发明名称 |
УСТРОЙСТВО ДЛЯ КАМЕРЫ СГОРАНИЯ ГАЗОВОЙ ТУРБИНЫ |
摘要 |
A device for a combustion chamber of a gas turbine for controlling the intake of gas into the combustion zone of the combustion chamber. The device includes a control element that is arranged outside the combustion chamber. This control element has a first covering for at least a first inlet to the combustion zone and is displaceable in relation to the combustion chamber. There is also a support for the control element that is connected to the cover. The cover is displaceable relative to the combustion chamber and a support ( 16 ) for the control element ( 12, 12' ) is connected to the cover. The support ( 16 ) is accommodated in a structure ( 4 ) at a rear of the combustion chamber. |
申请公布号 |
RU2004118421(A) |
申请公布日期 |
2005.07.10 |
申请号 |
RU20040118421 |
申请日期 |
2002.10.10 |
申请人 |
ВОЛЬВО АЭРО КОРПОРЕЙШН (SE) |
发明人 |
ЙЕНССОН Бертил (SE);ЮХАНССОН Патрик (SE) |
分类号 |
F23R3/00;F23R3/26;F23R3/28;F23R3/30;F23R3/34 |
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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