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Loading device and loading method for dynamic biaxial compression of solid propellant

A technology of solid propellants and loading devices, which is applied to measuring devices, using stable tension/pressure to test material strength, instruments, etc., can solve problems such as inability to test biaxial mechanical properties of materials, and achieve uniform and universal load distribution Good performance, reduce the effect of prestress and damage

Pending Publication Date: 2021-10-01
ROCKET FORCE UNIV OF ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the testing machine cannot directly cooperate with the test piece to realize the biaxial mechanical performance test of the material, so a new test fixture is needed to be used with the testing machine to carry out the research on the mechanical properties of the solid propellant material under biaxial high-speed compression

Method used

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  • Loading device and loading method for dynamic biaxial compression of solid propellant
  • Loading device and loading method for dynamic biaxial compression of solid propellant
  • Loading device and loading method for dynamic biaxial compression of solid propellant

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Embodiment Construction

[0052] The present invention is a loading device for dynamic biaxial compression of solid propellant, which comprises an upper clamp and a lower clamp which are matched and connected. A disc-shaped upper pressure plate 1 is fixedly connected to the upper loading table 2;

[0053] The lower clamp includes a lower clamp body and a lower loading platform 6 fixedly arranged at the lower end of the lower clamp body, and a bottom fixed sleeve 13 is fixedly connected to the lower loading platform 6;

[0054] The upper clamping body and the lower clamping body are fastened to each other, and the area between the upper clamping body and the lower clamping body is the clamping area 11. The clamping area 11 is in the shape of a cuboid, and the diagonal line of the clamping area 11 is located One of the planes is parallel to the vertical plane; a guiding device is also arranged between the upper clamping body and the lower clamping body;

[0055] The two ends of the upper clamping body a...

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Abstract

The invention relates to the technical field of material mechanical property tests, in particular to a loading device and a loading method for dynamic biaxial compression of a solid propellant. The loading device comprises an upper clamp and a lower clamp which are connected in a matched mode, the upper clamp comprises an upper clamp body and an upper loading table, and a disc-shaped upper pressing disc is fixedly connected to the upper loading table; the lower clamp comprises a lower clamp body and a lower loading table, and the lower loading table is fixedly connected with a bottom fixing sleeve seat; and the upper clamp body and the lower clamp body are buckled with each other, and the area between the upper clamp body and the lower clamp body is a clamping area. According to the clamp designed by the invention, biaxial compression loading test such as dynamic loading with the loading ratio of 1: 1, and the strain rate covering 1-100S <-1 > can be realized on a high-strain-rate hydraulic servo testing machine. The clamp is in micro contact with the surface of the test piece through a suspension structure composed of a double-hole wire locking device and a thin rope, direct operation on a test piece is avoided, and prestress and damage caused by the dead weight of a fixed test piece and the clamp are reduced.

Description

technical field [0001] The invention relates to the technical field of material mechanical performance testing, in particular to a loading device and a loading method for dynamic biaxial compression of solid propellants. Background technique [0002] At present, the test methods involved in the test standards for the mechanical properties of solid propellant materials mainly include quasi-static uniaxial tension and compression test methods with relatively mature test systems, and there is still a lack of methods for testing the mechanical properties of solid propellants under dynamic biaxial compression loading. Effective test method. However, the mechanical properties of solid propellants are not only significantly affected by strain rate change factors, but also by stress state factors, and there are obvious differences between uniaxial and biaxial mechanical properties. Therefore, in order to accurately grasp the mechanical properties of propellants under dynamic biaxia...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N3/04G01N3/12
CPCG01N3/04G01N3/12G01N2203/0019G01N2203/0048
Inventor 强洪夫耿挺京王学仁王哲君王广岳春国王祺洲
Owner ROCKET FORCE UNIV OF ENG
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