F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/54 (2006.01) F02K 1/70 (2006.01)
Patent
CA 2231942
A dual-flow thrust reverser of a jet turbine engine comprises pivoting doors (7) integral in forward thrust with the outer wall of the flow duct (15) of the fan and constituting obstructions to deflect flow and create reverse thrust. The door (7) consists of a panel (23) forming the external structure and of an internal structure (22) linked by a local structural link zone (25), the remainder of the external structures (23) and internal structures (22) being independent. The lock (27) securing the door (7) in the closed position is mounted in the said structural zone (25).
Un inverseur de poussée de turboréacteur à double flux comporte des portes pivotantes (7) intégrées en jet direct dans la paroi extérieure du conduit (15) de flux de soufflante et constituant des obstacles de déviation de flux en procurant une inversion de poussée. La porte (7) est constituée d'un panneau (23) formant structure externe et d'une structure interne (22) reliées par une zone de liaison structurale locale (25), le reste des structures externe (23) et interne (22) étant indépendantes. Le verrou (27) de maintien de la porte (7) en position fermée est installé dans ladite zone structurale (25).
Gonidec Patrick
Rouyer Pascal Gerard
Vauchel Guy Bernard
Goudreau Gage Dubuc
Hispano-Suiza Aerostructures
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