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A multi-rotor UAV system suitable for stable delivery under high-speed flight conditions

A multi-rotor UAV and UAV technology, which is applied in the direction of rotorcraft, aircraft stability, aircraft, etc., can solve the problems that the reliable automatic control of the deployment process cannot be realized, and the UAV cannot fly at a high speed, so as to achieve high safety , flexible effect

Active Publication Date: 2022-02-22
侯志强
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This patent solution only considers the application method of high-altitude delivery, and the deployment of the drone is completely done by means of a parachute, which cannot achieve reliable automatic control of the deployment process, so it cannot be directly applied to delivery methods such as carrier delivery or power-assisted push. , and the UAV cannot fly at high speed

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  • A multi-rotor UAV system suitable for stable delivery under high-speed flight conditions
  • A multi-rotor UAV system suitable for stable delivery under high-speed flight conditions
  • A multi-rotor UAV system suitable for stable delivery under high-speed flight conditions

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Embodiment Construction

[0026] In order to make the purpose, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0027] Such as figure 1 As shown, a multi-rotor UAV system suitable for stable delivery under high-speed flight conditions includes a flight control mechanism 1 and a multi-rotor configurable UAV 2 . Among them, the flight control mechanism 1 can guarantee the high-speed and stable flight of the UAV after it is carried by the carrier or power-assisted, and can adjust the attitude and speed of the UAV during high-speed flight; the multi-rotor variable configuration UAV 2. After the high-speed flight, it can be deployed autonomously to perform corresponding tasks for the multi-rotor UAV.

[0028] Such as figure 2As shown, the flight control mechanism 1 is sequentially divided into a detachable rectifying shape device 101 , a tail cabin 104 and a ...

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Abstract

The invention relates to a multi-rotor unmanned aerial vehicle system suitable for stable delivery under high-speed flight conditions, including a flight control mechanism and a multi-rotor variable-configurable unmanned aerial vehicle. Composed of a multi-rotor configurable UAV located inside the detachable rectification shape device, including a working load, a main control unit and a power supply unit, the outer periphery of the multi-rotor configurable UAV is equipped with a configurable rotor structure, The variable rotor structure can be folded and opened automatically, and the flight control mechanism can ensure the high-speed and stable flight of the UAV after it is carried by the carrier or powered by power, and can adjust the attitude and speed of the UAV during high-speed flight , the multi-rotor configurable UAV can autonomously deploy as a multi-rotor UAV to perform corresponding tasks after flying to the sky above the target area at high altitude and high speed.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a system suitable for stably launching unmanned aerial vehicles under high-speed flight conditions. Background technique [0002] In the existing military and civilian fields, drones have gradually become a new type of machine that is safe, stable, efficient and has great potential, and have begun to be widely used in various types of tasks such as reconnaissance, surveillance, search and rescue, and assessment. . Due to the characteristics of stable hovering, high safety, and flexible maneuvering, micro-miniature multi-rotor UAVs are more suitable for carrying out reconnaissance and interference tasks. However, due to the low power and slow speed of such drones, they cannot perform medium and long-distance missions. In order to give full play to the characteristics of the micro multi-rotor UAV and improve its range of action, the micro multi-rotor UAV can be t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/02B64C27/08B64C1/30B64C7/00B64C5/10
CPCB64C1/30B64C5/10B64C7/00B64C27/08B64C39/02
Inventor 侯志强王鹏芦丹林宏杰
Owner 侯志强