发明授权
- 专利标题: Gas turbine combustor and methodd of operating the same
- 专利标题(中): 燃气轮机及其运行方法
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申请号: US470596申请日: 1990-01-26
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公开(公告)号: US5121597A公开(公告)日: 1992-06-16
- 发明人: Haruo Urushidani , Seiichi Kirikami , Isao Sato , Nobuo Shimizu , Osamu Arai , Akira Shimura , Michio Kuroda , Tsuguaki Koga , Tadashi Kurokawa , Yoji Ishibashi , Katsukuni Hisano
- 申请人: Haruo Urushidani , Seiichi Kirikami , Isao Sato , Nobuo Shimizu , Osamu Arai , Akira Shimura , Michio Kuroda , Tsuguaki Koga , Tadashi Kurokawa , Yoji Ishibashi , Katsukuni Hisano
- 申请人地址: JPX Tokyo
- 专利权人: Hitachi, Ltd.
- 当前专利权人: Hitachi, Ltd.
- 当前专利权人地址: JPX Tokyo
- 优先权: JPX1-23884 19890203
- 主分类号: F02C7/26
- IPC分类号: F02C7/26 ; F02C9/34 ; F23C99/00 ; F23R3/16 ; F23R3/20 ; F23R3/26 ; F23R3/34
摘要:
A gas turbine combustor and a method of operating the gas turbine combustor, with the gas turbine combustor comprising a combustion sleeve, a combustion sub-chamber disposed at an upstream side of the combustion sleeve and having an air and fuel supply system, and a combustion main chamber disposed on a downstream side of the sub-chamber and having an air and fuel supply system. The combustion sub-chamber and combustion main chamber are formed in such a manner that the start-up of the gas turbine is effected by the hot combustion gas generated in the sub-chamber. The combustion sub-chamber is provided with an inner sleeve protruding from a side wall of the sub-chamber such that a tip of the inner sleeve is located in the vicinity of a downstream end of the sub-chamber, and a fuel nozzle is provided in a tip of the inner sleeve for increasing the fuel-to-air ratio during an initiating period of an increase in the gas turbine rotation speed.
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