FIELD: aircraft rescue systems.
SUBSTANCE: aircraft rescue system comprises a body, an opening emergency compartment in the upper part of the body, a braking device in the emergency compartment, a damper and shock-absorbing mechanism located in the lower part of the body, made telescopically in the vertical direction with the possibility of extension to a position below the aircraft landing gear. An emergency compartment is provided in the upper part of the aircraft body, and a braking device located in the emergency compartment is released in an emergency to assist in braking the aircraft body. The damper and damping mechanism runs below the chassis so that it makes contact with the ground first and absorbs the force of impact as the body is lowered.
EFFECT: invention is aimed at ensuring the safety of the aircraft and its crew.
10 cl, 15 dwg
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|
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