发明名称 |
A gas turbine engine system and an associated method thereof |
摘要 |
A gas turbine engine system (10) includes a compressor (14), a combustor (16), and a turbine (22). The combustor is coupled to the compressor and disposed downstream of the compressor. The combustor includes a secondary combustor section (20) coupled to a primary combustor section (18) and disposed downstream of the primary combustor section (18). The combustor also includes a transition nozzle (28) coupled to the secondary combustor section and disposed downstream of the secondary combustor section. The combustor further includes an injector (58) coupled to the secondary combustor section, for injecting an air-fuel mixture to the secondary combustor section. The turbine (22) is coupled to the combustor (16) and disposed downstream of the transition nozzle (28); wherein the transition nozzle is oriented substantially tangential to the turbine (22). |
申请公布号 |
EP2738355(B1) |
申请公布日期 |
2016.09.14 |
申请号 |
EP20130194988 |
申请日期 |
2013.11.29 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
HAYNES, JOEL MEIER;JOSHI, NARENDRA DIGAMBER;CHEN, HUIJUAN |
分类号 |
F01D9/02;F23R3/34 |
主分类号 |
F01D9/02 |
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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