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 |
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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