Door-type thrust reverser of a jet turbine engine with doors...

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

Patent

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F02K 1/54 (2006.01) F02K 1/70 (2006.01)

Patent

CA 2231933

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 deflecting obstructions after pivoting creating reverse thrust. A door (7) consists of a panel (23) forming the external structure and of an internal structure (22) which are mechanical separate and linked by a joining component formed of at least one elastic link (25, 26).

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) du flux de soufflante et constituant des obstacles de déviation après pivotement en procurant une inversion de poussée. Une porte (7) est constituée d'un panneau (23) formant la structure externe et d'une structure interne (22) qui sont mécaniquement dissociées et reliées par une jonction formée d'au moins une liaison élastique (25,26).

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