Door-type turbojet thrust reverser incorporating a sliding...

Details Door-type turbojet thrust reverser incorporating a sliding... Door-type turbojet thrust reverser incorporating a sliding...

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/70 (2006.01)

Patent

CA 2210509

A turbojet engine thrust reverser comprising pivoting doors (7), integrated into the outside wall of the duct in the stowed position and forming obstacles to create reverse thrust when deployed. Each door (7) consists of a pivoting flap (20) and a panel (21) that is superimposed over the flap (20) for undeflected thrust but can slide in relation to the flap so as to help divert the gas flow for reverse thrust.

Un inverseur de poussée de turboréacteur comporte des portes (7) pivotantes, intégrées en jet direct dans la paroi extérieure du conduit de flux et formant des obstacles de déviation en jet inversé. Chaque porte (7) est constituée d'un volet pivotant (20) et d'un panneau (21) disposé en superposition avec le volet (20) en jet direct et susceptible de coulisser par rapport au volet de manière à contribuer à la déviation du flux inversé.

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