发明名称 |
System for observing combustion conditions in a gas turbine |
摘要 |
A system for stabilizing combustion in a gas turbine engine comprises a) optical sensing means embedded within a fuel injector for observing conditions within a combustion chamber of a gas turbine engine; b) means for detecting combustion instabilities based upon conditions observed by the optical sensing means; and c) means for modulating a fuel flow rate to reduce detected combustion instabilities. |
申请公布号 |
EP2508801(A2) |
申请公布日期 |
2012.10.10 |
申请号 |
EP20120001631 |
申请日期 |
2005.03.30 |
申请人 |
ROSEMOUNT AEROSPACE INC. |
发明人 |
MYHRE, DOUGLAS C. |
分类号 |
F23N5/08;F01D17/02;F01D21/00;F02C9/26;F02C9/28 |
主分类号 |
F23N5/08 |
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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