发明名称 Gas turbine engine with convertible accessories
摘要 Drive means for connecting a gas turbine engine to its accessories are so constructed as to allow the accessories to be selectively positioned to any one of several predetermined circumferential positions about the perimeter of the engine. This feature permits convenient mounting of the same engine upon vehicles demanding radically different engine mounting arrangements.
申请公布号 US4068470(A) 申请公布日期 1978.01.17
申请号 US19740522109 申请日期 1974.11.08
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 SARGISSON, DONALD F.;ADAMSON, ARTHUR P.
分类号 B64D35/00;F02C7/32;(IPC1-7):F02K3/02;F16H35/00;F16H1/14 主分类号 B64D35/00
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