Manufacturing method of submarine oil well valve base
A technology for subsea oil wells and manufacturing methods, which is applied to wellbore/well valve devices, earthwork drilling, wellbore/well parts, etc., and can solve the problem of small friction coefficient of chrome plating layer, low hardness of chrome plating layer, and easy fall off of chrome plating layer and other problems, to achieve good dispersion and coverage, to avoid quenching stress concentration cracks, to improve the effect of density and continuity
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Embodiment 1
[0025] This embodiment provides a method for manufacturing a subsea oil well valve seat provided by the present invention. The chromium-molybdenum low-alloy steel is selected as the blank, and the component content of the chromium-molybdenum low-alloy steel includes the following components in mass percentages: carbon: 0.3%, Silicon: 0.18%, Manganese: 0.50%, Chromium: 0.90%, Molybdenum: 0.20%, Phosphorus: 0%, Sulfur: 0%, Hydrogen: 0ppm, Nickel: 0%, Vanadium: 0%, Copper: 0%, 0 % residual element, all the other are Fe, specifically comprise the following steps:
[0026] Step (1): Heat the billet to 880°C, upset the billet along the axial direction, air cool to 360°C and keep it warm for 420 minutes;
[0027] Step (2): reheat the billet in step (1) to 870°C, repeatedly upsetting along the two mutually perpendicular diameter directions of the cross section of the billet, and air-cool to 290°C for 180 minutes;
[0028] Step (3): Heat the billet in step (3) to 585°C, pull out the f...
Embodiment 2
[0037] This embodiment provides a method for manufacturing a subsea oil well valve seat. Chromium-molybdenum low-alloy steel is selected as the blank, and the component content of the chromium-molybdenum low-alloy steel includes the following components in mass percentages: carbon: 0.32%, silicon: 0.36% %, manganese: 0.70%, chromium: 1.10%, molybdenum: 0.30%, phosphorus: 0.02%, sulfur: 0.025%, hydrogen: 1.8ppm, nickel: 0.40%, vanadium: 0.03%, copper: 0.30%, 0.9% residual element, and the rest are Fe, which specifically includes the following steps:
[0038] Step (1): Heating the billet to 920°C, upsetting the billet in the axial direction, air cooling to 360°C and keeping it warm for 420 minutes;
[0039] Step (2): reheat the billet in step (1) to 890°C, repeatedly upsetting along the two mutually perpendicular diameter directions of the cross section of the billet, and air-cool to 310°C for 180 minutes;
[0040] Step (3): Heat the billet in step (3) to 615°C, pull out the fo...
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