Thrust reverser for a turbofan gas turbine engine

Details Thrust reverser for a turbofan gas turbine engine Thrust reverser for a turbofan gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/56 (2006.01)

Patent

CA 2638840

The thrust reverser includes, in one aspect, an interior flow deflector which defines a portion of a substantially continuous and uninterrupted nozzle interior surface with the interior of a jet pipe when the door is in a stowed position, thereby reducing aerodynamic losses and improving efficiency. In another aspect, improved sealing arrangement between the jet pipe and the door provides increased performance when the doors are stowed.

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