Chevron-type primary exhaust nozzle for aircraft turbofan...

Details Chevron-type primary exhaust nozzle for aircraft turbofan... Chevron-type primary exhaust nozzle for aircraft turbofan...

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/09 (2006.01) B64D 33/04 (2006.01) F02K 1/34 (2006.01) F02K 1/38 (2006.01) F02K 1/40 (2006.01) F02K 1/48 (2006.01)

Patent

CA 2501766

A primary exhaust nozzle for a turbofan engine of the double, separated air-flow type for aircraft comprises: an inner coat, within which there circulates a primary air flow (FP), comprising chevrons at an external end and an outer coat at least partially surrounding the inner coat and along which there flows a secondary air flow (FS), the outer coat being mobile along the inner coat. Also disclosed is an aircraft comprising such an exhaust nozzle.

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