Multipoint loading stress application cap for static test

A static test and force cap technology, used in instruments, measuring devices, scientific instruments, etc., can solve the problems of unclear bending moment loading, and the bending moment cannot reach the loading target load, and achieve the effect of reducing installation errors.

Active Publication Date: 2020-03-31
XIAN AEROSPACE PROPULSION TESTING TECH RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in the bending moment test, the current bending moment loading uses a lever structure to make a force difference between the two force application points to generate the bending moment. However, when the force difference of the two forces passes through the i

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  • Multipoint loading stress application cap for static test
  • Multipoint loading stress application cap for static test
  • Multipoint loading stress application cap for static test

Examples

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Embodiment Construction

[0022] Embodiments of the present invention are described in detail below, and the embodiments are exemplary and intended to explain the present invention, but should not be construed as limiting the present invention.

[0023] The existing booster caps are all two-point loading methods, which are mainly designed for axial compression and axial tension load tests. When the traditional booster cap is used for bending moment load loading, there is a large gap between the test data and the theoretical calculation, resulting in Bending moment loads are ambiguous.

[0024] In order to solve the above problems, this embodiment proposes a multi-point loading booster cap for static tests, the center of the multi-point loading booster cap adopts a beam-type load-bearing design, and the hollow cylindrical load-bearing column is used as the main load-bearing force structure, on the outer circumference of the load-bearing column, eight ray load-bearing beams distributed at equal angles ar...

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Abstract

The invention provides a multipoint loading stress application cap for a static test, which is characterized in that a hollow cylindrical force bearing column is adopted as a main force bearing structure in the center, and a plurality of ray force bearing beams distributed at equal included angles are fixed on the outer circumference of the force bearing column to serve as a main lever force transmission structure; a mounting hole is formed in the front surface of the outer end of each bearing beam as a loading point, and the centers of all the mounting holes are located on the same circumference with the center of the bearing column as the circle center. According to the multi-point loading stress application cap, on the basis that the test function of a traditional stress application capcan be completed, loads such as axial pressure and bending moment can be applied more evenly, and most installation errors are reduced; the mounting holes are formed in the front face and the side face of the outer end of the force bearing beam, loads such as shearing force and axial pressure can be conveniently achieved, and smooth testing is guaranteed.

Description

technical field [0001] The invention relates to the field of static tests, in particular to a multi-point loading force cap for static tests. Background technique [0002] Static tests play an important role in mechanical test research, especially axial compression, axial tension and bending moment tests, which can account for more than 80% of the total number of tests. [0003] The traditional static test booster cap is designed for two-point loading, see the schematic diagram figure 1 , the shrinkage structure is used to make the two-point loading force converge on the shrinkage structure, and then the loading force is evenly distributed on the circumferential structure by using the enlargement structure. This booster cap is suitable for pure axial compression or axial tension test. However, in the bending moment test, the current bending moment loading uses a lever structure to make a force difference between the two force application points to generate the bending momen...

Claims

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Application Information

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IPC IPC(8): G01N3/02
CPCG01N3/02G01N2203/0017G01N2203/0019G01N2203/0023G01N2203/0025
Inventor 田振宇姜文英李强顾筠翟晓谷红闫蓉董新乐
Owner XIAN AEROSPACE PROPULSION TESTING TECH RES INST
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