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

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Problems solved by technology

[0003] However, it is rare for existing U

Method used

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  • Tilting horizontal tail with power mechanism
  • Tilting horizontal tail with power mechanism

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

[0020] Reference figure 1 , 2 The illustrated tiltable horizontal tail fin with a power mechanism includes an aircraft body 1 on which a vertical tail wing 2 forming an integrated structure is also provided. The tail of the aircraft body 1 is also provided with a main body part and a tilting flat tail 3 arranged perpendicularly to the aircraft body 1. The tilting flat tail 3 includes two vertical tail fins 2 penetrating through the vertical tail 2 and two ends of the vertical tail fin 2 respectively. The flat tail beam 31 on the side and the horizontal tail wing 32 fixedly installed on the flat tail beam 31.

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

[0022] A conne...

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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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