发明名称 MULTI-EXIT COMBINED EVACUATION SLIDE
摘要 Systems and methods for multi-exit evacuation for aircraft are disclosed. In one embodiment, an inflatable evacuation slide for emergency evacuation includes two coupled inflatable portions. The first inflatable portion (112), which includes a first inclined sliding surface, is configured to provide downward egress from an, over-wing exit (108). Similarly, the second inflatable portion (114), which includes a second inclined surface, is likewise configured to provide downward egress from a non over-wing exit (106). In particular embodiments, the inflatable portions are configured to be deployed from a storage location proximate the over-wing and non over-wing exits. In other embodiments, at least one of the first and second inflatable portions includes a lateral area for horizontal movement (120). In alternative embodiments, the inflatable evacuation slide further includes a divider rail (124) disposed between the first inflatable portion and the second inflatable portion.
申请公布号 WO2008100711(A3) 申请公布日期 2008.10.09
申请号 WO2008US52523 申请日期 2008.01.30
申请人 THE BOEING COMPANY;MCDONALD, STEVEN, P.;LENABURG, ROBERT, J. 发明人 MCDONALD, STEVEN, P.;LENABURG, ROBERT, J.
分类号 B64D25/14 主分类号 B64D25/14
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