发明名称 |
Case deflection control in aircraft gas turbine engines |
摘要 |
A gas turbine engine and structure for mounting the gas turbine engine on an aircraft is disclosed. Techniques for controlling the magnitude of engine case deflection from the axis of the engine are developed. The transfer of a portion of the gust and thrust loads externally of the engine case to a location downstream of the rearward engine mount generates a reverse moment which counteracts deflection in the engine case.
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申请公布号 |
US4428189(A) |
申请公布日期 |
1984.01.31 |
申请号 |
US19800136608 |
申请日期 |
1980.04.02 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
GREENBERG, PAUL B.;LENKEIT, C. HEINZ;SEIBERT, WILLARD J. |
分类号 |
F02C7/00;F02C7/20;(IPC1-7):F02C7/20 |
主分类号 |
F02C7/00 |
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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