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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|