Spiral blade wear resisting layer alloy overlaying process

A helical blade and wear-resistant layer technology, which is applied in the field of alloy surfacing welding technology of the helical blade wear-resistant layer, can solve the problems of general wear resistance, short service life, complicated processing, etc., and achieve high comprehensive performance of wear resistance and corrosion resistance, Extend the service life and reduce the effect of production and processing

Active Publication Date: 2019-04-16
JIANGSU XINHONGDA GROUP
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Problems solved by technology

[0003] In the prior art, the material of the spiral blade is made of pure carbon steel or stainless steel and the method

Method used

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  • Spiral blade wear resisting layer alloy overlaying process
  • Spiral blade wear resisting layer alloy overlaying process

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Embodiment Construction

[0018] In order to have a further understanding of the purpose, structure, features, and functions of the present invention, the following detailed descriptions are provided in conjunction with the embodiments.

[0019] Please refer to figure 1 and figure 2 , figure 1 It is a flow chart of the alloy overlay welding process for the wear-resistant layer of the spiral blade according to an embodiment of the present invention, figure 2 It is a schematic diagram of the surfacing section structure of an embodiment of the present invention. The alloy surfacing process of the wear-resistant layer of the spiral blade of the present invention includes the following steps.

[0020] S1, remove the rust impurities on the end surface of the spiral blade 10 and the nearby welding area, such as oil, rust, water and other impurities. The main body of the spiral blade can be made of duplex steel 2205 material.

[0021] S2, use ERNiCrMo-3 nickel-chromium-molybdenum welding wire to weld th...

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Abstract

The invention provides a spiral blade wear resisting layer alloy overlaying process. Rust impurities on the end surfaces of spiral blades and in nearby welding areas are removed; transition layers areoverlaid along the end surfaces of the spiral blades by using ERNiCrMo-3 nickel chromium molybdenum welding wires through argon arc welding; during welding, narrow beads and short arcs are adopted without swinging; the welding current is 80-85 A; the inter-bead temperature is not higher than 130 DEG C; the overlaying layer number is two beads in each layer; the continuous welding is adopted; thewelding directions of two beads are opposite; the overlap quantity of the latter bead is one half of welding lines of the previous bead; welded parts are naturally cooled; the spiral blades are preheated to 200-250 DEG C; Stellite cobalt base alloy cladding layers are overlaid; during overlaying, the welding current is 75-80 A; the inter-bead temperature is not lower than 200 DEG C; the welding direction between the beads is reciprocating bead-by-bead welding; and welding joints between the welding beads are staggered. The service life of the blades can be greatly prolonged.

Description

technical field [0001] The invention relates to the technical field of spiral blade welding, in particular to an alloy surfacing process for a wear-resistant layer of a spiral blade. Background technique [0002] The farther the blade is from the drive shaft, the greater the force and the greater the edge wear of the blade. The process of depositing one or more layers of metals of the same material or different materials on the surface of mechanical parts by welding is called surfacing welding. [0003] In the prior art, the material of the spiral blade is made of pure carbon steel or stainless steel, and the method of adding Cr30 movable blade is used, which has general wear resistance, short service life and complicated processing. Contents of the invention [0004] In view of the above technical problems, the purpose of the present invention is to provide a helical blade wear-resistant layer alloy surfacing process with a relatively simple process and prolonging the se...

Claims

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Application Information

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IPC IPC(8): B23K9/04B23K9/32B23K35/30
CPCB23K9/04B23K9/044B23K9/32B23K35/30B23K35/3033
Inventor 陈爱民王秋生戴日全
Owner JIANGSU XINHONGDA GROUP
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