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.
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 代理人
主权项
地址