Societe Hispano Suiza

Societe De Constructio Des Avions Hurel-dubois

Jean-Paul Rene Hogie

Robert R Standish

Pascal Gerard Rouyer

Felix Carimali

Xavier Raymond Lore

Guy B Vauchel

A linkage system is disclosed for releasably latching a thrust reverser to an engine casing having a longitudinal axis, the linkage system having a seat on the thrust reverser and a movable latching member on the engine casing movable between an open position in which the latching member is displaced away from the seat, and a closed position in which the latching member is located adjacent to the seat so as to prevent displacement of the thrust reverser away from the engine casing.

Linkage system for an aircraft turbojet engine

A thrust reverser door for a turbofan-type turobjet engine thrust reversing system is disclosed defining a gas flow passage between inner and outer panels of the door. The passae has an inlet formed through the inner panel of the thrust reverser door and an outlet, directs a portion of the gas flowing through a cold flow air duct in a forward direction. The gas flowing in the forward direction inpinges upon gases flowing through a laterally facing opening in the housing in order to provide a forward component to this gas flow. A moveable flap may be attached to the thrust reverser door in order to cover the inlet to the passageway when the device is operated in the forward thrust mode.

Thrust reverser door having an exhaust gas passage

Growing community of inventors

Le Havre, France

Jean-Paul Rene Hogie