发明名称 TURBINE EXHAUST STRUT AIRFOIL AND GAS PATH PROFILE
摘要 A fuel injection system comprises a fuel conveying member and a nozzle tip assembly threadably engaged thereto. A sealing element is engaged in a fuel passage between the fuel conveying member and the nozzle tip for sealing the junction therebetween. The sealing element may include first and second sealing elements located proximate each other and having different cross-sectional shape.
申请公布号 CA2599816(A1) 申请公布日期 2008.02.29
申请号 CA20072599816 申请日期 2007.08.29
申请人 PRATT & WHITNEY CANADA CORP. 发明人 RUDRAPTNA, NAGARAJA;PATEL, BHAWAN B.;MORENKO, OLEG
分类号 F23R3/28;F02C7/22;F02C7/28;F02M61/18 主分类号 F23R3/28
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