F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
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.
Feuillard Philippe
Gerri Christian
Hemeury Philippe
Airbus France
Airbus Operations Sas
Bcf Llp
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