Aircraft with damping function

Abstract

The invention discloses an aircraft with a damping function. The aircraft with the damping function includes a machine body, wherein two second through holes are formed in the lower surface of inner wall of the machine body, first sliding wheels are arranged in the second through holes, the top ends of the first sliding wheels are fixedly connected with the bottom ends of the connecting rods, theback surfaces of the connecting rods are movably connected with the front surfaces of fixing blocks through hinge pins, the upper surfaces of the fixing blocks are fixedly connected with the lower surfaces of moving plates, second sliding grooves are formed in the opposite surfaces of the connecting rods, and second sliding wheels are slidably connected in the second sliding grooves. The first sliding wheels, the second through holes, the second sliding wheels, the second sliding grooves, the connecting rods, the hinge pins, the fixing blocks, limiting blocks, a first spring, fourth sliding grooves and fourth sliding blocks are matched with each other, the aircraft with the damping function avoids the damage caused to parts of the aircraft due to own gravity when the aircraft falls, so asto achieve the purpose of anti-vibration when the aircraft lands, and thus ensure the safety of the aircraft when the aircraft lands.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an aircraft with a damping function. Background technique [0002] An aircraft is an instrumental flying object manufactured by humans, capable of flying off the ground, flying in space and flying in the atmosphere or outside the atmosphere under the control of humans. Those flying in the atmosphere are called aircraft, and those flying in space are called spacecraft. [0003] At present, because the aircraft can adapt to various complex and harsh environments, the design is flexible, and the size is small, the aircraft is widely used in various fields. The aircraft needs to land after the work is completed, but most of the aircraft do not have shock absorbers, so When landing, it is easy to cause damage to the fuselage of the aircraft and even cause damage to the precision parts inside the aircraft fuselage, which affects the service life of the aircraft and increases the cost ...

AI Technical Summary

Problems solved by technology

[0005] Aiming at the deficiencies in the prior art, the present invention provides an aircraft with a shock absorbing function, which solves the problem that the existing aircraft does not have a shock absorbing device, so it is easy to cause damage to the fuselage of the aircraft or even cause damage to the fuselage of the aircraft when it lands. The internal precision parts cause damage, which affects the use time of the aircraft and increases the cost of use, and because the aircraft is integrated, it is very inconvenient to disassemble. When disassembling, the user needs to remove the wings from the aircraft, which is more cumbersome , it is not convenient for the user to maintain and repair the wing

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