two adjacent doors and at least one door is actuated by two actuating means.
L'invention concerne une nacelle (1) pour aéronef comprenant un capot (5), un moteur (6) logé dans un volume interne du capot, un canal (9) annulaire d'écoulement d'un flux de poussée secondaire ménagé entre Ie moteur et le capot, et au moins un inverseur de poussée (2) pour la formation d'un flux inverse à partir du flux de poussée secondaire circulant dans le canal annulaire. L'inverseur de poussée comporte une pluralité de portes (10) ménagées dans une partie arrière (7) du capot, de manière à former un bord de fuite dudit capot. L'inverseur de poussée peut comporte des moyens d'actionnement des portes tels qu'au moins un moyen d'actionnement actionne deux portes adjacentes et au moins une porte est actionnée par deux moyens d'actionnement.
Airbus France
Airbus Operations Sas
Bcf Llp
LandOfFree
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