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Force-thermal coupling test loading device for rotary cabin structure

A loading device and rotary technology, applied in measuring devices, using stable tension/pressure to test material strength, material thermal analysis, etc., can solve the problem of inability to adapt to pressure, temperature, shear coupling loading test requirements, single function, etc. problems, to achieve the effect of solving structural design and strength assessment problems, convenient operation and simple structure

Pending Publication Date: 2022-08-09
SHANGHAI SPACE PRECISION MACHINERY RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] At present, the function of the test device for simulating load in the existing technology is relatively single, and it cannot meet the test requirements of various pressure, temperature and shear force coupled loading.

Method used

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  • Force-thermal coupling test loading device for rotary cabin structure
  • Force-thermal coupling test loading device for rotary cabin structure
  • Force-thermal coupling test loading device for rotary cabin structure

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0060] This embodiment includes: an external pressure loading device, a thermal loading device, and a cross-sectional shear loading device; the external pressure loading device includes: a pressurizing bladder, a gas pressurizing system, and a liquid filling system, and the pressurizing bladder is charged by the liquid filling system. After injecting liquid and pressurizing through the gas pressurization system, it deforms toward the test piece 10 and compresses the test piece 10. The test piece 10 is connected to a heat loading device and heated by the heat loading device. The cross-sectional shear loading device includes a plurality of shear loading lever sets , the shear loading lever group is installed in the test piece 10 and applies shear force to the test piece 10, and the external pressure loading device, the thermal loading device and the cross-section shear loading device are connected to the test system terminal 15.

[0061] like figure 1 As shown, the external pres...

Embodiment 2

[0067] Example 2 is a preferred example of Example 1.

[0068] like Figure 1 to Figure 3 As shown, this embodiment includes: an external pressure loading device, a thermal loading device and a cross-sectional shear loading device. The external pressure loading device consists of air source 1, pressure reducing valve 2, booster valve 3, pressure relief valve 4, pressure relief port 5, rear pressure bearing tool 6, front end pressure bearing tool 7, front pressure booster bag 8, rear end The pressurized bladder 9 , the test base 11 , the pressure gauge 12 , the pressure sensor 13 , the pressure test line 14 , the test system terminal 15 , the filling pipeline 16 , the filling valve 17 , and the water source 18 are composed. The heat loading device is composed of a front-end electric heating blanket 19 , a rear-end electric heating blanket 20 , a temperature sensor and a test line 21 , and a test system terminal 15 . The cross-section shear loading device is composed of a fron...

Embodiment 3

[0075] like Figure 1 to Figure 3 As shown, the test piece 10 is installed on the test base 11, and the front-end pressurizing bag 8 and the rear-end pressurizing bag 9 are installed in the following manner: the front-end pressurizing bag 8 is installed inside the front-end pressure-bearing tool 7, and the front-end pressure-bearing tool 7 The inner wall surface is pasted with a flexible felt material to prevent the hard wall surface from damaging the front-end pressurizing bladder 8 during the pressurization process. Similarly, the rear pressure boosting bag 9 is installed inside the rear pressure bearing tool 6, and the inner wall of the rear pressure bearing tool 6 is pasted with a flexible felt material to prevent the hard wall from damaging the rear pressure bag 9 during the pressurization process. The rear-end pressure-bearing tooling 6 and the front-end pressure-bearing tooling 7 are both fixedly connected to the connecting ring by bolts, and the rear-end pressure-beari...

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Abstract

The invention provides a loading device for a force-heat coupling test of a rotary cabin structure. The loading device comprises an external pressure loading device, a heat loading device and a cross section shearing force loading device, the external pressure loading device comprises a pressurizing bag, a gas pressurizing system and a liquid filling system; the pressurizing bag is filled with liquid through the liquid filling system, deforms towards the test piece after being pressurized through the gas pressurizing system and compresses the test piece; the test piece is connected with the heat loading device and is heated through the heat loading device; the cross section shearing force loading device comprises a plurality of shearing force loading lever groups; the shearing force loading lever groups are mounted in the test piece and apply shearing force to the test piece; and the external pressure loading device, the heat loading device and the cross section shearing force loading device are connected with a test system terminal. According to the design scheme of the external pressure loading device, the heat loading device and the cross section shearing force loading device, the test device capable of meeting the test requirements of coupling loading of various pressures, temperatures and shearing forces is provided.

Description

technical field [0001] The invention relates to the field of test of the slewing type cabin body structure of an aerospace vehicle, in particular to a loading device for a mechanical and thermal coupling test of the slewing type cabin body structure. Background technique [0002] With the continuous improvement of the performance indicators of spacecraft, the bearing requirements of the rotary cabin structure are becoming more and more stringent. When the load conditions are simulated on the ground, the test requirements for pressure, temperature, and shear coupled loading are also gradually increasing. Therefore, it is necessary to determine the test loading method and the configuration of the test device according to the currently developed cabin structure and the characteristics of the load conditions during service. [0003] Patent document CN104697862A provides a mechanical-thermal coupling loading method for thermal strength test, which can realize high temperature, la...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N3/12G01N3/02G01N25/00G01N25/20
CPCG01N3/12G01N3/02G01N25/20G01N25/00G01N2203/0003G01N2203/0019
Inventor 刘博肖传清孙自强王小卫易果韩广威
Owner SHANGHAI SPACE PRECISION MACHINERY RES INST