Loading device and debugging method for epoxy resin model fracture test

A rupture test, epoxy resin technology, applied in the field of experimental mechanics, can solve the problems of large mechanical vibration value, large test error, large deformation, etc., and achieve the effect of eliminating oscillation, avoiding low fundamental frequency, and eliminating the increase of vibration value.

Pending Publication Date: 2021-10-29
AECC HUNAN AVIATION POWERPLANT RES INST
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0004] Aiming at the shortcomings and deficiencies of the prior art, the present invention aims to provide a loading device and a debugging method for epoxy resin model rupture tests, whi...

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  • Loading device and debugging method for epoxy resin model fracture test
  • Loading device and debugging method for epoxy resin model fracture test

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Embodiment Construction

[0029] In order to make the purpose, technical solution and advantages of the present invention clearer, the technical solution of the present invention will be further described in detail through the following embodiments and in conjunction with the accompanying drawings. In the specification, the same or similar reference numerals designate the same or similar components. The following description of the embodiments of the present invention with reference to the accompanying drawings is intended to explain the general inventive concept of the present invention, but should not be construed as a limitation of the present invention.

[0030] In addition, in the following detailed description, for purposes of explanation, numerous specific details are set forth in order to provide a comprehensive understanding of the embodiments of the present disclosure. It may be evident, however, that one or more embodiments may be practiced without these specific details. In other instances...

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Abstract

The invention discloses a loading device and a debugging method for an epoxy resin model fracture test, and belongs to the technical field of experimental mechanics. The loading device is composed of an electric control system, a detection sensing system, system software and a mechanical tool, wherein the electric control system comprises a PLC, an upper computer, a frequency conversion speed regulator and a motor, the mechanical tool comprises a base used for supporting and fixing the motor, a plum blossom joint elastic coupling installed on an output shaft of the motor, a transmission shaft, a stand column type bearing seat and an incubator inner bearing seat. The real working condition of the prototype is simulated when the epoxy resin model fracture test is carried out, the elastic-plastic state of the prototype is simulated by utilizing the transition state of the model, and the test precision is improved. The circumferential pre-tightening force is added to the epoxy resin model, so that the deformation of the model before fracture is reduced, and the test is more in line with the real working conditions of the prototype.

Description

technical field [0001] The invention belongs to the technical field of experimental mechanics, in particular to a loading device and a debugging method for an epoxy resin model rupture test. Background technique [0002] The epoxy resin model is widely used in the field of experimental mechanics, and it has good optical and mechanical properties. Its test device is generally relatively simple, suitable for applying tension, compression, bending, torsion, centrifugal and other loads. The current model hybrid loading device and the photosensitive resin model centrifugal loading device are both designed for elastic stress analysis. The model used in the test works in a highly elastic state, and the material is completely elastic. The directly obtained model stress is converted into the prototype stress through similarity theory. , this technology cannot effectively obtain the fracture speed and fracture position at present. At present, the test technology for obtaining the ru...

Claims

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Application Information

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IPC IPC(8): G01N3/02
CPCG01N3/02G01N2203/005G01N2203/0067G01N2203/0222G01N2203/0226
Inventor 郭天才文华陈亚农陈昌根夏清黄臻荣张韵秋
Owner AECC HUNAN AVIATION POWERPLANT RES INST
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