发明名称 |
GAS TURBINE COMBUSTOR |
摘要 |
An internal cylinder which has the opening section from which combustion gas is blown out is inserted into the tail cylinder which becomes a flow path of the combustion gas, and is engaged with the tail cylinder, while securing a clearance between the edge of the opening section and the internal wall surface of the tail cylinder. Air compressed with a compressor is jetted from the clearance along the internal wall surface of the tail cylinder, and a film of cooling air is formed on the internal wall surface of the tail cylinder.
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申请公布号 |
CA2380914(C) |
申请公布日期 |
2007.11.06 |
申请号 |
CA20022380914 |
申请日期 |
2002.04.05 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
AKAGI, KOUICHI;TOMIMOTO, SOUICHIROU |
分类号 |
F02C7/18;F23R3/02;F23R3/00;F23R3/04;F23R3/42 |
主分类号 |
F02C7/18 |
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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