发明名称 |
Tangentially aligned pre-mixing combustion chamber for a gas turbine |
摘要 |
A pre-mixing combustion chamber (8) for a gas turbine is disclosed which includes a main stage with at least one pre-mixing chamber and a combustion chamber fashioned at least partly dynamically balanced relative to its longitudinal axis with a main combustion zone (3) and an after-combustion zone (5) placed downstream, whereby the at least one pre-mixing chamber discharges into the combustion chamber in the region of the main combustion zone tangentially producing twisting action. The pre-mixing chamber also includes a pilot stage (4) with a pilot injection means, whereby the main combustion zone in the combustion chamber proceeds essentially coaxial to the after-combustion zone, and the pilot stage is arranged at that end of the combustion chamber remote from the after-combustion zone.
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申请公布号 |
US6202420(B1) |
申请公布日期 |
2001.03.20 |
申请号 |
US19980211837 |
申请日期 |
1998.12.15 |
申请人 |
MTU MOTOREN-UND TURBINEN-UNION MüNCHEN GMBH |
发明人 |
ZARZALIS NIKOLOAS;RIPPLINGER THOMAS |
分类号 |
F23R3/30;F23R3/28;F23R3/34;F23R3/58;(IPC1-7):F23R3/30 |
主分类号 |
F23R3/30 |
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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