发明名称 Hybrid emergency ejection system
摘要 An emergency escape sequence for a commercial aircraft is shown. Individual pods that are separable from the aircraft are ejected individually, following the separation and ejection of the upper cabin from the fuselage. Parachutes are deployed to assist in the safe descent of the pods. Airbags are also deployed to soften the landing and provide flotation in case of a water landing.
申请公布号 US2011233341(A1) 申请公布日期 2011.09.29
申请号 US20100802569 申请日期 2010.06.09
申请人 MONTEFORTE MICHAEL A 发明人 MONTEFORTE MICHAEL A.
分类号 B64D25/12 主分类号 B64D25/12
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