发明名称 TURBOFAN GAS TURBINE ENGINE AND NACELLE ARRANGEMENT
摘要 The arrangement comprises a fan by-pass duct located within the nacelle and having an inlet and an outlet. The outlet is generally oriented substantially radially and at an intermediary location along the nacelle. The nacelle has an aft section with an initially convex and substantially outwardly extending surface adjacent to the outlet of the fan by-pass duct. The surface of the aft section decreases in curvature and becomes concave towards a rear end of the engine.
申请公布号 US2008118348(A1) 申请公布日期 2008.05.22
申请号 US20060561601 申请日期 2006.11.20
申请人 ALECU DANIEL T 发明人 ALECU DANIEL T.
分类号 F01D17/00 主分类号 F01D17/00
代理机构 代理人
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