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Multi-rotor unmanned aerial vehicle aerial throwing fixed wing takeoff mechanism

A multi-rotor UAV and fixed-wing technology, applied in the direction of rotorcraft, aircraft parts, aircraft, etc., can solve the problems of high cost, weak maneuverability, and large occupied space, so as to improve the success rate, slow down the flight speed, The effect of convenient personnel control

Inactive Publication Date: 2019-05-28
智飞智能装备科技东台有限公司
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Traditional fixed-wing UAVs accelerate take-off through the runway, which takes up a lot of space, high cost, limited by the site, and weak maneuverability

Method used

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  • Multi-rotor unmanned aerial vehicle aerial throwing fixed wing takeoff mechanism
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  • Multi-rotor unmanned aerial vehicle aerial throwing fixed wing takeoff mechanism

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Embodiment Construction

[0024] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0025] see Figure 1-Figure 7As shown, the present invention provides a technical solution: a multi-rotor unmanned aerial vehicle throwing fixed-wing take-off mechanism, including a multi-rotor unmanned aerial vehicle 1, a mounting mechanism 2 and a fixed-wing unmanned aerial vehicle 3. A controller is arranged in the man-machine 1, and a mounting mechanism 2 is installed on the body of the multi-rotor UAV 1, and the top of the mounting mechanism...

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Abstract

The invention discloses a multi-rotor unmanned aerial vehicle aerial throwing fixed wing takeoff mechanism. The multi-rotor unmanned aerial vehicle aerial throwing fixed wing takeoff mechanism comprises a multi-rotor unmanned aerial vehicle, a mounting mechanism and a fixed wing unmanned aerial vehicle; the mounting mechanism is arranged on the body of the multi-rotor unmanned aerial vehicle; thetop of the mounting mechanism is fixed below the body of the multi-rotor unmanned aerial vehicle through screws; a mounting mechanism battery and a mounting mechanism remote control signal controllerare arranged on the inner left side of the mounting mechanism; and the fixed wing unmanned aerial vehicle is arranged below the mounting mechanism. The multi-rotor unmanned aerial vehicle hangs the fixed wing unmanned aerial vehicle below the multi-rotor unmanned aerial vehicle through the mounting mechanism, a ground unmanned aerial vehicle operator uses a remote controller to transmit an instruction to the mounting mechanism after the multi-rotor unmanned aerial vehicle vertically ascends to a certain height, the mounting mechanism separates the fixed wing unmanned aerial vehicle in the air,and the fixed wing unmanned aerial vehicle enters a cruising task state, so that the site requirement of runway takeoff is omitted, the responsible mechanism of a catapult launcher is omitted, the fixed wing unmanned aerial vehicle can be mounted and taken off continuously and big motorized advantage is achieved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a multi-rotor unmanned aerial vehicle air-throwing fixed-wing take-off mechanism. Background technique [0002] UAVs refer to unmanned aircraft controlled by wireless remote control equipment and their own control devices, such as unmanned helicopters, fixed-wing UAVs, and unmanned paragliders. In the past ten years, drones have been widely used in aerial photography, power inspection, environmental monitoring, forest fire prevention, disaster inspection, anti-terrorism lifesaving, military reconnaissance, battlefield assessment and other fields. [0003] Traditional fixed-wing UAVs are accelerated to take off through the runway, which takes up a lot of space, high cost, limited by the site, and weak in maneuverability. Contents of the invention [0004] The purpose of the present invention is to provide a multi-rotor unmanned aerial vehicle throwing fixed-win...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D5/00B64D17/80B64C27/08B64C27/20
Inventor 朱银广朱毅原军锋周旭寅谢锐杨
Owner 智飞智能装备科技东台有限公司
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