发明名称 Combustion chamber for gas turbine engine
摘要 <p>A combustion chamber suitable for a gas turbine engine is provided with at least one Helmholtz resonator having a resonator cavity and a damping tube in flow communication with the chamber interior. The damping tube is provided with at least one cooling hole extending through its wall for improved damping and cooling.</p>
申请公布号 EP1962018(B1) 申请公布日期 2015.10.14
申请号 EP20080009068 申请日期 2003.12.18
申请人 ROLLS-ROYCE PLC;ROLLS-ROYCE DEUTSCHLAND LTD & CO KG 发明人 ALAN PHILIP, GEARY;KLAUS STEFAN STEINBACH;KENNETH JAMES YOUNG;VOLKER HERZOG;MIKLOS GERENDAS;IAIN DAVID DUPERE
分类号 F23R3/00;F23M99/00;F23R3/06 主分类号 F23R3/00
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