发明名称 FUEL MANIFOLD INLET TUBE
摘要 An inlet tube supplies fuel to a manifold of a combustor in a gas turbine engine, the manifold defining a manifold plane. The inlet tube comprises a tube body having a channel providing fluid flow communication between first and second ends of the tube body. At least a portion of the channel defines a tube body plane which is spaced apart from the manifold plane.
申请公布号 US2007163265(A1) 申请公布日期 2007.07.19
申请号 US20070669493 申请日期 2007.01.31
申请人 FISH JASON;PATEL BHAWAN B 发明人 FISH JASON;PATEL BHAWAN B.
分类号 F02C7/26;F02C7/22;F23R3/28 主分类号 F02C7/26
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