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Unmanned aerial vehicle device working on heavy load condition and control method

A drone and heavy-duty technology, applied in the field of drones, can solve the problems of difficult flying tasks of drones, restrictions on the use of drones, and large onboard energy consumption, so as to expand the operating time and scope of operations , prolong working time and improve working efficiency

Inactive Publication Date: 2016-07-27
BEIFANG UNIV OF NATITIES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to overcome the problem in the prior art that due to the limited onboard energy of the UAV, the UAV needs to consume a large amount of onboard energy under heavy load conditions, which makes it difficult for the UAV to perform long-term flight tasks. , a problem that has a huge impact on the operating efficiency and popularization of unmanned aerial vehicles, provides a kind of unmanned aerial vehicle device and control method that work under heavy load conditions, and the unmanned aerial vehicle device can reduce the unmanned aerial vehicle under heavy load conditions The consumption of on-board energy enables the UAV to consume the on-board energy in a long period of time, prolonging the flight operation time under heavy load conditions, so as to improve the operating efficiency of the UAV and expand the UAV’s ability to operate under heavy loads. The operating time and operating range under load conditions overcome the shortcomings of the limited use of drones under heavy load conditions

Method used

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  • Unmanned aerial vehicle device working on heavy load condition and control method
  • Unmanned aerial vehicle device working on heavy load condition and control method
  • Unmanned aerial vehicle device working on heavy load condition and control method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0043] This embodiment is used in occasions where the unmanned aerial vehicle conducts flight operations under heavy load conditions.

[0044] Such as figure 2 As shown, the drone device working under heavy load conditions includes the main body of the drone and the main control unit that controls the normal operation of the various systems of the drone, and also includes an airbag device 5 that provides upward pulling force for the drone. The airbag device 5 is arranged above the main structure of the drone, and its interior is filled with light-density gas less dense than air, and the airbag device 5 is also connected with an exhaust device for discharging its internal gas capacity.

[0045] The airbag device 5 is a telescopic device whose volume changes with gas volume and gas pressure, and the material of the telescopic device is flexible fabric. Using flexible fabrics such as nylon fibers as the airbag device has a greater advantage in use. As a device that provides a s...

Embodiment 2

[0058] This embodiment is used in occasions where the unmanned aerial vehicle conducts flight operations under heavy load conditions.

[0059] Such as image 3 As shown, the drone device working under heavy load conditions includes the main body of the drone and the main control unit that controls the normal operation of the various systems of the drone, and also includes an airbag device 5 that provides upward pulling force for the drone. The airbag device 5 is arranged above the main structure of the drone, and its interior is filled with light-density gas less dense than air, and the airbag device 5 is also connected with an exhaust device for discharging its internal gas capacity.

[0060]The airbag device 5 is a telescopic device whose volume changes with gas volume and gas pressure, and the material of the telescopic device is flexible fabric. Using flexible fabrics such as nylon fibers as the airbag device has a greater advantage in use. As a device that provides a sou...

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Abstract

The invention belongs to the field of unmanned aerial vehicles and provides an unmanned aerial vehicle device on the heavy load condition and a control method. The unmanned aerial vehicle device on the heavy load condition comprises an unmanned aerial vehicle body structure and a master control unit controlling various systems of the unmanned aerial vehicle to be operated normally. The unmanned aerial vehicle device on the heavy load condition further comprises an air bag device providing upward tension for the unmanned aerial vehicle. The air bag device is arranged above the unmanned aerial vehicle body structure and filled with low-density gas with the density lower than that of air. The air bag device is further connected with an exhaust device for exhausting gas volume inside the air bag device. The tension generated by the air bag device is adjustable by controlling the gas volume inside the air bag device. According to the device, onboard energy consumption of an unmanned aerial vehicle on the heavy load condition is lowered, and the flight working time of the unmanned aerial vehicle is prolonged, so that the working efficiency of the unmanned aerial vehicle is achieved, the working time of the unmanned aerial vehicle on the heavy load condition is prolonged, the working range of the unmanned aerial vehicle on the heavy load condition is enlarged, and the defect that use of the unmanned aerial vehicle is limited on the heavy load condition is overcome.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle device and a control method working under heavy load conditions. Background technique [0002] UAV, also known as unmanned aircraft, remote control or self-cruising aircraft, is a low-cost, low-loss, and highly maneuverable aircraft that can carry loads. It has been widely used in military, scientific research, and civilian fields. . In the military field, UAVs can be used in enemy situation detection, communication relay, early warning, target training, etc., and can even directly form a UAV formation to fight against the enemy; in the field of scientific research, it can be used for flight test verification, new Feasibility simulation evaluation of equipment and new schemes, acquisition of aerial images, sampling and condition monitoring in harsh environments, etc.; in the civilian field, UAVs can be used for agricultural moisture monitoring, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64B1/58B64B1/62B64C27/08
CPCB64B1/58B64B1/62B64C27/08B64U10/30B64U10/10
Inventor 韦海成肖明霞潘俊涛张白王淼军
Owner BEIFANG UNIV OF NATITIES
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