发明名称 |
CURVED CENTERLINE AIR INTAKE FOR A GAS TURBINE ENGINE |
摘要 |
<p>13DV-7424 CURVED CENTERLINE AIR INTAKE FOR A GAS TURBINE ENGINE 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 |
CA1140349(A) |
申请公布日期 |
1983.02.01 |
申请号 |
CA19800350627 |
申请日期 |
1980.04.24 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
RUEHR, WILLIAM C.;SMITH, EDWIN B.;YOUNGHANS, JAMES L. |
分类号 |
B64D33/02;F02C7/04;(IPC1-7):F02C7/04 |
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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