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Aircraft tire mounting device

An installation device, a technology for aircraft tires, applied in tire installation, aircraft parts, ground devices, etc., can solve the problem of inability to fine-tune the axial position of aircraft tires, and achieve the effect of improving accuracy

Inactive Publication Date: 2020-06-05
荆门怡盛源环保科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The main purpose of the present invention is to provide an aircraft tire installation device to solve the problem that the axial position of the tire needs to be fine-tuned during the installation process, and the prior art cannot realize the fine-tuning of the axial position of the aircraft tire

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Embodiment Construction

[0031] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0032] It should be pointed out that the following detailed description is exemplary and intended to provide further explanation to the present application. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs.

[0033] For the convenience of description, spatially relative terms may be used here, such as "on ...", "over ...", "on the surface of ...", "above", etc., to describe the The spatial positional relationship between one device or feature shown and other devices or features. It will be understood that the spatially relative terms are intended to encomp...

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Abstract

The invention provides an aircraft tire mounting device. The aircraft tire mounting device comprises a base; an arc-shaped seat; a sliding guide rail is arranged in an inner cavity of the base, the arc-shaped base is arranged on the sliding guide rail in a sliding mode, an arc-shaped protective plate is connected to the inner side of the arc-shaped base in a sliding mode, and an arc-shaped clamping plate is fixedly arranged at the top of the arc-shaped protective plate. An arc-shaped sliding groove is formed in the inner side wall of the arc-shaped base, and a sliding strip block matched withthe sliding groove is fixedly arranged on the outer side wall of the arc-shaped protective plate. A telescopic mechanism is further fixedly arranged on the inner wall of the base, and the output end of the telescopic mechanism is fixedly connected with the outer side wall of the arc-shaped seat; a butt joint mechanism is arranged on the side wall of one side of the arc-shaped protective plate andcomprises first driving blocks symmetrically arranged on the side wall of the arc-shaped protective plate. According to the technical scheme, the problem that in the prior art, when the axial positionof the tire needs to be finely adjusted in the installation process, the function of finely adjusting the axial position of the aircraft tire cannot be achieved is effectively solved.

Description

technical field [0001] The invention relates to the technical field of aircraft tire clamping and lifting equipment, in particular to an aircraft tire mounting device. Background technique [0002] Aircraft tires can be tubed or tubeless. They support the weight of the aircraft on the ground while creating the necessary traction for braking and stopping the aircraft. The tires also help absorb shock during landing and cushion take-off, roll-out and the influence of the ground roughness when gliding. [0003] When aircraft tires break down and need to be repaired or aircraft wheels are installed, due to their large mass, it is difficult to lift them manually, and in the process of lifting the tires, they often shake or even slip due to loose clamping. Therefore, Additional devices are required to clamp and lift the tires so that the tires can be moved to the position of the mounting shaft of the aircraft landing gear. The patent application number is 201810560720.1, and the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B60B29/00B64F5/50
CPCB60B29/001B60B29/002B64F5/50
Inventor 黄振梅冯可云赵子敬张延瑞李卫军
Owner 荆门怡盛源环保科技有限公司
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