发明名称 EXTERNAL STRUCTURE MOUNTING SYSTEM FOR USE WITH AN AIRCRAFT
摘要 A mounting system for mounting an external structure to an aircraft includes a plurality of first mounting structures coupled to the aircraft and at least one link coupled to each first mounting structure of the plurality of mounting structures. The mounting system also includes a second mounting structure positioned proximate the at least one link, wherein the second mounting structure includes at least one aperture defined therein. An eccentric bearing is positioned in the at least one aperture and is configured to couple the second mounting structure to the at least one link. The eccentric bearing includes a bore extending therethrough that is offset from an axial center of the eccentric bearing.
申请公布号 US2017081016(A1) 申请公布日期 2017.03.23
申请号 US201514862779 申请日期 2015.09.23
申请人 The Boeing Company 发明人 Harleman Thomas J.
分类号 B64C7/00 主分类号 B64C7/00
代理机构 代理人
主权项 1. A mounting system for mounting an external structure to an aircraft, said mounting system comprising: a plurality of first mounting structures coupled to the aircraft; at least one link coupled to each first mounting structure of said plurality of first mounting structures; a second mounting structure positioned proximate said at least one link, said second mounting structure comprising at least one aperture defined therein; an eccentric bearing positioned in said aperture and configured to couple said second mounting structure to said at least one link, wherein said eccentric bearing comprises a bore extending therethrough that is offset from an axial center of said eccentric bearing.
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