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Non-hoisting type disassembling and assembling method for medium and large unmanned aerial vehicles

A non-hoisting, unmanned aerial vehicle technology, applied in the direction of lifting devices, metal processing equipment, metal processing, etc., can solve the problems of disassembly and assembly of medium and large unmanned aerial vehicles in non-hoisting form, so as to improve the daily use rate and improve the automatic The effect of safeguarding capacity

Active Publication Date: 2022-07-22
四川腾盾科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The object of the present invention is: the present invention provides a non-hoisting disassembly and assembly method for medium and large UAVs, which solves the problem of non-hoisting disassembly and assembly of medium and large UAVs

Method used

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  • Non-hoisting type disassembling and assembling method for medium and large unmanned aerial vehicles
  • Non-hoisting type disassembling and assembling method for medium and large unmanned aerial vehicles
  • Non-hoisting type disassembling and assembling method for medium and large unmanned aerial vehicles

Examples

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Embodiment 1

[0036] The UAV has a front three-point layout. Its tail brace, outer wing, flat tail, propeller and other outer contours are relatively light components, which are separated from the UAV in advance. The remaining UAV structural states are: fuselage (front landing gear and front fuselage). combination), the central wing (two engines and nacelles, the main landing gear is installed in the nacelle), the nose landing gear and the main landing gear are in the down state, hereinafter referred to as the combination of the fuselage and the central wing.

[0037] refer to figure 1 As shown in the figure, a non-hoisting decomposition method of medium and large unmanned aerial vehicles adopts equipment including a supporting chassis 1, a fuselage bracket 2, a nacelle bracket 3 and a lifting mechanism 9, and the forward direction is the direction of the supporting chassis 1. The right and left directions are the rear ends of the supporting chassis 1, which include the following steps.

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Embodiment 2

[0054] A non-hoisting assembly method for medium and large unmanned aerial vehicles, which adopts the opposite steps of the above-mentioned non-hoisting decomposition method for medium and large unmanned aerial vehicles, and assembles from step ⑨ to step ①, and the action sequence of each step is also from the following steps. operate before. Others are the same as in Example 1.

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Abstract

The invention discloses a non-hoisting type disassembling and assembling method for medium and large unmanned aerial vehicles. During decomposition, firstly, the fuselage bracket capable of moving in a three-dimensional mode is moved to a proper position, then the unmanned aerial vehicle is pulled to the position over the bracket, and the unmanned aerial vehicle is jacked up through the jacking function of the fuselage bracket; after the undercarriage lifts off the ground, the front undercarriage is folded, and the split type central wing nacelle bracket is placed at the bottom of a nacelle of a central wing; and descending the fuselage bracket, and completing the disassembly of the unmanned aerial vehicle under the cooperation of the fuselage bracket and the central wing support nacelle frame. During assembly, opposite steps of the non-hoisting type disassembling method for the medium and large unmanned aerial vehicles are adopted. The unmanned aerial vehicle has the beneficial effects that the dependence of disassembly and assembly of the unmanned aerial vehicle on a crane is eliminated, and the self-guarantee capability is improved; and the bracket can also be used as daily bearing equipment, so that the daily utilization rate of the bearing equipment is improved.

Description

technical field [0001] The invention belongs to the field of unmanned aerial vehicle packaging and transportation, in particular to a non-hoisting disassembly and assembly method for medium and large unmanned aerial vehicles. Background technique [0002] In view of the requirements of convenience, confidentiality and integration, the storage and position transfer of UAVs involve the disassembly and assembly of UAVs. The disassembly and assembly of medium and large UAVs requires reducing the dependence on rental equipment and avoiding the use of cranes to complete the disassembly and assembly of UAVs. [0003] Combined with the above analysis, it is a development trend and imperative to develop a non-hoisting UAV decomposition and assembly method. SUMMARY OF THE INVENTION [0004] The purpose of the present invention is: the present invention provides a non-hoisting disassembly and assembly method of medium and large unmanned aerial vehicles, which solves the problem of d...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P19/04B66F7/06
CPCB23P19/04B66F7/0625B66F7/065B64U10/25B64U80/70
Inventor 胡斌叶佳孙齐峰陈洪昌赵志龙
Owner 四川腾盾科技有限公司