发明名称 Landing gear attachment
摘要 A landing gear attachment apparatus (100) has a landing gear side bearing retention arrangement (104) connected to an aircraft side attachment apparatus (102), held together by a series of fuse pins. The interaction between a fuse pin carrier and a trunnion block varies the amount of load required to separate the landing gear from the fuselage depending on the direction of the load.
申请公布号 US8851418(B2) 申请公布日期 2014.10.07
申请号 US201213569528 申请日期 2012.08.08
申请人 Airbus Operations Limited 发明人 Ekmed{hacek over (z)}ić Andrija;Straccia Mario;Jones Philip
分类号 B64C25/10;B64C25/14;B64C25/20;B64C25/04 主分类号 B64C25/10
代理机构 Nixon & Vanderhye P.C. 代理人 Nixon & Vanderhye P.C.
主权项 1. An aircraft landing gear attachment comprising: an aircraft mount; a trunnion block; a reaction block positioned in first direction relative to the trunnion block, in abutment with the trunnion block but detached from the trunnion block, wherein in which the trunnion block is connected to the mount by a first frangible connection such that a force applied to the trunnion block in said first direction separates the trunnion block and the mount at a first predetermined force level, and said reaction block is attached to the mount by a second frangible connection and a force applied to the trunnion block in a second direction different from said first direction separates the trunnion block and the mount.
地址 Bristol GB