FIELD: aircraft rescue systems.
SUBSTANCE: present invention is an aircraft rescue system that solves the technical problem that an aircraft is capable of assisting in braking and landing of an aircraft and absorbing impact force during descent to ensure the safety of an aircraft and its crew. The rescue system comprises an aircraft body, wherein an opening emergency compartment is provided in the upper part of the aircraft body, a braking device is provided in the emergency compartment, and the braking device is designed to be released from the emergency compartment to ensure braking and landing of the aircraft body. The damper and shock-absorbing mechanism is located in the lower part of the aircraft body, and the damper and shock-absorbing mechanism is provided telescopically in the vertical direction and the damper and shock-absorbing mechanism is made with the possibility of extension to a position below the aircraft chassis.
EFFECT: according to the present invention, an emergency compartment is provided at the top of an 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 damper mechanism extends below the landing gear, and the damper and damper mechanism first touches the ground, so that the impact force of the lowering of the aircraft body can be absorbed and serious accidents caused by the impact force of the lowering of the aircraft body can be prevented.
10 cl, 30 dwg
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Authors
Dates
2022-10-12—Published
2022-01-12—Filed