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Unmanned aerial vehicle

A technology of unmanned aerial vehicle and fuselage, applied in the field of aircraft and unmanned aerial vehicle, can solve the problems of unstable flight process, easy to shake when taking off and landing, etc.

Active Publication Date: 2016-04-20
北京合众泰达科技有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the continuous development of science and technology, drone technology has been greatly improved in recent years, and many intelligent and multi-functional unmanned aerial vehicles have appeared, but there are still some problems in drone technology, such as the flight process Stable, easy to shake during lifting and landing

Method used

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Embodiment Construction

[0014] The present invention will be further described below in conjunction with specific embodiments. The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not as a limitation to the present invention.

[0015] Such as figure 1 , figure 2 , image 3 As shown, an unmanned aerial vehicle comprises a nose 4, a fuselage 1, a tail 3, and two wings 2, the nose 4 is fixedly mounted on the end of the fuselage 1, and the tail 3 is fixedly mounted on the fuselage 1 tail, the length directions of nose 4, fuselage 1 and tail 3 are located on the same straight line. The two side wings 2 are respectively fixedly installed on both sides of the fuselage 1 . The front and rear of the fuselage 1 are respectively provided with mounting holes perpendicular to the longitudinal direction of the fuselage 1. The front rotor 14 is installed in the mounting holes at the front of the fuselage 1, and the axis of the front rotor 14 is colli...

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Abstract

The invention discloses an unmanned aerial vehicle. The unmanned aerial vehicle comprises a nose, a fuselage, an empennage and two side wings and is characterized in that the nose is fixedly mounted at one end of the fuselage, the empennage is fixedly mounted at the tail of the fuselage, and length directions of the nose, the fuselage and the empennage are located in the same straight line; the two side wings are fixedly mounted on two sides of the fuselage; a mounting box is arranged in the middle of the fuselage, a control system is mounted inside the mounting box, a battery is mounted inside of the mounting box of the fuselage, and a mounting box electric push rod, front wheel taking-off and landing electric push rods, rear wheel taking-off and landing electric push rods, a front rotor motor, a middle rotor motor, a rear rotor motor and side rotor motors are connected with the control system and the battery inside the mounting box of the fuselage through wires respectively. The unmanned aerial vehicle can run stably, and telescopic amounts of the front wheel taking-off and landing electric push rods and the rear wheel taking-off and landing electric push rods can be adjusted in real time, so that the unmanned aerial vehicle can be adapted to different terrains.

Description

technical field [0001] The invention relates to an aircraft, in particular to an unmanned aerial vehicle, and belongs to the technical field of flight machinery equipment. Background technique [0002] With the continuous development of science and technology, drone technology has been greatly improved in recent years, and many intelligent and multi-functional unmanned aerial vehicles have appeared, but there are still some problems in drone technology, such as the flight process Stable, easy to shake during lifting and landing. Contents of the invention [0003] In view of the above problems, the present invention provides an unmanned aerial vehicle, which realizes the purpose of stable operation of the unmanned aerial vehicle under high-speed flight by setting front, middle, rear, left and right symmetrical power sources. [0004] The technical scheme adopted by the present invention is: an unmanned aerial vehicle, comprising a nose, a fuselage, a tail, and two side win...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/28B64C25/24
CPCB64C25/24B64C27/26B64C27/28B64U10/25B64U30/20B64U50/19B64U2101/30
Inventor 不公告发明人
Owner 北京合众泰达科技有限公司
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