发明名称 |
ANSCHLUSSSTÜCKE MIT REDUNDANTEN DICHTUNGEN FÜR KRAFTSTOFFLEITUNGEN, KRAFTSTOFFBEHÄLTER UND WEITERE ANORDNUNGEN |
摘要 |
Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems are disclosed. A fitting in accordance with one embodiment can be positioned adjacent to an aperture in a fuel tank wall having an inner surface and an outer surface. The fitting can include a first member having a flange and a barrel. The barrel can further include a passageway. A first flange seal can be positioned at a face of the flange and can be sealably coupled to a surface, for example, the tank wall. A second flange seal can be disposed outwardly from the first flange seal against the surface. The fitting can further include a second member (e.g., a sensor) positioned within the passageway of the barrel. The fitting can further include first and second barrel seals positioned between the barrel and the second member. |
申请公布号 |
AT453081(T) |
申请公布日期 |
2010.01.15 |
申请号 |
AT20060252981T |
申请日期 |
2006.06.09 |
申请人 |
THE BOEING COMPANY |
发明人 |
CARNS, JAMES A.;CUTLER, THERON L.;SHELLY, MARK A.;VAN KAMPEN, BENJAMIN P. |
分类号 |
F16L39/00;B64D37/00;F16L41/14 |
主分类号 |
F16L39/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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