Title:
ガスタービンエンジン推力を発生するための方法及び装置
Document Type and Number:
Japanese Patent JP4471644
Kind Code:
B2
Abstract:
A pulse detonation system (12) for a gas turbine engine (10) includes a core engine (30). The pulse detonation system is downstream from the core engine and is configured to create a temperature rise and a pressure rise within the gas turbine engine and to increase engine thrust. The pulse detonation system comprises a multi-staged pulse detonation augmentor (60) that comprises a predetonator (48) operable with at least a first operating stage wherein a less-than-stoichiometric fuel-air mixture is provided to the predetonator.
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Inventors:
John Michael Cochofer
Application Number:
JP2003421876A
Publication Date:
June 02, 2010
Filing Date:
December 19, 2003
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F02C5/10; F02K1/00; F02K3/075; F02K3/08; F02K7/04; F02K7/06; F02K7/075; F23R7/00
Domestic Patent References:
JP29006654B1 | ||||
JP2001355515A | ||||
JP1134029A | ||||
JP8135504A |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Nobukazu Ito
Hirokazu Ogura
Nobukazu Ito