| 摘要 |
<p>The invention relates to an aircraft ejection device for passengers and cargo. The inventive device is characterised in that it consists of a series of platforms (29, 30, 31) which are disposed in the form of correlative sections along the length of the aircraft, said platforms comprising a main frame (1). Rocket boosters (2) and a damping canvas or inflatable raft (3) are disposed under said main frame. Moreover, the aforementioned main frame (1) contains fuel housings (5) for the rocket boosters (2), housings for the booster (2) control systems, containers of inert gas for inflating the raft and cubicles (8) for emergency, position-finding equipment, etc., all of which are accessible by means of flap doors. The passenger seats (25) or the cargo are housed in a casing (11) of said main frame. The above-mentioned platforms (29, 30, 31) comprise an upper, lateral reinforcing structure (26) bearing parachutes (27) which is laterally installed in the fuselage (28) using ejection guides (33).</p> |
