Gas turbine compressor

Details Gas turbine compressor Gas turbine compressor

F - Mech Eng,Light,Heat,Weapons

04

D

F04D 27/02 (2006.01)

Patent

CA 2720172

A gas turbine compressor, comprising a compressor housing (2), guide vanes (4), and rotor blades (8), has valve-controlled blow-in openings (10) for stabilizing the compressor now by means of air that is blown in. The air flow is detected by means of pressure sensors (20, 22) and the valves (16) are controlled as a function thereof.

L'invention concerne un compresseur de turbine à gaz muni d'un carter de compresseur (2), d'aubes directrices (4), ainsi que d'aubes mobiles (8). Le compresseur selon l'invention présente des ouvertures d'insufflation (10) commandées par soupape et servant à stabiliser l'écoulement du compresseur au moyen d'air insufflé. L'écoulement d'air est détecté au moyen de capteurs de pression (20, 22), les soupapes (16) étant commandées en fonction de la pression déterminée.

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