Blind hole method based residual stress distribution measurement method for composite material plate
A composite material and residual stress technology, applied in force/torque/work measuring instruments, measuring devices, analysis materials, etc., can solve problems such as error, single measurement stress direction, and large stress gap, so as to improve scientificity and accuracy , flexible and accurate measurement, the effect of precise measurement
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2020-10-30
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention belongs to the field of residual stress measurement of composite materials, and relates to a method for measuring residual stress distribution of composite material plates based on a blind hole method. Background technique
[0002] During the molding process of the composite material, due to the difference in the thermal expansion coefficient of the fiber and the matrix and the difference in the internal and external cooling rates, obvious residual stress will be generated during the cooling process. The generation of residual stress will cause the plate to warp and deform. There are many adverse effects in the use process. Therefore, in order to achieve the purpose of controlling the residual stress, the measurement of the residual stress of the composite material is particularly critical. At present, the commonly used residual stress measurement methods are mainly divided into two categories: non-destructive testing and destructive tes...
Examples
Embodiment Construction
[0043] The specific embodiments of the present invention will be described in detail below in conjunction with the technical solutions and accompanying drawings.
[0044] figure 1 It is a flowchart of the measurement and calculation of the residual stress of the composite material plate; Figure 4 is a schematic diagram of the residual stress measurement of a composite sheet based on the step drilling method.
[0045] (1) determine the area to be measured and the direction of the composite material plate 1, figure 2 and image 3 A common test scheme is shown, and 8 drilling positions are determined. The longitudinal stress is measured on one side of the plate and the transverse stress is measured on the other side. In addition, the drilling position and the direction of the strain gauge can be determined by oneself according to the requirements.
[0046](2) Grind the first drilling position I in the area to be tested with fine sandpaper in a direction 45° from the strain g...