发明名称 |
APPARATUS, SYSTEM AND METHOD FOR OBSERVING COMBUSTOR FLAME IN GAS TURBINE ENGINE |
摘要 |
PROBLEM TO BE SOLVED: To accurately observe and track combustor flames moving in a combustion chamber of a gas turbine engine.SOLUTION: A fuel injector for a gas turbine engine includes: a nozzle body for injecting fuel and air into a combustor; and an on-axis optical probe located within the nozzle body for observing combustor flame radiation, wherein the optical probe includes a plurality of optical fiber bundles extending to a distal end of the probe, and a shaped lens is supported at the distal end of the probe to provide a multi-directional field of view of combustion characteristics and properties in an operating gas turbine engine combustor. |
申请公布号 |
JP2013199929(A) |
申请公布日期 |
2013.10.03 |
申请号 |
JP20130061313 |
申请日期 |
2013.03.25 |
申请人 |
ROSEMOUNT AEROSPACE INC |
发明人 |
MYHRE DOUGLAS C;MIICHEL JOSEPH R;AADLAND TIMOTHY |
分类号 |
F02C9/00;F02C7/00;F02C7/228;F02C9/28 |
主分类号 |
F02C9/00 |
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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