发明名称 |
A DEVICE FOR A COMBUSTION CHAMBER OF A GAS TURBINE |
摘要 |
The invention relates to a device for a combustion chamber (1) in a gas turbine for controlling the intake of gas to the combustion zone (10, 11) of the combustion chamber. The device comprises a control element (12) which is arranged outside the combustion chamber and which in turn comprises a means (13) for covering at least one inlet to the combustion zone, the cover means being displaceable in relation to the combustion chamber. The device further comprises a means (16) connected to the cover means for supporting the control element. The means of support (16) is accommodated in a structure (4) at the rear of the combustion chamber (1).
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申请公布号 |
CA2467334(C) |
申请公布日期 |
2010.09.28 |
申请号 |
CA20022467334 |
申请日期 |
2002.10.10 |
申请人 |
VOLVO AERO CORPORATION |
发明人 |
JOENSSON, BERTIL;JOHANSSON, PATRIK |
分类号 |
F23R3/00;F23R3/26;F23R3/28;F23R3/30;F23R3/34;F23R3/60 |
主分类号 |
F23R3/00 |
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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