Engine exhaust system

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 33/04 (2006.01) F02K 1/00 (2006.01)

Patent

CA 2654751

An exhaust system for an aircraft has a primary exhaust duct for communicating exhaust gas from an engine exhaust exit and is configured for movement with the engine. A secondary exhaust duct is in fluid communication with the primary exhaust duct and is movably mounted to the airframe. The system has means for maintaining a generally consistent relative alignment between the primary duct and the secondary duct.

L'invention concerne un système d'échappement pour avion qui comprend un conduit d'échappement principal pour véhiculer le gaz d'échappement depuis la sortie d'échappement du moteur. Il est configuré pour se déplacer avec le moteur. Un conduit d'échappement secondaire est en communication fluidique avec le conduit d'échappement principal et est monté de manière mobile sur la cellule. Le système est doté de moyens pour maintenir un alignement relatif généralement constant entre le conduit principal et le conduit secondaire.

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