Vertical take-off and landing rotary wing type unmanned aerial vehicle

An unmanned aerial vehicle and vertical take-off and landing technology, applied in the field of unmanned aerial vehicles, can solve the problems of low maneuverability, high site requirements, and poor versatility, and achieve the effects of maneuverability, low purchase cost, and strong versatility

Active Publication Date: 2014-05-21
甘肃神龙航空科技有限公司
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Existing high-altitude operations, whether it is high-altitude spraying of pesticides in agricultural applications, or high-altitude imaging and other applications, all use manned aircraft. Not only is the cost

Method used

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  • Vertical take-off and landing rotary wing type unmanned aerial vehicle
  • Vertical take-off and landing rotary wing type unmanned aerial vehicle
  • Vertical take-off and landing rotary wing type unmanned aerial vehicle

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Embodiment Construction

[0019] 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, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0020] Such as figure 1 , figure 2 A kind of vertical take-off and landing rotor type unmanned aerial vehicle shown, mainly comprises main frame assembly 10, engine group 40, rotor assembly 20, tail drive assembly 30 and collective distance slider group 60; Said main frame assembly 10 includes a main shaft 101 and upper side plates 102 arranged on both sides of the main shaft 101. The main shaft 101 is located at the center of the machine; the two upper side plat...

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Abstract

The invention relates to the field of unmanned aerial vehicles, and in particular discloses a vertical take-off and landing rotary wing type unmanned aerial vehicle. The vertical take-off and landing rotary wing type unmanned aerial vehicle comprises a main frame assembly, an engine unit, a rotary wing assembly, a tail drive assembly and a total distance sliding block group, wherein the main frame assembly comprises a main shaft and two upper side plates oppositely arranged at two sides of the main shaft, the two upper side plates are fixedly connected with two lower side plates, a facility frame is connected with the two lower side plates and is provided with a drive unit, and the main shaft is vertically connected with the drive unit; the engine unit comprises an engine and a silencer connected with the engine, and the engine is a single-cylinder engine with displacement of 26CC. The vertical take-off and landing rotary wing type unmanned aerial vehicle disclosed by the invention has the advantages that the effective load of the aerial vehicle can achieve 5KG, the aerial vehicle is capable of vertically taking off and landing, has low requirements on floor space and has no requirement on special take-off/landing field or runway, the flying speed and height can be freely controlled, the manufacturing cost is low, the flexibility and the universality are high, and the operation of pilots is safe.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a vertical take-off and landing rotor type unmanned aerial vehicle. Background technique [0002] At present, the conventional high-altitude operations are mainly manned aerial vehicles, but the take-off and landing are limited by the site during the operation, and due to the large shape, the aerial flight cannot operate in the complex surrounding environment. With the acceleration of the opening of my country's low-altitude field and the reform of the airspace management system, as well as people's understanding of efficient operations, the application of unmanned aerial vehicles is becoming more and more extensive. Whether it is applied in the field of national defense transportation or in the field of agricultural and forestry scientific research, from the perspective of operational accuracy, flight controllable range and application fields, the development and applicat...

Claims

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Application Information

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IPC IPC(8): B64C29/02B64C27/02B64C27/52B64C25/04
Inventor 郭云艳邱程杨志杰李青富
Owner 甘肃神龙航空科技有限公司
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