Process for hardfacing a progressing cavity pump/motor rotor
a technology of progressing cavity and hardfacing, which is applied in the direction of rotary or oscillating piston engines, coatings, rotary piston engines, etc., can solve the problems that spray-on and fused coatings are still subject to flexing and impact, pitting and spalling
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example i
[0051] For an intended metallic coating thickness of 9 mils, the surface of a progressing cavity pump was roughened by grit blasting and subsequently hardfaced by flame spraying a WC containing metallic material onto the roughened surface. Typically, only that portion of the rotor surface which comes into contact with the fluids to be pumped is roughened and provided with a hardfacing layer. The grit used was steel grit with a hardness of 30 Rockwell and was blown at the rotor using an air pressure of 85 psi.
example ii
[0052] A metallic coating thickness of 15 mils was applied and all other conditions were identical to those described in Example I.
example iii
[0053] A metallic coating of 15 to 20 mils was applied to a surface which was roughened by grit blasting to a surface roughness of 10 to 12 mils. The grit had a hardness of 40 Rockwell and was blown at the rotor using an air pressure of 95 psi.
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Abstract
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