Sample table for scanning electron microscope in-situ observation of stress corrosion cracking of metal material
A stress corrosion, metal material technology used in the field of scanning electron microscope sample stages to solve problems such as limitations
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Embodiment 1
[0030] The invention records the SEM in-situ observation process of stress corrosion cracking of U75V steel in 1.0% HCl aqueous solution. The process is given by 4 SEM images: the morphology image of the prefabricated crack maintained in a constant displacement state; the morphology image maintained in a 1.0% HCl aqueous solution for 20 hours, it can be seen that the surface is corroded and the crack expands; it is maintained for 40 hours The appearance of crack growth, crack tip passivation; the appearance of 60h hours, corrosion aggravated, crack growth, microcrack connection before the crack tip. Crack propagation from 20 hours to 40 hours, measured crack tip opening displacement from 5.0 μm to 8.13 μm, an increase of 3.13 μm. That is: 6 = 3.13 μm.
Embodiment 2
[0032] Use the present invention to record H62 brass at 0.5MNH 4 SEM in situ observation process of stress corrosion cracking in OH aqueous solution. The process is given by two SEM images, which are: the image of the prefabricated crack maintaining a constant displacement state, and the crack tip forms a slip line; at 0.5MNH 4 The morphology of the OH aqueous solution under load for 5 minutes shows that a small amount of corrosion products appear on the surfaces on both sides of the crack. It was measured that the crack length extended from 116.0 μm in the initial state to 130.0 μm, an increase of 14.0 μm. Calculate the crack growth rate: da / dt=14.0 / 5=2.8 μm / min.
Embodiment 3
[0034]The present invention records the SEM in-situ observation process of stress corrosion cracking of 7075-T6 aging aluminum alloy in 0.5M NaCl aqueous solution. The process is given by two SEM images, which are the stress corrosion fracture image of the crack in 0.5M NaCl aqueous solution for 1.0h, with a magnification of 30 times; the surface of the sample is corroded, and step cracks appear at the crack tip; the crack growth image after 2.0h , 200X magnification, step crack growth, showing the role of precipitation versus crack growth. The front length of the step crack extended from 179.0 μm to 320.0 μm, an increase of 141.0 μm. Calculate the crack growth rate: da / dt=141.0 / 60=2.33 μm / min.
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