CN204934205U - A kind of Combined hard-alloy composite ring - Google Patents

A kind of Combined hard-alloy composite ring Download PDF

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Publication number
CN204934205U
CN204934205U CN201520753887.1U CN201520753887U CN204934205U CN 204934205 U CN204934205 U CN 204934205U CN 201520753887 U CN201520753887 U CN 201520753887U CN 204934205 U CN204934205 U CN 204934205U
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China
Prior art keywords
intermediate layer
alloy
internal layer
alloy composite
composite ring
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Expired - Fee Related
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CN201520753887.1U
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Chinese (zh)
Inventor
齐鸿羽
孙泽超
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Individual
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Abstract

The utility model discloses a kind of Combined hard-alloy composite ring, described collars is ring-type, comprise set gradually from outside to inside skin, intermediate layer and internal layer, described intermediate layer is compounded in described outer inner surface by laser melting coating, and described internal layer is connected with described intermediate layer interference fit.This collars solves the process difficulties of carbide alloy compound, and when also solving carbide alloy and ferrous materials mechanical combination, magnitude of interference great Yi produces cracked problem.

Description

A kind of Combined hard-alloy composite ring
Technical field
The utility model belongs to mechanical manufacturing field, relates to a kind of Combined hard-alloy composite ring.
Background technology
Cemented carbide composite roll collar was based on the problem adopting casting technique to solve carbide ring and cast iron or cast steel how metallurgical binding in the past, brought the change of the complexity of manufacturing process and the serviceability of carbide ring.And carbide alloy and ferrous materials mechanical combination time magnitude of interference great Yi produce cracked problem.
Utility model content
The utility model makes improvement for above-mentioned Problems existing, and namely the technical problems to be solved in the utility model is to provide a kind of Combined hard-alloy composite ring, and structure is made up of three layers of unlike material.Skin is carbide alloy; Arrange intermediate layer and reach metallurgical binding with outer by laser melting coating, the bond strength of land is larger; Internal layer has higher intensity and good wearability, is convenient to combine with mandrel, and this collars structure can save more outer material.
In order to solve the problems of the technologies described above, the utility model proposes so a kind of Combined hard-alloy composite ring, described collars is ring-type, comprise set gradually from outside to inside skin, intermediate layer and internal layer, described intermediate layer and described skin carry out metallurgical binding by laser melting coating, and mechanical combination is carried out by interference fit in described internal layer and described intermediate layer.
Further, described skin is circular or irregular ring-type.
Further, described skin is that carbide alloy is outer, and described intermediate layer is ferrous alloy or Nickel-base Alloy Interlayer, and described internal layer is steel alloy internal layer.
Further, described intermediate layer and skin carry out metallurgical binding by laser melting coating.
Further, described internal layer and described intermediate layer complete interference fit by hot charging or cold charge.
Further, described collars external diameter is 150-450mm, and described outer field thickness is 10-30mm, and the thickness in described intermediate layer is 5-15mm.
Preferably, described collars external diameter is 340mm, and described outer field thickness is 15mm, and the thickness in described intermediate layer is 7.5mm.
Preferably, described collars external diameter is 380mm, and described outer field thickness is 25mm, and the thickness in described intermediate layer is 10mm.
The beneficial effects of the utility model:
The present invention adopts laser melting and coating process cladding ferrous alloy or nickel-base alloy on hard alloy substrate, carbide alloy is working surface, there is characteristic and the serviceability of the carbide alloy that traditional handicraft is produced, ferrous alloy or form metallurgical binding between nickel-base alloy and carbide alloy, has possessed the characteristic with other iron and steel material quality interference fit.This technical scheme solves the process difficulties of carbide alloy compound, and when also solving carbide alloy and ferrous materials mechanical combination, magnitude of interference great Yi produces cracked problem.And the skin of this collars can be designed as various irregularly shaped, can reduce the use of outer material.
Accompanying drawing explanation
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Fig. 1 is the structural representation of the utility model embodiment 1;
Fig. 2 is the sectional view along A-A direction in Fig. 1;
Fig. 3 is the structural representation of the utility model embodiment 2;
Fig. 4 is the sectional view along B-B direction in Fig. 3;
Fig. 5 is the structural representation of the utility model embodiment 3;
Fig. 6 is the sectional view along C-C direction in Fig. 5;
In figure: 1, outer, 2, intermediate layer, 3, internal layer.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Embodiment 1
As shown in Figure 1-2, this collars comprise set gradually from outside to inside skin 1, intermediate layer 2 and internal layer 3, described intermediate layer 2 by laser melting coating at described outer 1 inner surface, described internal layer 3 is connected with described intermediate layer 2 interference fit, described outer 1 is circular, described outer 1 is that carbide alloy is outer, described intermediate layer 2 is ferrous alloy intermediate layer, described internal layer 3 is steel alloy internal layer, described collars external diameter is 340mm, the described thickness of outer 1 is 15mm, and the thickness in described intermediate layer 2 is 7.5mm.
This collars is mainly used in bar wire rod rolling mill finished frame assembly roller.
Embodiment 2
As shown in Figure 3-4, this collars comprise set gradually from outside to inside skin 1, intermediate layer 2 and internal layer 3, described intermediate layer 2 by laser melting coating at described outer 1 inner surface, described internal layer 3 is connected with described intermediate layer 2 interference fit, described outer 1 is circular, described outer 1 is that carbide alloy is outer, described intermediate layer 2 is ferrous alloy intermediate layer, described internal layer 3 is steel alloy internal layer, described collars external diameter is 380mm, the described thickness of outer 1 is 15mm, and the thickness in described intermediate layer 2 is 7.5mm.
This collars saves the material of outer 1 relative to embodiment 1.
Embodiment 3
As seen in figs. 5-6, this collars comprise set gradually from outside to inside skin 1, intermediate layer 2 and internal layer 3, described intermediate layer 2 by laser melting coating at described outer 1 inner surface, described internal layer 3 is connected with described intermediate layer 2 interference fit, described outer 1 is irregular ring-type, described outer 1 is that carbide alloy is outer, described intermediate layer 2 is ferrous alloy intermediate layer, described internal layer 3 is steel alloy internal layer, described collars external diameter is 380mm, the described thickness of outer 1 is 25mm, and the thickness in described intermediate layer 2 is 10mm.
This collars is mainly used in bar materials on continuous rolling mill finish rolling section assembly roller.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.

