Emergency evacuation system, in particular for a tailless aeroplane
A technology of aircraft and equipment, applied in the equipment field of the third layer, can solve the problem of not providing channels
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[0034] figure 1 A pressure chamber 12 integrated in the middle wing 11 of a wing-body aircraft 20 is schematically represented. As shown, only the door 12a at the front of the cabin 12 leads directly to the outside. In contrast, in the lateral and rear regions, an unpressurized wing structure 11 extends from a pressure wall 13 of the nacelle 12 , which is spherical in the drawing. In order to ensure sufficient emergency evacuation capability, for each emergency exit position in the nacelle 12, an additional emergency exit door or emergency exit hatch is provided in these areas, that is, the top exit leading to the outside in the outer skin of the aircraft 20 Hatch 15 and bottom exit hatch 16.
[0035] Since a large part of the underside of the wing 11 (and thus also the bottom exit door 16) is below the waterline during an emergency landing on water, safe exit from the aircraft can only be ensured through the exit at the top of the wing. On land, likewise, in certain damage...
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