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).
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
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