Title:
ガスタービンエンジンを運転するための方法及び装置
Document Type and Number:
Japanese Patent JP4562129
Kind Code:
B2
Abstract:
A gas turbine engine (10), including a first compressor (14), a second compressor (16), and a turbine (20), coupled together in serial flow arrangement. The operation includes channeling compressed airflow (53) discharged from the first compressor through an intercooler (50) having a cooling medium flowing therethrough, operating the intercooler such that condensate is formed in the intercooler from the compressed airflow, and channeling the condensate to an inlet (26,30) of the first or second compressor to facilitate reducing an operating temperature of the gas turbine engine.
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Inventors:
Michael joseph real
Narendra Digger Joshi
David Paul Wolf
Narendra Digger Joshi
David Paul Wolf
Application Number:
JP2005021071A
Publication Date:
October 13, 2010
Filing Date:
January 28, 2005
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
A63B71/06; A63B63/00; F01D25/32; F02C7/143; F02C3/30; G01B11/00; G06T1/00; G06T7/00; G06T7/60
Domestic Patent References:
JP9166028A | ||||
JP5187359A | ||||
JP56162227A |
Foreign References:
US20050252231 |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Nobukazu Ito
Toshihisa Kurokawa
Hirokazu Ogura
Nobukazu Ito
Toshihisa Kurokawa