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 |
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代理人 |
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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 |