Thrust reverser for a jet engine

F - Mech Eng,Light,Heat,Weapons – 02 – K

Patent

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F02K 1/72 (2006.01) F02K 1/70 (2006.01)

Patent

CA 2680485

The invention relates to a thrust reverser (9) for an aircraft nacelle (1), including: a front frame (11), a cowl (21) which can move between an operating position and an intermediate maintenance position downstream of the front frame (11), means (26) for moving the cowl (21) between closed and open positions, and an inner structure (23) which can move between an operating position and an intermediate maintenance position downstream of the front frame (11). In addition, the cowl (21) comprises two half-cowls (21a, 21b) and the inner structure (23) comprises two structure halves (23a, 23b), whereby said half-cowls (21a, 21b) and said inner structure halves (23a, 23b) can open outward when the cowl (21) and the inner structure (23) are in the intermediate maintenance position.

Cet inverseur de poussée (9) pour nacelle d'avion (1) comprend : un cadre avant (11), un capot mobile (21) entre une position de fonctionnement et une position intermédiaire de maintenance située en aval dudit cadre avant (11), des moyens (26) pour déplacer ledit capot (21) entre des positions fermée et ouverte, une structure interne (23) mobile entre une position de fonctionnement et une position intermédiaire de maintenance située en aval dudit cadre avant (11). En outre, ledit capot (21) comprend deux demi-capots (21a, 21b) et ladite structure interne (23) comprend deux demi-structures internes (23a, 23b), ces demi-capots (21a, 21b) et ces demi-structures internes (23a, 23b) sont aptes à s'ouvrir vers l'extérieur lorsque ledit capot (21) et ladite structure interne (23) se trouvent en position intermédiaire de maintenance.

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