发明名称 SEALING BLADDERLESS SYSTEM AND METHOD
摘要 Apparatus and methods are provided to minimize the escape of fuel out of a fuel tank when a tank wall is penetrated by a bullet. In one embodiment, a pressure differential may be maintained between a pressure within a fuel tank cavity and another pressure outside the fuel tank cavity in order to minimize the loss of fuel upon penetration of the fuel tank. In another embodiment, a compressed rubber layer of fuel-reactive rubber may be provided which is adapted to be attached to a fuel tank wall and to swell upon contact with fuel in order to substantially seal a penetrated hole in the fuel tank wall.
申请公布号 US2008264951(A1) 申请公布日期 2008.10.30
申请号 US20070740753 申请日期 2007.04.26
申请人 THE BOEING COMPANY 发明人 TWEET TRACY L.;SHELLY MARK A.
分类号 B64D37/06 主分类号 B64D37/06
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