Basal body for composite structure hard alloy

A cemented carbide and composite structure technology, applied in the field of continuous interface composite structure cemented carbide matrix, can solve problems such as uneven stress, interface cracking, poor bonding, etc., to reduce raw material costs, improve flexural strength, improve Wet Corner Effect

Inactive Publication Date: 2007-08-01
自贡市天恒合金应用技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, the key to the quality of composite cemented carbide lies in the interface bonding mechanism between the substrate and the use layer. There are generally two aspects that affect the combination of the substrate and the use layer: First, the large difference in characteristics between the substrate and the use layer leads to poor bonding: the current conventional It is easy to obtain and low-cost steel, alloy steel, steel-bonded hard alloy and other materials with little or no W and Co as the matrix, but because these matrixes are alloys formed by adding other elements or compounds mainly to Fe, There is a large difference in the composition of the cemented carbide formed by adding a binder phase mainly to the hard phase, resulting in a large difference in the properties of the substrate and the cemented carbide layer. The most important characteristic difference is the thermal expansion coefficient between the substrate and the layer And the modulus of elasticity, the test shows that when the thermal expansion coefficient of the matrix is ​​greater than that of the use layer, a tensile stress is formed in the matrix, and the tensile stress produces cracks at the vertical interface on the matrix, and the residual tensile stress on the surface of the matrix is ​​unfavorable to the material properties; when the use layer When the coefficient of thermal expansion is greater than that of the matrix, the residual compressive stress will be formed in the matrix, which is beneficial to improve the physical and mechanical properties of the matrix, but if the difference in thermal expansion coefficient between the two is large, it will easily cause interface cracking, or cracks at the vertical interface in the use layer
In addition, because the elastic modulus of the matrix and the use layer are different, the layer with a larger elastic modulus bears more load, which is also easy to cause uneven force and cause the use layer to fall off.
The second is that there is a combination defect between the use layer a

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0019] In this embodiment, the matrix for the YG8 composite structure cemented carbide tensile die is prepared as

[0020] example:

[0021] Matrix composition: TiC+WC+Ni+Co+Mo; basic composition percentage: TiC-WC / Ni+Co+Mo=73% / 27%, TiC / WC: 64% / 36%, Ni+Co / Mo: 92.6 % / 7.4%, where the percentage of Co in the matrix=(0.25 / 1-0.08)*0.08=2%; to prepare a 100kg matrix: TiC=47kg, WC-Co pre-alloyed powder=28kg, Ni=23kg, Mo= 2kg, sent into the ball mill for wet grinding for 16 hours, unloaded, dried, blended, and sieved according to the conventional powder metallurgy production process of cemented carbide, and the base mixture and the use layer YG8 cemented carbide mixture are separately weighed and fed , Layered into the mold for one-time pressing and forming, the pressed compact is placed in a sintering furnace at the same temperature and one-time sintering to obtain a continuous interface composite structure cemented carbide matrix with TiC-WC as the hard phase.

specific Embodiment 2

[0022] This embodiment takes the preparation of the base body for the YG10X composite structure cemented carbide disc knife as an example:

[0023] Matrix composition: TiC+WC+Ni+Co+Mo 2 C; Matrix composition percentage: TiC-WC / Ni+Co+Mo 2 C=78% / 22%, TiC / WC=50% / 50%, Ni+Co / Mo 2 C=90% / 10%, where the percentage of Co in the matrix=(0.39 / 1-0.072)*0.072=3%; to prepare a 100kg matrix: TiC=39kg, WC-Co pre-alloyed powder=40kg, Ni=19kg , Mo 2 C=2kg, sent into a ball mill for wet grinding for 20 hours, and prepared a cemented carbide matrix with a continuous interface composite structure with TiC-WC as the hard phase according to the method in Example 1.

specific Embodiment 3

[0024] This embodiment takes the preparation of the matrix for the YG20 composite structure cemented carbide die as an example:

[0025]Matrix composition: WC+Ni+Co+Fe; matrix composition percentage: WC / Ni+Co+Fe=75% / 25%, Ni+Co / Fe=48% / 52%, where the percentage of Co in the matrix= 0.75 / 1-0.076×0.076=6%, prepare 100kg matrix: WC-Co pre-alloyed powder=81kg, Ni=6kg, Fe=13kg, sent to the ball mill for wet grinding for 24 hours, and prepared according to the method in Example 1. WC is a cemented carbide matrix with a continuous interface composite structure of the hard phase.

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PUM

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Abstract

The invention discloses a carbide alloy base body taking TiC- WC or WC as hard phase and used for continuous interface composite construction. It comprises hard phase and adhesive phase, said hard phase is TiC- WC or WC, and said adhesive phase is Ni compound. The base body is added with part of WC-Co- containing prelacy powder made from regenerative hard alloy to reuse W and Co, and base body is added with a large part of hard phase (TiC) and Ni compound to reduce W and Co consumption, the adhesive phase Ni compound combines with adhesive phase Co through intermolecular linkage to make the composite interface transite continuously without foreign matter generation, no slit and carbon elimination, gash and stratification. So the carbide alloy base body is characterized by wide application and good comprehensive performance, which is the same to that of normal single layer hard alloy.

Description

Technical field [0001] The invention belongs to the field of cemented carbide material preparation, and in particular provides a cemented carbide matrix with TiC-WC or WC as the hard phase for continuous interface composite structure. Background technique [0002] The commonly used cemented carbide is a single layer structure, and its composition consists of a hard phase (such as WC, WC-TiC, etc.) and a binder phase (such as Co, Co+Ni, etc.). This single layer structure is composed of Phase metal molecular bonds interact to form a continuous transitional whole, which has the characteristics of wide application and good comprehensive performance. In the actual use process of cemented carbide, the use part that is used to process the workpiece and is consumed only accounts for a small part of the entire cemented carbide volume. This part is called the used layer, which acts as a supporting lining to give the cemented carbide a certain shape. The overall non-used part of the size ac...

Claims

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Application Information

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IPC IPC(8): C22C29/06
Inventor 罗达成范丽何跃进
Owner 自贡市天恒合金应用技术有限公司
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