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Flexible wallboard assembling tool

A technology of assembly tooling and flexible wall panels, which is applied in aircraft assembly and other directions, can solve problems such as inability to respond quickly to panels, backward aircraft assembly technology, and increased aircraft manufacturing costs, achieving shortened production preparation cycles, high positioning accuracy, and easy maintenance Effect

Inactive Publication Date: 2020-03-27
ZHEJIANG UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, compared with foreign countries, my country's aircraft assembly technology is still relatively backward, and the current assembly level is increasingly unable to meet the requirements of modern society for aircraft long life and high reliability.
In the field of panel assembly, the domestic aviation industry mostly uses a traditional rigid tooling model in which a set of tooling corresponds to a set of panel components. Rigid tooling cannot quickly respond to different types of panel, which increases aircraft manufacturing costs, prolongs production cycles, and reduces Enterprise benefits, and the positioning accuracy is low, and the accumulation of assembly errors is relatively large

Method used

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  • Flexible wallboard assembling tool

Examples

Experimental program
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Effect test

Embodiment

[0048] See figure 1 The flexible wall panel assembly tool of this embodiment includes a base, and the base is provided with a processing station, an assembly station, and a hole-making station. The base includes a first fixed base 1 and a second fixed base 6 that are perpendicular to each other. The first fixed base 1 is equipped with a skin adsorption unit 2 through an X-direction sliding table 8, and the second fixed base 6 is installed with a Y-direction sliding platform 7. Wall panel frame positioning assembly 5. The skin 3 is fixed by the skin adsorption unit 2, and the wall plate frame 4 is fixed by the wall plate frame positioning assembly 5, and the assembly process is performed at the assembly station.

[0049] See figure 2 , The first fixed base 1 is provided with a limit block 101, a limit block 106, an X-direction guide rail 103, a slider 104, a limit switch 105, a guide rail protective cover 107, a screw fixing seat 108, an X-direction screw 109 and a servo Motor 1...

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Abstract

The invention discloses a flexible wall plate assembling tool e, which belongs to the technical field of aircraft digital assembly. The tool comprises a base provided with a processing station, an assembly station and a drilling station, and an X-direction sliding table which is arranged on the base, slides between the processing station and the assembly station, is movably arranged on the base along the X direction, and is provided with a skin adsorption unit for fixing a skin; a Y-direction sliding table which slides between the assembly station and the drilling station; a base which is movably mounted on the base along the Y direction; wherein the Y-direction sliding table is provided with a wall plate frame positioning assembly for fixing the wall plate frame. The wallboard frame positioning assembly comprises a plurality of positioners which are oppositely arranged, each positioner comprises a fixing frame which is connected with the wallboard frame and has three-axis freedom degrees, an X-direction driving mechanism, a Y-direction driving mechanism and a Z-direction driving mechanism, and the X-direction driving mechanism, the Y-direction driving mechanism and the Z-directiondriving mechanism are used for driving the fixing frames and used for adjusting the position of the wallboard frame. Based on digital control technology, compared with a positioning mode of a traditional rigid tool, the digital positioning precision is greatly improved.

Description

Technical field [0001] The invention relates to the technical field of aircraft digital assembly, in particular to a flexible wall panel assembly tool. Background technique [0002] The aircraft siding structure is the basic structure of the aircraft fuselage, and its assembly quality directly affects the aerodynamic layout and appearance of the aircraft body, and indirectly affects the flight safety and service life of the aircraft. The skin is an important part of the aircraft siding structure and also the positioning reference for the assembly of the siding structure. [0003] Aircraft assembly is an important part of the aircraft manufacturing process, and the assembly quality directly affects the final quality, cost and production cycle of the aircraft. The assembly of siding components is an important part of aircraft assembly. The assembly quality of siding components directly affects the subsequent assembly quality of fuselage and wings, which is the basis for ensuring the...

Claims

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Application Information

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IPC IPC(8): B64F5/10
CPCB64F5/10
Inventor 方强郝巨张程常颂扬耿慧曹玉进王鸿昇刘航王天
Owner ZHEJIANG UNIV
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