发明名称 Gas turbine engine auxiliary component mount
摘要 A mount system for an auxiliary component includes two side brackets and a top bracket for rigidly attaching an auxiliary component to an engine casing. Each side bracket defines mount segments, a deformable member and two retainer members between the mount segment. The deformable member plastically deforms during a fan-blade out event, thereby absorbing a majority of the high shock load experienced on the auxiliary component. The retainer members maintain the attachment between the auxiliary component and the engine casing subsequent to the fan-blade out event.
申请公布号 US2007125087(A1) 申请公布日期 2007.06.07
申请号 US20050291348 申请日期 2005.12.01
申请人 HAMILTON SUNDSTRAND 发明人 CALLAGHAN CRAIG M.
分类号 F02C7/32 主分类号 F02C7/32
代理机构 代理人
主权项
地址