发明名称 Multiple pure tone elimination strut assembly
摘要 An acoustic noise elimination assembly having a capability for disrupting the continuity of fields of sound pressures forwardly projected from fans or rotors of a type commonly found in the fan or compressor first stage for air-breathing engines, when operating at tip speeds in the supersonic range. The assembly incudes a tubular cowl 12 defining a duct for delivering an airstream axially into the intake for a jet engine E and a sound barrier 14, defined by a plurality of intersecting flat plates or struts 14a-14d having a line of intersection coincident with a longitudinal axis of the tubular cowl, which serves to disrupt the continuity of rotating fields of multiple pure tonal components of noise.
申请公布号 US4300656(A) 申请公布日期 1981.11.17
申请号 US19800185869 申请日期 1980.09.11
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 BURCHAM, FRANK W.
分类号 B64D33/02;F02C7/045;(IPC1-7):B64D33/02 主分类号 B64D33/02
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