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 GB2444692(B) 申请公布日期 2010.09.29
申请号 GB20080007001 申请日期 2006.09.25
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 CRAIG M CALLAGHAN
分类号 F02C7/32;B64D41/00 主分类号 F02C7/32
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