发明名称 |
Curved centerline air intake for a gas turbine engine |
摘要 |
An inlet for a gas turbine engine is disposed about a curved centerline for the purpose of accepting intake air that is flowing at an angle to engine centerline and progressively turning that intake airflow along a curved path into alignment with the engine. This curved inlet is intended for use in under-the-wing locations and similar regions where airflow direction is altered by aerodynamic characteristics of the airplane. By curving the inlet, aerodynamic loss and acoustic generation and emission are decreased.
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申请公布号 |
US4220171(A) |
申请公布日期 |
1980.09.02 |
申请号 |
US19790038980 |
申请日期 |
1979.05.14 |
申请人 |
U S OF AMERICA NASA ADMINISTRATOR |
发明人 |
RUEHR, WILLIAM C;SMITH, EDWIN B;YOUNGHANS, JAMES L |
分类号 |
B64D33/02;F02C7/04;(IPC1-7):B64D33/02 |
主分类号 |
B64D33/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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