Shock absorbing, balancing and anti-collision flying device for high-altitude flight and transportation

Abstract

The invention discloses a shock absorbing, balancing and anti-collision flying device for high-altitude flight and transportation. The shock absorbing, balancing and anti-collision flying device for the high-altitude flight and transportation comprises a shock absorbing device and a balancing device; the shock absorbing device comprises an upper pressing strip and a lower pressing strip, which are arranged at the bottom of an aircraft; a rebounding mechanism and a shock absorbing mechanism are arranged between the upper pressing strip and the lower pressing strip; a pipeline is arranged on the aircraft; a gravity groove is formed in the aircraft; a plurality of accommodating grooves are formed in the pipeline; water storage vesicles are arranged in the accommodating grooves; and a plurality of nail cones are arranged on a pressure strip. Compared with the prior art, the shock absorbing, balancing and anti-collision flying device for the high-altitude flight and transportation is advantaged in that the vibration generated by the falling of the device is relieved through the rebounding mechanism; once the vibration force generated by falling is too large and cargoes are easily damaged, the shock absorbing mechanism can realize an effect of absorbing a large amount of vibration forces; and when the aircraft is out of control in the air, the water storage vesicles can be punctured by using the nail cones so that the water flows into the gravity groove to control the aircraft to be not inclined in case that the gravity is concentrated upon the lower part of the aircraft.

Description

technical field [0001] The invention relates to a flying device, in particular to a shock-absorbing and balanced anti-collision flying device for high-altitude flight transportation, which belongs to the field of logistics transportation. Background technique [0002] The aircraft in the related art includes a power unit, a flight control unit, and an additional load unit if a specific function is to be realized. However, in the aircraft of the related art, the flight control unit and the power unit adopt the hard connection method of direct connection, so that the vibration generated by the power unit during work will be directly transmitted to the flight control unit, causing the flight control unit to vibrate with the power unit, especially Yes, the load usually carried on the fuselage will also vibrate with the power unit, making the flight control unit and load unable to meet the needs of practical applications, which greatly affects the accuracy of the aircraft during ...

AI Technical Summary

Problems solved by technology

[0006] In the above three related technologies, there is no effective solution to the efficient shock absorbing device that the aircraft should have when carrying cargo or emergency landing. In order to meet the needs of carrying cargo, the installation position of the shock absorbing device must also be installed in contact with the ground. Therefore, there are higher requirements for its structural arrangement and shock absorption effect.

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