发明名称 Ejection escape system for a passenger airplane
摘要 An ejection escape system for passenger airplane that there is a locking mechanism at the connection of the left top cabin cover, the right top cabin cover with the airplane body, there is also a locking mechanism at the connection of the left top cabin cover and the right top cabin cover, the passenger seat is an ejection escape seat, the switches for the locking mechanism and the ejection escape seat are installed in the cockpit, where the pilot can turn on the locking mechanism switch to open the left and right top cabin covers and turn on the ejection escape switch to eject the seat out of the airplane through the opening of the left and right top cabin covers.
申请公布号 US6695257(B2) 申请公布日期 2004.02.24
申请号 US20020205439 申请日期 2002.07.26
申请人 LIN JUNG-MIN 发明人 LIN JUNG-MIN
分类号 B64C1/32;B64D25/10;(IPC1-7):B64D25/12 主分类号 B64C1/32
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