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Tilting horizontal tail with power mechanism

A technology of horizontal tail and power mechanism, which is applied in the field of aircraft and can solve the problems of rare tail tilting

Inactive Publication Date: 2016-03-23
SHANGHAI YOUZU INTELLIGENT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, it is rare for existing UAVs to realize tail tilting during flight.

Method used

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Embodiment Construction

[0019] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific embodiments.

[0020] refer to figure 1 , 2 The shown tiltable horizontal tail with a power mechanism includes an aircraft body 1 on which a vertical tail 2 forming an integrated structure is also arranged. The tail portion of the aircraft body 1 is also provided with a main body part and the inclined horizontal tail 3 which is arranged vertically on the aircraft body 1. The flat tail beam 31 on the side, and the horizontal empennage 32 fixedly installed on the flat tail beam 31.

[0021] Wherein, an actuator 4 for driving the horizontal tail beam 31 to rotate is also installed inside the vertical tail 2;

[0022] A connecting rod 33 that can rotate synchronously with the flat tail beam 31 is respectively fixed on the flat tail beam 31 on both sides of the ve...

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Abstract

The invention relates to a tilting horizontal tail with a power mechanism. The tilting horizontal tail comprises an aircraft body, a vertical tail and a tilting flat tail, wherein the vertical tail and the tilting flat tail are arranged on the aircraft body. The tilting horizontal tail is characterized in that the tilting flat tail comprises a flat tail beam penetrating the vertical tail and horizontal tail bodies arranged on the flat tail beam, and an actuator used for driving the flat tail beam to rotate is further arranged in the vertical tail. The tilting horizontal tail has the beneficial effects that the actuator arranged in the vertical tail is used for driving the flat tail beam penetrating the vertical tail to rotate, so that the horizontal tail bodies, connecting rods and a propeller engine are driven by the flat tail beam to tilt or stop at any angle, and the overall coordination and functional diversity of an aircraft are achieved through the lifting power or thrust power of the propeller engine.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a tiltable horizontal tail with a power mechanism. Background technique [0002] With the rapid development of science and technology and the continuous increase of various special needs, aircraft, especially unmanned aerial vehicles, have been widely used in recent years. [0003] However, it is rare for existing unmanned aerial vehicles to realize tail tilting during flight. It has been confirmed by research that the tilting of the UAV tail is very beneficial to the overall coordination performance. [0004] In order to solve the above problems and achieve the goal, the inventor of the present invention invented a tiltable horizontal tail with a compact structure and a power mechanism, which is widely applicable to aircraft. Contents of the invention [0005] The object of the present invention is to provide a tiltable horizontal tail with a power mechanism, which has scie...

Claims

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Application Information

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IPC IPC(8): B64C5/10B64D27/02
CPCB64C5/10B64D27/02
Inventor 郭士钧王鹂辉温求遒贺媛媛
Owner SHANGHAI YOUZU INTELLIGENT TECH CO LTD
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