A device and method for measuring out-of-plane tensile mechanical properties of composite materials
A composite material and external stretching technology, which is applied in the direction of measuring devices, using stable tension/pressure to test the strength of materials, and analyzing materials, can solve problems such as low stiffness, thermal stress matching, and poor alignment, and achieve Less equipment investment, lower thermal expansion coefficient, and lower manufacturing cost
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Embodiment 1
[0041] see Figure 1-7 , a device for measuring out-of-plane tensile mechanical properties of composite materials, including an upper beam 1 and a lower beam 2, the lower beam 2 is arranged at the bottom of the device body, and a guide column is connected to the upper beam 1 and the lower beam 2 3. The bottom end of the guide column 3 is fixedly connected with the lower beam 2, and the upper beam 1 is connected to the guide column 3 by sliding fit; the lower end of the upper beam 1 is connected with the gantry upper pressure roller assembly 4, and the upper end of the lower beam 2 is connected with the gantry frame The lower pressure roller assembly 5, the upper pressure roller assembly 4 of the gantry frame and the lower pressure roller assembly 5 of the gantry frame are connected with an accessory spacer assembly 6.
[0042] The upper pressure roller assembly 4 of the gantry frame includes an upper gantry frame 401, which is fixedly installed on the lower end of the upper be...
Embodiment 2
[0066] see Figure 1-7 , based on Embodiment 1, the difference is that;
[0067] A biaxially oriented mechanical loading device (such as figure 1 shown), the device is mainly composed of lower beam 2, upper beam 1, guide column 3, gantry upper pressure roller assembly 4, gantry lower pressure roller assembly 5, and accessory spacer assembly 6. The upper pressure roller assembly 4 of the gantry frame and the lower pressure roller assembly 5 of the gantry frame can be freely adjusted within 50-160mm (test span) along the upper and lower grooves of the upper beam 1 and lower beam 2 as required.
[0068] figure 2 Diagram of the assembly procedure for the device body. First there is a longitudinal groove in the middle part of the upper beam 1, and this side of the transverse boss is facing down, and the rectangular hole in the middle is aligned with the rectangular boss at the upper end of the accessory spacer assembly 6, and is installed on the annex spacer assembly 6. Align ...
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