发明名称 Combustion chamber for gas turbines
摘要 The combustion chamber system for a gas turbine comprises a series of individual tubular combustion chambers (2) which open into a common annular combustion chamber (3). The height of this varies periodically and is minimal in the areas between the tubular combustion chambers.
申请公布号 EP1284391(A1) 申请公布日期 2003.02.19
申请号 EP20010119559 申请日期 2001.08.14
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 TIEMANN, PETER
分类号 F23R3/46;F01D9/02;F23R3/00;(IPC1-7):F23R3/00 主分类号 F23R3/46
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