发明名称 |
Engine testing mounting adaptor |
摘要 |
A flexible adaptor mounts an aircraft gas turbine engine to a test stand. The adaptor includes an upper frame configured for mounting on the test stand, and a lower frame spaced from the upper frame and configured for supporting the engine. A spring flexibly joins the lower frame to the upper frame to simulate the flexibility of an aircraft wing which supports the engine during operation.
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申请公布号 |
US5396791(A) |
申请公布日期 |
1995.03.14 |
申请号 |
US19930106475 |
申请日期 |
1993.08.13 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
MOLLMANN, DANIEL E.;BOEHM, PAMELA M.;GAFFNEY, EUGENE F.;SWIFT, MICHAEL P.;STEGEMILLER, MARK E.;JOHNSON, KENNETH O.;CARMICHAEL, STEPHEN L. |
分类号 |
B64F5/00;F01D25/28;G01L5/13;(IPC1-7):G01L1/10 |
主分类号 |
B64F5/00 |
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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