发明名称 GAS TURBINE ENGINE STATOR VANE ASSEMBLY
摘要 A method of assembling gas turbine engine front architecture includes positioning inner and outer fairings relative to one another. Multiple vanes are arranged circumferentially between the inner and outer fairings. A liquid sealant is applied around a perimeter of the vanes to seal between the vanes and at least one of the fairings.
申请公布号 US2012189438(A1) 申请公布日期 2012.07.26
申请号 US201113010174 申请日期 2011.01.20
申请人 FEIGLESON STEVEN J.;TREMBLAY DENNIS R.;EDWARDS WILLIAM R. 发明人 FEIGLESON STEVEN J.;TREMBLAY DENNIS R.;EDWARDS WILLIAM R.
分类号 F01D1/02;B32B37/02;B32B37/12 主分类号 F01D1/02
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