Plasma enhanced compressor duct

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 5/14 (2006.01) F01D 9/04 (2006.01) F04D 29/54 (2006.01) F04D 29/68 (2006.01) F15D 1/12 (2006.01)

Patent

CA 2749132

A compression system is disclosed, comprising a first compressor having a first flowpath, a second compressor having a second flowpath located axially aft from the first compressor, and a transition duct capable of flowing an airfow from the first compressor to the second compressor, the transition duct having at least one plasma actuator mounted in the transition duct.

Linvention concerne un système de compression comprenant un premier compresseur présentant une première trajectoire, un second compresseur présentant une seconde trajectoire situé axialement vers larrière depuis le premier compresseur, et un conduit de transition permettant lécoulement dair du premier compresseur vers le second compresseur, le conduit de transition comprenant au moins un actionneur plasma monté dans le conduit de transition.

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