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Vectored thrust type unmanned aerial vehicle

A thrust type, unmanned aerial vehicle technology, applied in aircraft parts, aircraft control, flight direction control and other directions, can solve the problems of tail stall, unmanned aerial vehicle crash, unable to stop the unmanned aerial vehicle, etc., to improve maneuverability and shorten slippage. The effect of improving running distance and stealth performance

Inactive Publication Date: 2013-04-03
天津全华时代航天科技发展有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when the drone’s angle of attack gradually increases, the tail of the drone will fall into the low-energy wake of the wing, which may cause the tail to stall, and even cause the drone to enter a tail spin and cause a crash. At this time, even if the motor is working Normal, also unable to keep the drone balanced and stay in the air

Method used

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  • Vectored thrust type unmanned aerial vehicle
  • Vectored thrust type unmanned aerial vehicle

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Embodiment Construction

[0021] The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments. The following embodiments are only descriptive, not restrictive, and cannot limit the protection scope of the present invention.

[0022] A vector thrust UAV, comprising a propeller 1, a fuselage 2, a wing 3 and a tail 9, the propeller is coaxially installed at the front end of the longitudinal axis of the fuselage and is driven and controlled by a brushless motor installed in the fuselage. The wings are installed symmetrically on both sides of the middle part, and the tail wings are installed symmetrically on both sides of the tail part of the longitudinal axis of the fuselage. The innovation of the present invention lies in:

[0023] A vector thrust device is coaxially installed at the tail of the longitudinal axis of the fuselage. The vector thrust device includes a motor 4, a nozzle 5 and a nozzle diverter 6. The motor is installed ins...

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Abstract

The invention relates to a vectored thrust type unmanned aerial vehicle. The vehicle comprises propellers, a body, wings and empennages, wherein the propellers are coaxially mounted at the front end of a longitudinal shaft of the body; the wings are symmetrically mounted on two sides of the middle part of the body; the empennages are symmetrically mounted on two sides of the tail part of the body; a vectored thrust device is mounted at the tail part of the longitudinal shaft of the body, and comprises a motor and a spray pipe; the motor is mounted inside the body; and the front end of the spray pipe is connected with the motor, and the tail end of the spray pipe extends outside the tail end of the body. The vehicle has the advantages of scientific design, reasonable structure, strong controllability, quick taking-off and landing speed, good safety, small size, light weight and good maneuvering characteristic, can guarantee low-speed maneuvering flight in a state of high attack angle, can effectively improve the maneuverability, and can shorten the skating distance in the taking-off and landing process.

Description

technical field [0001] The invention belongs to the field of unmanned aerial vehicles, in particular to a vector thrust type unmanned aerial vehicle. Background technique [0002] The thrust acting on the UAV is a magnitude and direction quantity. This quantity is called a vector. Thrust vector technology is a technology that obtains additional steering torque by deflecting the direction of the motor jet. [0003] At present, the flight angle of attack of ordinary UAVs is relatively small. In this state, the wings and tails of UAVs can generate enough lift to ensure the normal flight of UAVs. However, when the angle of attack of the drone gradually increases, the tail of the drone will fall into the low-energy wake of the wing, which may cause the tail to stall, or even cause the drone to enter a tail spin and cause a crash. At this time, even if the motor works Normal, also can't get the drone to balance and stay in the air. [0004] After searching, the following related...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C15/02
Inventor 权军田凯
Owner 天津全华时代航天科技发展有限公司
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