Novel efficient tilt rotor unmanned aerial vehicle

A technology of unmanned aerial vehicles and tilt rotors, applied in the field of aviation products, can solve the problems of reduced aircraft aerodynamic efficiency, poor control performance, low efficiency of vertical rotors, etc., to achieve enhanced pitch control performance, enhanced heading control performance, and improved battery life the effect of time
CN108382579APending Publication Date: 2018-08-10北京天宇新超航空科技有限公司

Patent Information

Authority / Receiving Office
CN · China
Current Assignee / Owner
北京天宇新超航空科技有限公司
Publication Date
2018-08-10

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Abstract

The invention discloses a novel efficient tilt rotor unmanned aerial vehicle. Unmanned aerial vehicle layout has higher aerodynamic efficiency and better level-flight longitudinal direction and coursecontrol performance, and high-speed and high-efficiency flight can be achieved on the premise of vertical take-off and landing. The unmanned aerial vehicle comprises tilt rotors, vertical flight mechanisms, fixed wings, a fixed vertical fin, a stabilator, a body structure and a landing gear. The unmanned aerial vehicle needs to experience a vertical flight state, a transition flight state and a level flight state from take-off to level flight. The tilt rotors and the vertical flight mechanisms can rotate through an actuation mechanism, so that the unmanned aerial vehicle can vertically take off and horizontally fly at high speed, the tilt rotors can change a distance, take account of rotating efficiency in the vertical flight state and the level flight state and drive the unmanned aerialvehicle to fly at high speed, the vertical flight mechanisms and the tilt rotors collectively provide lift force and control force of vertical take-off and landing in the vertical flight state, the vertical flight mechanisms are stored on two sides of a body in the level flight state, and a good aerodynamic shape of the unmanned aerial vehicle is kept.
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Description

technical field

[0001] The invention relates to a tilt rotor vertical take-off and landing aircraft, which belongs to the technical field of aviation products. Background technique

[0002] The tilt-rotor unmanned aerial vehicle has both the vertical take-off and landing capability of the helicopter and the high-speed flight performance of the propeller fixed-wing aircraft, and belongs to the vertical take-off and landing aircraft. The direction of the dynamic force of the tilt-rotor unmanned aerial vehicle can be tilted, and it has a wide range of application prospects. The main applications include logistics, line inspection, forest fire prevention, and environmental monitoring. Although the tilt-rotor unmanned aerial vehicle can meet the application requirements of some special scenarios, there are still problems such as low vertical rotor efficiency, poor control performance and low aerodynamic efficiency in practical applications. For example: 1. The existing tilt-roto...

Claims

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