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multi-purpose drone

A multi-purpose, unmanned aerial vehicle technology, applied in the direction of unmanned aircraft, rotorcraft, motor vehicles, etc., can solve the problems of accident-prone and single function of unmanned aerial vehicles, and achieve the effect of broad market space and convenient use

Active Publication Date: 2018-10-30
ZHOUSHAN JUYANG TECH DEV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The problem to be solved by the present invention is that the function of the unmanned aerial vehicle is single and easy to fail.

Method used

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Embodiment Construction

[0016] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0017] Multi-purpose large drone, including frame 1, wing 2, rotor propeller 3, carbon fiber rod 4, balloon 5, rotating rod 6, rotator 7, floater 8, parachute 9, trigger 10, control system 11 , camera 12, thermal imaging head 13, radar probe 14 and air pump 15, described frame 1 both sides is provided with wing 2, and wing 2 is equipped with small turbojet engine, provides powerful horizontal flight power; Frame 1 rear There is a rotating rod 6, and the wing 2 and the rotating rod 6 are provided with a rotor propeller 3 for vertical take-off and landing, and a carbon fiber rod 4 is arranged beside the rotor propeller 3, which has good elasticity; The upper part is provided with a rotator 7, a floater 8, a trigger 10 and a control system 11, the trigger 10 is provided with a parachute 9, and the rotator 7 is connected to two rotating rods 6, which can ad...

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Abstract

Multipurpose large UAV, belonging to the field of UAV equipment, including frame, wing, rotor propeller, carbon fiber rod, balloon, rotating rod, rotator, floater, parachute, trigger, control system, camera, thermal Imaging head, radar probe and air pump, there are wings on both sides of the frame, a rotating rod at the rear of the frame, rotor propellers for vertical take-off and landing are arranged on the wings and rotating rods, carbon fiber rods are arranged beside the rotor propellers, carbon fiber rods There is a balloon on the top of the frame, a rotator, a floater, a trigger, and a control system are installed on the upper part of the frame, a parachute is arranged on the trigger, the rotator is connected to two rotating rods, and a camera, a thermal imaging head, a radar, etc. are installed on the lower part of the frame. A probe and an air pump; the control system is connected with a rotator, a floater, a trigger, a camera, a thermal imaging head, a radar probe, and an air pump through wires, and the air pump is connected with a balloon.

Description

technical field [0001] The invention relates to a multipurpose large unmanned aerial vehicle, belonging to the field of unmanned aerial vehicle equipment. Background technique [0002] With the implementation of the ocean development strategy and the rapid economic development, drones are used more and more widely, but the current drones are generally small rotorcraft, which are basically used for short-distance land cruises and are prone to crashes The safety is poor, and it is more difficult to implement offshore operation tasks, which is an urgent problem to be solved at present. Contents of the invention [0003] The purpose of the present invention is to provide a multi-purpose large unmanned aerial vehicle. [0004] The problem to be solved by the present invention is the shortcoming that the unmanned aerial vehicle has a single function and is prone to accidents. [0005] For realizing the purpose of the present invention, the technical scheme that the present inv...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/02B64C27/08B64D45/00
CPCB64C27/08B64C39/02B64D45/00B64U50/12B64U10/10B64U2101/00
Inventor 方懂平
Owner ZHOUSHAN JUYANG TECH DEV
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