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
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