A method of launching a drone

A technology for unmanned aerial vehicles and launch platforms, applied in the field of unmanned aerial vehicles, can solve the problems of high manufacturing and use costs, difficult maintenance and complex structures, etc., and achieve the effects of fast rotation rate, easy storage, and reduced size

Active Publication Date: 2021-07-02
ZHENGZHOU KANGXIAO TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, my country's UAV launch system mainly adopts hydraulic, pneumatic, rocket-assisted and other methods, but these launch methods have complex structures, high manufacturing and use costs, and difficult maintenance.

Method used

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  • A method of launching a drone
  • A method of launching a drone
  • A method of launching a drone

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Embodiment Construction

[0033] Such as Figure 1-6As shown, the unmanned aerial vehicle launcher includes a launching platform 1, a rotating platform 2 and a launching base 3. The bottom of the launching base 3 is provided with four walking wheels 4, and the rotating platform 2 is connected to the launching base by a thrust bearing 5 in rotation. 3. On the upper surface, the launch base 3 is provided with a hydraulic station 6 and a rotary power mechanism for driving the rotation of the rotary table 2. The length direction of the launch platform 1 is set along the front and rear directions, and the rear bottom of the launch platform 1 is hinged on the rotary table 2. The rear side of the launch platform 1 is hinged with a lift cylinder 7 between the bottom of the front side of the launch platform 1 and the front side of the turntable 2. The launch platform 1 is provided with a launch push mechanism, and the rear side of the launch platform 1 is provided with a folding plate auxiliary mechanism. The s...

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Abstract

A method for launching an unmanned aerial vehicle, comprising the following steps: (1). First, the unmanned aerial vehicle launching device is pulled and transported to the launching site by an engineering vehicle: the said unmanned aerial vehicle launching device includes a launching platform, a rotating platform and a launching base There are four walking wheels at the bottom of the launching base, and the rotating platform is connected to the upper surface of the launching base through thrust bearings. There is a hydraulic station and a rotary power mechanism for driving the rotating platform in the launching base. The launching platform The length direction of the launch platform is set along the front and rear directions, the rear bottom of the launch platform is hinged on the rear side of the rotary table, and a lifting cylinder is hinged between the front bottom of the launch platform and the front side of the rotary table, and a launch push mechanism is provided on the launch platform; To sum up, the present invention has simple structure, reasonable design, and low cost. The hydraulic motor provides the power source, which is driven by the chain structure to drive the take-off of the UAV, which provides a guarantee for the smooth take-off of the modern UAV.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a method for launching an unmanned aerial vehicle. Background technique [0002] UAV is the abbreviation of "unmanned aircraft", which mainly relies on radio remote control or through autopilot to realize autonomous flight control. It is one of today's high-tech weapons and equipment. It is widely used in many military operations such as battlefield reconnaissance, electronic countermeasures, and air strikes. It is known as the "clairvoyance" and "killer mace" of the modern battlefield. At present, my country's UAV launch system mainly adopts hydraulic, pneumatic, rocket-assisted and other methods, but these launch methods have complex structures, high manufacturing and use costs, and difficult maintenance. Contents of the invention [0003] In order to solve the deficiencies in the prior art, the present invention provides a method for launching a...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/06
CPCB64F1/06B64U70/70
Inventor 关欣张志华张书勤胡翔
Owner ZHENGZHOU KANGXIAO TECH CO LTD
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