Process for assembling and welding ultralong hollow shafting auger flight

A spiral blade and welding process technology, which is applied in the field of assembly and welding process of super-long hollow shaft spiral blades, can solve the problems of high industry threshold, asymmetric structure, high production cost, etc., to ensure wear resistance and hardness, and eliminate welding stress , making simple effects

Active Publication Date: 2009-04-22
CITIC HEAVY INDUSTRIES CO LTD
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  • Summary
  • Abstract
  • Description
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AI Technical Summary

Problems solved by technology

[0004] The selected base metal has high strength, in other words poor weldability, preheating before welding is the most prominent contradiction, asymmetric structure, poor rigidity, not suitable for welding tooling, high production cost, large deformation after stress relief
[0005] Due to the high threshold of the industry, outstanding technological added va...

Method used

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Examples

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Embodiment Construction

[0026] Taking the assembly and welding process of the blade-type screw shaft of the shield machine as an example, the main design parameters are as follows:

[0027] I. The screw shaft adopts a diameter of 194mm, a wall thickness of 35mm, a length of 10200mm, and a material of 45 # Steel pipe fabrication.

[0028] II. The continuous spiral blade is made of Q345B plate with an outer diameter of 696mm and a plate thickness of 30mm.

[0029] III. A 5mm wear-resistant layer is surfacing in the thickness direction of the outer circular plate of the continuous spiral blade, and the hardness requirement is HRC554~60.

[0030] IV. The cylindricity of the continuous helical blade and the helical shaft after welding is not greater than 5mm.

[0031] Assembly welding process of the present invention is stated as follows:

[0032] 1: The ultra-long hollow shaft preheating welding spiral blade assembly welding process includes the following contents:

[0033] 1) Cut 1 / 2 of the spiral b...

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PUM

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Abstract

The invention provides an assembly welding process for an ultra-long hollow shaft helical blade, which mainly comprises two assembly welding processes, namely the pre-heating welding of the helical blade on the ultra-long hollow shaft and the overlaying welding of the antiwear layer on the helical blade and a process of the overall annealing of overlaying welding. In the assembly welding processes, the small-pore tubing negative pressure siphoning type air supply combustion-supporting gas heating is utilized to solve the problem of preheating the high-carbon equivalent material; by evaluating the welding processes of a plurality of overlaying welding materials, the welding method, the welding material and the welding condition are finally determined; and the result meets the hardness(HRC54 to 06) of the antiwear layer required in the design, which is the necessary hardness obtained after annealing, and solves the new welding stress problem generated due to the overlaying welding after annealing. Moreover, the process has the advantages of easily obtained material, simple preparation, time conservation and labor conservation, and low cost.

Description

technical field [0001] The invention belongs to the field of welding technology, and in particular relates to an assembly and welding process of an ultra-long hollow shaft helical blade. Background technique [0002] The blade-type screw shaft configured on the shield machine is a hollow super-long-body welded structural part. The weldability of this type of structural part is generally determined from the carbon equivalent of the base metal, the restraint degree of the structure, and the hydrogen content of the deposited metal. define and judge. The difficulty of manufacturing structural parts often depends on the symmetry and rigidity of the structure, the degree of automation of applicable welding methods, labor intensity and working environment and other factors. [0003] The outstanding issues for the production of this type of structural parts are: [0004] The selected base metal has high strength, in other words, poor weldability, preheating before welding is the m...

Claims

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Application Information

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IPC IPC(8): B23K31/02B23K9/16B23K9/235B23K9/095B23K9/04C21D9/00
Inventor 白金生王丽宏
Owner CITIC HEAVY INDUSTRIES CO LTD
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