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
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