Vertical take-off and landing unmanned aerial vehicle increase lift control device and control method thereof

A technology of vertical take-off and landing and control device, which is applied to vertical take-off and landing aircraft, motor vehicles, wing adjustment and other directions, and can solve the problems of small range and low flying speed of drones.

Active Publication Date: 2017-02-01
厦门腾希航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] If the pulling force and lift force are all provided by the power plant during the flight, it will cause the UAV to fly at a low speed and range.

Method used

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  • Vertical take-off and landing unmanned aerial vehicle increase lift control device and control method thereof
  • Vertical take-off and landing unmanned aerial vehicle increase lift control device and control method thereof
  • Vertical take-off and landing unmanned aerial vehicle increase lift control device and control method thereof

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Embodiment Construction

[0024] Such as Figure 1~4 As shown, the embodiment of the vertical take-off and landing UAV increased lift control device is provided with a pair of folding drive motors 5, a pair of foldable flaps 6, a fuel sensor 7, a cargo delivery sensor 8, and a flight control system 9.

[0025] The vertical take-off and landing UAV is provided with a pair of propeller engines 1, a wing-body fusion flight wing 2, an adjustable vertical tail 3, and a pair of adjustable horizontal tails 4; On the left and right sides of the front end, the propeller engine 1 is used to provide the pulling force required for the flight of the UAV, the wing-body fusion flight wing 2 is used to provide lift for the UAV in level flight, and the adjustable vertical tail 3 is located on the wing-body fusion flight wing 2. At the top of the rear end, a pair of adjustable horizontal tail fins 4 are arranged on the left and right sides of the rear end of the wing-body fusion flying wing 2; the left flying wing fulcr...

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Abstract

The invention relates to a vertical take-off and landing unmanned plane lift augmentation control device and a vertical take-off and landing unmanned plane lift augmentation control method, and relates to a vertical take-off and landing unmanned plane. The control device is provided with foldable drive motors, foldable wing flaps, an oil amount sensor, a cargo dispensing amount sensor and a flight control system, wherein the foldable drive motors and the foldable wing flaps are arranged in compartments at two sides of wing body fused flying wings; the output end of the oil amount sensor and the output end of the cargo dispensing amount sensor are connected with the input end of the flight control system, the output end of the flight control system is connected with the foldable drive motor, and the oil amount sensor, the cargo dispensing amount sensor and the flight control system are arranged in the wing body fused flying wings. By adopting the vertical take-off and landing unmanned plane lift augmentation control device, an unmanned plane can vertically take off and land, hover, inversely fly and make spot turn, the mobility is good, and the requirement on the take-off and landing condition is relatively low; the cruising ability is strong, and the unmanned plane is suitable for the flight task with relatively high requirement for the flight hour; the unmanned plane is good in stability and is suitable for carrying an automatic driverscope, an airborne camera and a to-be-dispensed material resources; under a level flight state, the lift area can be adjusted along with the variation of the gravity.

Description

technical field [0001] The invention relates to a vertical take-off and landing unmanned aerial vehicle, in particular to a vertical take-off and landing unmanned aerial vehicle increasing control device and a control method thereof. Background technique [0002] An unmanned aircraft is an unmanned aircraft whose flight is controlled by a remote control device or an on-board program control device. Because of its wide range of uses, simple structure, good cost-effectiveness, no risk of casualties, and good maneuverability, it plays an extremely important role in modern warfare and has broad prospects in the civilian field. [0003] At present, the take-off methods of UAVs mainly include zero-length launch, slide-rail launch, vehicle roll-out, landing gear roll-out, parent aircraft air release, container-type launcher launch, hand throw, and vertical take-off. Among them, UAVs that take off vertically require the smallest take-off site area and are not restricted by terrain ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C3/56B64C39/10B64C29/00
Inventor 郑云隆滕健欧阳智贤潘成剑周驯黄尤延铖
Owner 厦门腾希航空科技有限公司
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