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Test piece for realizing biaxial stress state through uniaxial loading of spherical working section

A biaxial stress, working section technology, applied in the direction of applying stable tension/pressure to test the strength of materials, measuring devices, instruments, etc. Initial shape, reduced test difficulty and cost, small residual deformation effect

Active Publication Date: 2020-10-30
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] For the designed multi-axial fatigue test piece, the test is usually carried out on a multi-axial fatigue testing machine, which brings another difficulty in the research process, that is, the way of applying the load is greatly restricted
Using a multi-axial fatigue testing machine to load, the test cost is also high, and the load is usually a tensile torsion load, which is more limited

Method used

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  • Test piece for realizing biaxial stress state through uniaxial loading of spherical working section
  • Test piece for realizing biaxial stress state through uniaxial loading of spherical working section
  • Test piece for realizing biaxial stress state through uniaxial loading of spherical working section

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Embodiment Construction

[0023] The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0024] The uniaxial loading of the spherical working section of the present invention realizes the biaxial stress state. The test piece has a plate-like structure as a whole, a working section 1 with a rhombus structure in the middle, and clamping sections 2 with a rectangular structure on the left and right sides, and the working section 1 with a diamond structure. Both sides of the two diagonals are partially symmetrical. Such as figure 1 , figure 2 shown.

[0025] The ends of the clamping section 2 of the rectangular structure on both sides are respectively connected to the positions of the two opposite angles A and B in the working section 1 of the rhombus structure, and the middle bisector of the clamping section 2 in the left and right directions of the rectangular structure is connected with the clamping The diagonals of angle A and angle B are col...

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Abstract

The invention discloses a test piece for realizing a biaxial stress state through uniaxial loading of a spherical working section. The test piece is integrally of a plate-shaped structure, the middlepart is a working section, the left and right sides are clamping sections, the working section is of a rhombic structure, and the two sides of two diagonal lines are partially symmetrical. Spherical recesses and special-shaped holes are designed in the working section; the spherical recesses are designed on the front and back surfaces of the working section and are positioned in the center of theworking section; the number of the special-shaped holes is four, and the four special-shaped holes are formed in the four parts, equally divided by the two angular bisectors, of the working section respectively. Loading of the test piece is achieved through a uniaxial fatigue testing machine, under the designed spherical recesses and special-shaped holes, a multi-axial stress state of stretching in the horizontal direction and compressing in the vertical direction is finally generated in the center of the whole test piece, and a typical tension / compression multi-axial stress state is formed. According to the invention, simulation of the tension and pressure biaxial state of the disc center of a turbine disc can be realized, part-level assessment tests can be partially replaced, the structural design period is shortened, and the test cost is saved.

Description

technical field [0001] The invention belongs to the technical field of mechanical structure strength assessment and simulation part design, and is a test piece aimed at the uniaxial loading of the spherical working section to realize the biaxial stress state. The force state can reflect the stress characteristics of the structure. Background technique [0002] At present, in typical structures of turbomachinery blades, discs, shafts, etc., including aeroengines and internal combustion engines, stress concentration locations such as hole edges and fillets are key parts that are prone to fatigue cracks and subsequent damage. In order to ensure the safety of these positions, it is usually necessary to carry out strength assessment through tests, especially fatigue strength assessment. For components, it is undoubtedly a long cycle and high cost to carry out component-level tests for overall structural assessment. At the same time, there are many uncontrollable factors in the t...

Claims

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Application Information

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IPC IPC(8): G01N3/08G01N3/04G01N3/02
CPCG01N3/02G01N3/04G01N3/08
Inventor 魏大盛马梦弟王延荣蒋向华
Owner BEIHANG UNIV
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