发明名称 GAS TURBINE ENGINE AUXILIARY COMPONENT MOUNT
摘要 <p>A mount system for an auxiliary component includes two side brackets (42, 44) and a top bracket (46) for rigidly attaching an auxiliary component (32) to an engine casing (22). Each side bracket (42, 44) defines mount segment (50, 52), a deformable member (SO) and two retainer members (62, 64) between the mount segments. The deformable member (60) plastically deforms during a fan-blade out event, thereby absorbing a majority of the high shock load experienced on the auxiliary component (32). The retainer members (62, 64) maintain the attachment between the auxiliary component (32) and the engine casing (22) subsequent to the fan-blade out event.</p>
申请公布号 WO2007064388(A1) 申请公布日期 2007.06.07
申请号 WO2006US37381 申请日期 2006.09.25
申请人 HAMILTON SUNDSTRAND;CALLAGHAN, CRAIG M. 发明人 CALLAGHAN, CRAIG M.
分类号 F02C7/32;B64D41/00 主分类号 F02C7/32
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