Thrust reverser

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

Patent

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Details

F02K 1/56 (2006.01)

Patent

CA 2639079

The thrust reverser is used with an aircraft gas turbine engine and includes upper and lower doors pivotable between a stowed position and a deployed position. When deployed, the doors redirect a portion of the efflux to generate a nose-down pitching moment on an aircraft to improve handling during thrust reversing on a runway.

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