Rapid evaluation method for low-cycle fatigue performance of ultrathin automobile steel plate
A low-cycle fatigue and automotive steel plate technology, applied in the direction of strength characteristics, measuring devices, instruments, etc., can solve the problems of the influence of the accuracy of test results and the increase of material consumption, and achieve the effect of simple and fast testing process and saving experimental materials
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Embodiment 1
[0090] Carry out cantilever beam symmetrical bending fatigue loading on a DP590 steel sheet with an original thickness of 2 mm, determine the thickness range of the cantilever beam bending fatigue loading sample according to step S1, and design the thin foil size according to step S11: 1:11mm, l 0 : 3mm, w: 3.5mm, measure the average grain size of ferrite as d=9.5μm; calculate the number of grains passing through the first stage of fatigue crack propagation by step S12, Y≈1, σ y '≈400MPa, Δσ value is about 400~450MPa, calculated as i=3~4; from step S13, if the plate is subjected to tension-compression symmetric fatigue loading, calculate the number of grains that the crack propagates through in the second stage j≈2000 / 9.5≈210; combined with steps S14, S15 and S16, the value range of m is 2.5-4, and the calculated thickness range of the thin foil sample is t=60-160 μm. Then proceed to step S2, from step S21, select the thin foil thickness as 50 μm, 100 μm, 150 μm, 200 μm; est...
Embodiment 2
[0092] Carry out cantilever beam symmetrical bending fatigue loading on a DP steel sheet for automobiles with an original thickness of 2mm and a martensite volume fraction of 14%, determine the thickness range of the cantilever beam bending fatigue loading sample according to step S1, and design according to step S11 Thin foil size: l: 11mm, l 0 : 3mm, w: 3.5mm, measure the average grain size of ferrite as d=9.5μm; calculate the number of grains passing through the first stage of fatigue crack propagation by step S12, Y≈1, σ y '≈400MPa, Δσ value is about 400~450MPa, calculated as i=3~4; from step S13, if the plate is subjected to tension-compression symmetric fatigue loading, calculate the number of grains that the crack propagates through in the second stage j≈2000 / 9.5≈210; combined with steps S14, S15 and S16, the value range of m is 2.5-4, and the calculated thickness range of the thin foil sample is t=60-160 μm. Then proceed to step S2, from step S21, select thin foil th...
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