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Standard sample bonding tool

A standard sample and bonding technology, which is applied in the direction of workpiece clamping device, test sample preparation, sampling, etc., can solve the problems of failure to meet the precision requirements of ASTMC297, damage to the mechanical properties of the bonded structure, and the movement of bonded samples, etc. problem, to achieve the effect of adjustable adhesive force, simple structure and high bonding efficiency

Inactive Publication Date: 2019-11-29
THE RES INST FOR SPECIAL STRUCTURES OF AERONAUTICAL COMPOSITE AVIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the adhesive needs a certain amount of time to solidify, the force of the workpiece during the clamping process is prone to dislocation of the bonding sample, resulting in poor bonding accuracy, which cannot meet the accuracy requirements of ASTM C297
However, the method of rough bonding first and then finishing the shape can ensure the final dimensional accuracy, but the secondary mechanical stress on the bonded parts will destroy the mechanical properties of the original bonded structure and affect the final test results.

Method used

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Embodiment Construction

[0021] The present invention will be further introduced below in conjunction with the accompanying drawings. A standard sample bonding tooling of the present invention includes a mechanical test block, a platform 4, two guide posts 2, three positioning blocks 1 and a pressure block 3. The mechanical test block described is an ASTM C297 mechanical performance standard sample, which is arranged on the platform 4, and the two guide posts 2 are vertically arranged on both sides of the mechanical test block, and are detachably fixed on the platform 4. The three positioning blocks 1 are horizontally arranged on the guide pillars 2 of two cylindrical structures, and can slide up and down along the guide pillars 2. By adjusting the distance of the positioning blocks 1, the bonding of sandwich structures with different thicknesses can be realized. 3 is arranged on the top of the mechanical test block, and the platform 4 is a horizontal structure, which is used for placing standard sampl...

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Abstract

The invention discloses a standard sample bonding tool. The standard sample bonding tool comprises a mechanical test block, a platform, two guide columns, three positioning blocks and a pressing block, wherein the mechanical test block is arranged on the platform, and the two guide columns are vertically arranged on the two sides of the mechanical test block, the three positioning blocks are horizontally arranged on the two guide columns and can slide up and down along the guide columns, and the pressing block is arranged at the top of the mechanical test block. The standard sample bonding tool has the advantages that the bonding precision is high, the repeatability is good, the structure is simple, the operation is convenient, the adhesion force can be adjusted, and the bonding efficiencyis high.

Description

technical field [0001] The invention relates to the technical field of composite material manufacturing technology, in particular to a standard sample bonding tool. Background technique [0002] The composite honeycomb sandwich structure needs to be tested for mechanical properties, and the test pieces are prepared and tested according to ASTM C297. This standard requires high-precision bonding of honeycomb sandwich structures and aluminum alloys. [0003] My existing standard specimens are bonded by hand and then clamped with bow clamps. Since the adhesive needs a certain amount of time to solidify, the force of the workpiece during the clamping process is prone to misalignment of the bonding sample, resulting in poor bonding accuracy, which cannot meet the accuracy requirements of ASTM C297. The method of rough bonding first and then finishing the shape can ensure the final dimensional accuracy, but the secondary mechanical stress on the bonded parts will destroy the mec...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B25B11/00G01N1/28
CPCB25B11/00G01N1/286
Inventor 邓守成刘猛
Owner THE RES INST FOR SPECIAL STRUCTURES OF AERONAUTICAL COMPOSITE AVIC