发明名称 QUICK INSTALLATION FUEL DAM
摘要 The disclosure generally relates to baffle fuel dams and tank boundary fuel dams having a single-piece or two-piece construction. In one example, a baffle fuel dam is a single piece having slotted holes sized and spaced to accommodate for tolerance variations during installation. The baffle fuel dams also include a base angle that allows installation at multiple locations. The disclosure also relates to tank boundary fuel dams that include a two-piece configuration which incorporates slotted holes to accommodate tolerance variations and that are sized/spaced for different installation locations. The tank boundary fuel dams may also include a base angle that allows installation at multiple locations.
申请公布号 US2016355273(A1) 申请公布日期 2016.12.08
申请号 US201514729685 申请日期 2015.06.03
申请人 THE BOEING COMPANY 发明人 Perez Diaz Fernando L.;Tanner Richard;Rodriguez Brendamari
分类号 B64D37/08;B64C3/34;B64C3/18 主分类号 B64D37/08
代理机构 代理人
主权项 1. A fuel dam for a fuel tank of an aircraft, the fuel tank including a plurality of reservoirs separated by ribs having intersections for accommodating stringers, the fuel dam comprising a planar body including: a first leg portion and a second leg portion; and a bridge portion connecting the leg portions and defining a recess between the first and second leg portions such that when the fuel dam is installed in the fuel tank at one of the intersections, the recess is disposed about a stringer in a substantially interference fitting relationship between the first and second leg portions.
地址 Chicago IL US