Claims (7)

1. a Combined hard-alloy composite ring, it is characterized in that: described collars is ring-type, comprise set gradually from outside to inside skin, intermediate layer and internal layer, described intermediate layer and described skin carry out metallurgical binding by laser melting coating, and mechanical combination is carried out by interference fit in described internal layer and described intermediate layer.
2. a kind of Combined hard-alloy composite ring according to claim 1, is characterized in that: described skin is circular or irregular ring-type.
3. a kind of Combined hard-alloy composite ring according to claim 1, is characterized in that: described skin is that carbide alloy is outer, and described intermediate layer is ferrous alloy or Nickel-base Alloy Interlayer, and described internal layer is steel alloy internal layer.
4. a kind of Combined hard-alloy composite ring according to claim 1, is characterized in that: described internal layer and described intermediate layer complete interference fit by hot charging or cold charge.
5. a kind of Combined hard-alloy composite ring according to claim 1, it is characterized in that: described collars external diameter is 150-450mm, described outer field thickness is 10-30mm, and the thickness in described intermediate layer is 5-15mm.
6. a kind of Combined hard-alloy composite ring according to claim 5, it is characterized in that: described collars external diameter is 340mm, described outer field thickness is 15mm, and the thickness in described intermediate layer is 7.5mm.
7. a kind of Combined hard-alloy composite ring according to claim 5, it is characterized in that: described collars external diameter is 380mm, described outer field thickness is 25mm, and the thickness in described intermediate layer is 10mm.
CN201520753887.1U 2015-09-23 2015-09-23 A kind of Combined hard-alloy composite ring Expired - Fee Related CN204934205U (en)

Priority Applications (1)

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Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520753887.1U CN204934205U (en) 2015-09-23 2015-09-23 A kind of Combined hard-alloy composite ring

Publications (1)

Publication Number Publication Date
CN204934205U true CN204934205U (en) 2016-01-06

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106623435A (en) * 2017-03-03 2017-05-10 湖南三泰新材料股份有限公司 Hard alloy compound roller and manufacturing method thereof
CN106623861A (en) * 2016-10-17 2017-05-10 武汉春禾科技有限公司 Wear-resistant roll collar
WO2017201729A1 (en) * 2016-05-27 2017-11-30 山东省四方技术开发有限公司 Profiled composite-casted roll and preparation method therefor
CN118143170A (en) * 2024-05-10 2024-06-07 太原理工大学 Layered metal ring rolling equipment with circumferential corrugated composite interface and method

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017201729A1 (en) * 2016-05-27 2017-11-30 山东省四方技术开发有限公司 Profiled composite-casted roll and preparation method therefor
US10814382B2 (en) 2016-05-27 2020-10-27 Shandong Province Sifang Technical Development Group Co., Ltd. Special-shaped roll formed by a composite casting method and preparation process therefore
CN106623861A (en) * 2016-10-17 2017-05-10 武汉春禾科技有限公司 Wear-resistant roll collar
CN106623435A (en) * 2017-03-03 2017-05-10 湖南三泰新材料股份有限公司 Hard alloy compound roller and manufacturing method thereof
CN118143170A (en) * 2024-05-10 2024-06-07 太原理工大学 Layered metal ring rolling equipment with circumferential corrugated composite interface and method

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CF01 Termination of patent right due to non-payment of annual fee
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Granted publication date: 20160106

Termination date: 20210923