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Aircraft wing mounting tool

A wing and aircraft technology, applied in the field of aircraft wings, can solve problems such as inconvenient wing installation, and achieve the effect of avoiding shaking

Pending Publication Date: 2022-07-29
西安建卓航空机械制造有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, when the above-mentioned device is in use, it is necessary to install wings of different sizes, and it is not convenient to install wings of different sizes due to the fixed connection between the wing profile frame plate and the mounting table.

Method used

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  • Aircraft wing mounting tool
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Embodiment Construction

[0032] The technical solution of the present patent will be described in further detail below in conjunction with specific embodiments.

[0033] Embodiments of the present patent are described in detail below, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present patent, but should not be construed as a limitation on the present patent.

[0034] In the description of this patent, it should be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", The orientation or positional relationship indicated by "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the ...

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PUM

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Abstract

The invention discloses an aircraft wing mounting tool and belongs to the technical field of aircraft wings, the aircraft wing mounting tool comprises a workbench and a wing-shaped frame plate, an adjusting groove of a T-shaped structure is formed in the top of the workbench, adjusting blocks of a T-shaped structure are slidably connected to the two sides of the inner wall of the adjusting groove, and placing blocks are fixedly connected to the tops of the adjusting blocks; a fixing rod is fixedly connected to the bottom of the wing-shaped frame plate, a fixing groove which is in sliding fit with the fixing rod and is matched with the fixing rod is formed in the top of the placing block, limiting mechanisms are fixedly connected to the two sides of the fixing rod, each limiting mechanism comprises a plurality of evenly-distributed limiting springs, limiting grooves are formed in the two sides of the fixing rod, and the limiting springs are arranged in the limiting grooves. One end of the limiting spring is fixedly connected with the inner wall of one side of the limiting groove, and the other end of the limiting spring is fixedly connected with a limiting block in sliding fit with the inner wall of the limiting groove. According to the wing mounting device, the effect of conveniently mounting wings with different sizes can be achieved.

Description

technical field [0001] The invention belongs to the technical field of aircraft wings, in particular to an aircraft wing installation tool. Background technique [0002] The wing is one of the important parts of the aircraft, which is installed on the fuselage. Its main function is to generate lift, and at the same time, ammunition compartments and fuel tanks can be arranged in the wings, and the landing gear can be stored during flight. In addition, flaps for improving take-off and landing performance and ailerons for lateral control of the aircraft are also installed on the wings, and some are also equipped with slats and other lift-increasing devices on the leading edge of the wings. In the production of hardware parts An aircraft wing mounting tool is required. [0003] In the prior art, an aircraft wing installation tool generally includes an installation platform, and the top of the installation platform is fixedly connected to an airfoil frame plate by screws. [0...

Claims

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Application Information

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IPC IPC(8): B25B27/00B25B11/02
CPCB25B27/00B25B11/02
Inventor 武晓平
Owner 西安建卓航空机械制造有限公司