发明名称 Apparatus for observing combustion conditions in a gas turbine engine
摘要 A fuel injector for a gas turbine combustor is disclosed which includes a feed arm having a flange for mounting the injector within the combustor and a fuel nozzle depending from the feed arm for injecting fuel into the combustor for combustion. An optical sensor array is operatively associated with the fuel nozzle for observing combustor flame characteristics. The optical sensor array includes a plurality of sapphire rods positioned to be close enough to the combustor flame to oxidize soot deposits thereon.
申请公布号 US7484369(B2) 申请公布日期 2009.02.03
申请号 US20050210095 申请日期 2005.08.23
申请人 ROSEMOUNT AEROSPACE INC. 发明人 MYHRE DOUGLAS C.
分类号 F02C7/00;F01D17/02;F01D21/00;F02C9/26;F02C9/28;F23N5/08 主分类号 F02C7/00
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