发明授权
- 专利标题: Gas turbine combustor and combustion method therefor
- 专利标题(中): 燃气轮机燃烧器及其燃烧方法
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申请号: US563191申请日: 1990-08-06
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公开(公告)号: US5069029A公开(公告)日: 1991-12-03
- 发明人: Michio Kuroda , Seiichi Kirikami , Katsukuni Hisano , Nobuyuki Iizuka , Haruo Urushidani , Isao Sato , Yoji Ishibashi , Takashi Ohmori
- 申请人: Michio Kuroda , Seiichi Kirikami , Katsukuni Hisano , Nobuyuki Iizuka , Haruo Urushidani , Isao Sato , Yoji Ishibashi , Takashi Ohmori
- 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: JPX62-50060 19870305
- 主分类号: F23C99/00
- IPC分类号: F23C99/00 ; F23R3/26 ; F23R3/34 ; F02C3/14 ; F23R3/32
摘要:
A gas turbine combustor comprising a head combustion chamber and a rear combustion chamber connected to a downstream side of the head combustion chamber, a first stage burner for premixing first stage fuel and air and supplying the resultant fuel and air premixture into the head combustion chamber to effect first stage premix combution, a second stage burner for premixing second stage fuel and air and the resultant fuel and air premixture into the rear combustion chamber to effect premix combustion in addition to the first stage premix combustion, and a device for regulating flow rates of combustion air to be premixed with first and second stage fuel. The combustor is further provided with a pilot burner in the head combustion chamber to form pilot flame and stabilize the first stage premix combustion.
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