发明名称 |
METHODS AND APPARATUS FOR GENERATING GAS TURBINE ENGINE THRUST |
摘要 |
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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申请公布号 |
CA2452972(C) |
申请公布日期 |
2010.01.26 |
申请号 |
CA20032452972 |
申请日期 |
2003.12.11 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
KOSHOFFER, JOHN MICHAEL |
分类号 |
F02C5/10;F02K3/10;F02K1/00;F02K3/02;F02K3/075;F02K3/08;F02K7/04;F02K7/06;F02K7/075;F23R7/00 |
主分类号 |
F02C5/10 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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