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Title:
プラズマ圧縮機
Document Type and Number:
Japanese Patent JP2011508149
Kind Code:
A
Abstract:
A gas turbine engine is disclosed, comprising a compressor having a circumferential row of blades, a casing surrounding the tips of the blades, located radially apart from the tips of the blades and at least one plasma generator located on the casing. The plasma generator comprises a first electrode and a second electrode separated by a dielectric material. The gas turbine engine further comprises an engine control system which controls the operation of the plasma generator such that the stable operating range of the compressor is increased.

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Inventors:
Wadia, Aspi Rusthom
Clark, David Scott
Lee, Chimp
Breeze String Fellow, Andrew
McNulty, Gregory Scott
Application Number:
JP2010540726A
Publication Date:
March 10, 2011
Filing Date:
December 05, 2008
Export Citation:
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Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F04D27/00; F04D27/02; F04D29/00; F04D29/52; F04D29/66; H05H1/24
Domestic Patent References:
JP2007317656A2007-12-06
Foreign References:
WO2005114013A12005-12-01
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa