Pivoting door thrust reverser for a turbofan gas turbine engine

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

Patent

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F02K 1/56 (2006.01)

Patent

CA 2638842

A pivot arrangement for a thrust reverser door of a gas turbine engine, the pivot fitting having a base and a shaft projecting from a main side of the base. The shaft receives a preferably curved pivot arm of the door to provide a low profile arrangement which improves performance when the doors are stowed.

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