发明名称 |
PRESA DHARIA AD ASSE INCURVATO PER TURBOMOTORE A GAS |
摘要 |
<p>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.</p> |
申请公布号 |
IT1131162(B) |
申请公布日期 |
1986.06.18 |
申请号 |
IT19800021936 |
申请日期 |
1980.05.09 |
申请人 |
GENERAL ELECTRIC CO |
发明人 |
RUEHR WILLIAM CARL;YOUNGHANS JAMES LEROY;SMITH EDWIN BRADSHAW |
分类号 |
B64D33/02;F02C7/04;(IPC1-7):F02K/ |
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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