发明名称 Integrated gas turbine engine-nacelle
摘要 A nacelle for use with a gas turbine engine is provided with an integral webbed structure resembling a spoked wheel for rigidly interconnecting the nacelle and engine. The nacelle is entirely supported in its spacial relationship with the engine by means of the webbed structure. The inner surface of the nacelle defines the outer limits of the engine motive fluid flow annulus while the outer surface of the nacelle defines a steamlined envelope for the engine.
申请公布号 US4055041(A) 申请公布日期 1977.10.25
申请号 US19750628221 申请日期 1975.11.03
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 ADAMSON, ARTHUR P.;SARGISSON, DONALD F.;STOTLER, JR., CHARLES L.
分类号 B64D27/18;B64D29/00;F01D11/08;F02C7/20;(IPC1-7):F02C7/20;F02K3/04 主分类号 B64D27/18
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