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
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