发明名称 Mounting bypass gas turbines engines on aircraft
摘要 A bypass gas turbine engine is mounted from an aircraft pylon by a mounting arrangement in which the engine outer casing and the core gas generator are mounted independently to the pylon and in which all the connections between the outer casing and the pylon and between the core gas generator and the pylon lie in substantially the same two planes.
申请公布号 US4013246(A) 申请公布日期 1977.03.22
申请号 US19750640158 申请日期 1975.12.12
申请人 ROLLS-ROYCE (1971) LIMITED 发明人 NIGHTINGALE, DOUGLAS JOHN
分类号 B64D27/26;B64D27/18;B64D29/00;(IPC1-7):B64D27/16 主分类号 B64D27/26
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