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Built-in V tail vane surface driving mechanism

A drive mechanism, built-in technology, applied in aircraft parts, aircraft control, transportation and packaging, etc., can solve problems such as inability to modularize design and troublesome installation

Active Publication Date: 2016-01-20
深圳飞马机器人科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The rudder surface of the UAV's conventional V-tail is driven by the steering head and the drive paddle. The drive connecting rod is installed in a leaky way, which cannot be modularized and the installation is troublesome.

Method used

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  • Built-in V tail vane surface driving mechanism
  • Built-in V tail vane surface driving mechanism

Examples

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Embodiment Construction

[0015] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0016] This embodiment provides a built-in V-tail rudder surface drive mechanism, such as figure 1 and figure 2 As shown, the built-in V-tail rudder surface driving mechanism includes a fuselage 104 and a rudder surface 101, wherein an integral frame 113 is fixedly arranged in the fuselage, and the integral frame 113 is provided with a steering gear placement position 119 and a steering gear placement position 120, wherein , the steering gear placement position 119 is used to install the steering gear 114, and the steering gear placement position 120 is used to install the steering gear 117, and each steering gear is connected to the first rotating arm, wherein the first rotating arm is a steering gear piece, for example, The steering gear 117 is connected with the steering gear piece 116 .

[0017] The overall frame 113 is also equipped w...

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Abstract

The invention discloses a built-in V tail vane surface driving mechanism. The built-in V tail vane surface driving mechanism comprises a machine body and a vane surface. Steering engines for providing driving power, first tumblers for being connected with the steering engines, a second tumbler for driving the vane surface, a third tumbler for being in transmission driving connection with the second tumbler, and connecting rods for being in transmission connection with the first tumbler and the third tumbler are arranged in the machine body. The first tumblers are steering engine pieces for connecting the steering engines with the connecting rods, the second tumbler is a driving stirring piece directly connected with the vane surface in a matched mode and used for driving the vane surface, and the third tumbler is a shaft seat transmission stirring piece and is in driving connection with the driving stirring piece through an arranged stirring piece connecting shaft. The built-in V tail vane surface driving mechanism is convenient to assemble, more reliable in driving and more attractive in appearance, and the internal space of the machine body can be more effectively utilized through modular installation of an overall framework.

Description

technical field [0001] The invention relates to a mechanical structure, in particular to a built-in V-tail rudder surface driving mechanism. Background technique [0002] The rudder surface of the UAV's conventional V-tail is driven by the steering head and the drive paddle. The drive connecting rod is installed in a leaky way, which cannot be modularized and the installation is more troublesome. [0003] Therefore, there are defects in the prior art and need to be improved. Contents of the invention [0004] The technical problem to be solved by the present invention is to provide a built-in V-tail rudder surface drive mechanism with a more beautiful appearance, a more modular mechanism, a more reliable drive, and a more effective use of the internal space of the fuselage. [0005] The technical scheme of the present invention is as follows: a built-in V-tail rudder surface drive mechanism, including a fuselage and a rudder surface, the inside of the fuselage is provided...

Claims

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Application Information

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IPC IPC(8): B64C9/02
Inventor 崔艳鸿
Owner 深圳飞马机器人科技有限公司
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