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Rocker arm type unmanned aerial vehicle ski buffering device

A buffer device and rocker-type technology, which is applied in sleds/sleds, aircraft parts, transportation and packaging, etc., can solve the problems of poor lateral stability of the body, reduce recovery overload, and small buffer strokes, and achieve high lateral stability. Reduce the effect of recovery overload and large buffer stroke

Inactive Publication Date: 2019-05-24
NORTHWESTERN POLYTECHNICAL UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to avoid the deficiencies existing in the prior art, overcome the problems of small buffering stroke of the UAV skid buffer device, interference between the movement of the skid bar and the shock absorber, and poor lateral stability of the body during the buffering process; the present invention proposes a rocker arm type unmanned Machine skid buffer device, the skid buffer device has the characteristics of high weather environment adaptability, large buffer stroke, and can reduce recovery overload

Method used

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  • Rocker arm type unmanned aerial vehicle ski buffering device
  • Rocker arm type unmanned aerial vehicle ski buffering device
  • Rocker arm type unmanned aerial vehicle ski buffering device

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Embodiment Construction

[0023] This embodiment is a rocker type unmanned aerial vehicle skid buffer device.

[0024] refer to Figure 1 ~ Figure 4 , the rocker-arm type UAV sled buffer device of this embodiment is a UAV rocker-arm type sled buffer device with a front and rear joint coaxial design. The skid buffer device is connected by the upper fuselage joint 3, the shock absorber fuselage connecting pin 4, the shock absorber 5, the rocker arm connecting pin 6, the skid bar 7, the front joint 8 of the skid bar, and the skid bar fuselage. Pin 9, rocking arm 10, rocking arm fuselage joint 11 form. Wherein, the upper fuselage joint 3 is installed on the lower side of the body, and the lug on the upper end of the upper fuselage joint 3 and the shock absorber 5 is connected by the shock absorber fuselage connecting pin 4; the lower end of the shock absorber 5 is connected with the rocker arm 10 are connected by the shock absorber rocker arm connecting pin 6.

[0025] The front joint 8 of the skid bar ...

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Abstract

The invention discloses a rocker arm type unmanned aerial vehicle ski buffering device. The rocker arm type unmanned aerial vehicle ski buffering device is composed an upper vehicle body connector, adamper, a ski bar and a rocker arm, wherein the upper vehicle body connector is arranged under a vehicle body and connected with the upper end of the damper through a damper-vehicle body connecting pin; a ski bar front connector is arranged in front of the vehicle body and connected with the ski bar through a ski bar-vehicle body connecting pin; the lower end of the damper is connected with the rocker arm through a damper-rocker arm connecting pin. During parachute landing, when the ski bar touches down, a ski bar support arm module can rotate around the ski bar front connector and a rocker arm-vehicle body connector under the action of support reaction force of the ground; during rotation, the ski bar support module can compress the damper, which then absorbs the sinking kinetic energy ofthe vehicle body to achieve buffering and damping effects; the ski is in a rocker arm type structure to achieve a long buffer stroke and reduce recovery overloading, and by means of high sideslip andground fiction, can absorb more impact energy to effectively protect safety of the vehicle body and equipment.

Description

technical field [0001] The invention relates to the technical field of UAV design, in particular to a rocker arm type UAV skid buffer device. Background technique [0002] Compared with traditional flying combat platforms, UAVs are small in size and highly concealed, and can go deep into the opponent's frontier to perform more dangerous tasks. Therefore, it is widely used in many fields such as enemy reconnaissance, electronic jamming, communication relay and air defense suppression. [0003] The sled shock absorption mode of UAV parachute recovery is not restricted by airport conditions, and has the characteristics of high battlefield mobility, simple control and strong site adaptability. It is currently the mainstream recovery method for most small and medium-sized UAV platforms. During the process of UAV parachute recovery and sled buffering, the UAV enters the sky above the predetermined recovery site, and the recovery parachute is inflated to open, stabilizing the sink...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/52B64C25/58
Inventor 闵荣席庆彪郭文安
Owner NORTHWESTERN POLYTECHNICAL UNIV
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