Compressor and gas turbine engine with a plasma actuator

Details Compressor and gas turbine engine with a plasma actuator Compressor and gas turbine engine with a plasma actuator

F - Mech Eng,Light,Heat,Weapons

04

D

F04D 27/02 (2006.01) F04D 27/00 (2006.01) F04D 29/52 (2006.01) F15D 1/12 (2006.01)

Patent

CA 2710007

A compression system is disclosed, the compression system comprising a rotor having a plurality of blades arranged around a centerline axis, each blade having a blade airfoil and a blade tip, and at least one plasma actuator located on a blade. Exemplary embodiments of a detection system for detecting an instability in a compression system rotor and a mitigation system comprising at least one plasma actuator mounted on a blade to facilitate the improvement of the stability of the rotor are disclosed.

L'invention concerne un système de compression comportant un rotor ayant une pluralité de pales agencée autour d'un axe central, chaque pale ayant une surface portante de pale et un embout de pale, et au moins un actionneur de plasma situé sur une pale. Des exemples de modes de réalisation d'un système de détection pour détecter une instabilité dans un rotor de système de compression et un système d'atténuation comprenant au moins un actionneur de plasma monté sur une pale pour faciliter l'amélioration de la stabilité du rotor sont révélés.

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