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1. (WO2007051444) MULTISTAGE COMPRESSOR FOR A GAS TURBINE, COMPRISING DISCHARGE PORTS AND INJECTION PORTS TO STABILIZE THE COMPRESSOR FLOW

Pub. No.:    WO/2007/051444    International Application No.:    PCT/DE2006/001889
Publication Date: 2007-5-10 International Filing Date: 2006-10-26
IPC: F01D 5/14
F04D 29/68
F04D 27/02
Applicants: MTU AERO ENGINES GMBH
GRAUER, Frank
Inventors: GRAUER, Frank
Title: MULTISTAGE COMPRESSOR FOR A GAS TURBINE, COMPRISING DISCHARGE PORTS AND INJECTION PORTS TO STABILIZE THE COMPRESSOR FLOW
Abstract:
Disclosed is a multistage compressor (1) for a gas turbine, comprising a compressor housing (2), guide vanes (7), impeller vanes (6), a hub area (3), discharge ports (5), and injection ports (4) to stabilize the compressor. The inventive multistage compressor is characterized in that the discharge ports (5) are disposed at least one stage downstream of the injection ports (4), thus solving the problems of prior art while making it possible to significantly increase efficiency and reduce the engine weight.