CN1319731C - Thermo shaping method of composite material component port surface - Google Patents

Thermo shaping method of composite material component port surface Download PDF

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Publication number
CN1319731C
CN1319731C CNB2005100602350A CN200510060235A CN1319731C CN 1319731 C CN1319731 C CN 1319731C CN B2005100602350 A CNB2005100602350 A CN B2005100602350A CN 200510060235 A CN200510060235 A CN 200510060235A CN 1319731 C CN1319731 C CN 1319731C
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CN
China
Prior art keywords
composite material
material component
shaping method
port surface
component port
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CNB2005100602350A
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Chinese (zh)
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CN1718429A (en
Inventor
揭朝奎
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Zhejiang New Jialian Electronics Co., Ltd.
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揭朝奎
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Publication date
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Priority to CNB2005100602350A priority Critical patent/CN1319731C/en
Publication of CN1718429A publication Critical patent/CN1718429A/en
Application granted granted Critical
Publication of CN1319731C publication Critical patent/CN1319731C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The present invention discloses a hot forming method on the surface of a composite material component. The present invention aims to provide a hot forming method on the surface of a composite material component, which has the advantages of simple manufacturing process, high processing precision, favorable roughness and low manufacturing cost. The method of the present invention comprises: firstly, the shape of base material is processed according to component requirements; secondly, copper powder is sintered on the friction surface of a component; finally, non-metallic material friction reducing particles are laid on the friction surface and are sintered in a mold which is heated or in a heated hot mold under the pressurizing condition. The method has great application value for the manufacture of composite material components with large and non-uniform material thickness.

Description

The thermo shaping method of composite material component port surface
Technical field
The present invention relates to a kind of part forming method, relate in particular to a kind of laminated composite material part forming method with steel-copper-nonmetallic materials.
Background technology
Metal material, macromolecular material and ceramic material respectively possess some good points on serviceability and are not enough, and the range of application of oneself is respectively arranged.Along with science and technology development, more and more higher to the requirement of material, use single material to satisfy these requirements and become more and more difficult.Therefore, composite has appearred, at present, the general laminated composite material of Shi Yonging, as the oil-free lubrication sliding bearing of steel-copper-nonmetallic materials, these sliding bearings generally are axle sleeve class shapes.Its technology is: cutting steel plate-surface of steel plate shop copper powder sintering-smoothing-surface is spread nonmetallic materials anti-attrition particles sintering-smoothing and is rolled onto specific thickness and becomes blank-put in storage according to sliding bearing size blanking-circle circle-shaping-check.This flat sheet of making composite earlier reshapes method for processing and only is fit to the uniform part of thickness, because the inconsistency of material physical property, as the thermal expansion factor difference, when high temperature, separates between the easily wrinkling or material faying face; In the BENDING PROCESS after material becomes flat board, because the curvature difference of material ectonexine also can cause the separation between the material faying face, in addition, because in the shaping process, slidingsurface scratches easily, and the precision of processing and coarse also being difficult to guarantee, influence the quality of part.And for material thickness part big, in uneven thickness, be the plane as lower surface, upper surface is that rubbing surface is that the manufacturing of arcuate part just seems very difficult.
Summary of the invention
The object of the present invention is to provide that a kind of technology is simple, machining accuracy is high and the thermo shaping method of the composite material component port surface of coarse good, low cost of manufacture.
In order to achieve the above object, a kind of technical scheme of thermo shaping method of composite material component port surface is: comprise at first that according to part it is the shape of base material that requirement processes with the steel; Secondly at the friction surface sintered copper powder; Spread nonmetallic materials anti-attrition particles sintering at friction surface again, it is characterized in that at the sintering of spreading nonmetallic materials anti-attrition particle it being to finish under the condition of in mould, pressurizeing in heating or heating back the mould in heat.Described pressurization is meant and keeps the just demoulding after 1 minute after part pressurizes at least in mould.
Method according to the above-mentioned back sintering that is shaped earlier comes the formed composite material piece surface has the following advantages:
1, technology is simple.It has overcome traditional handicraft with the bending forming forming effect that is beyond one's reach.
2, machining accuracy and coarse good.Requirement on machining accuracy to the blank part is not high, guarantees surperficial machining accuracy and roughness by mould, and is good to producing interchangeablity in batches especially.
3, low cost of manufacture.Can remove complicated machining and multiple tracks trimming from, the production efficiency height.
Description of drawings
Fig. 1 is the front view of slideway;
Fig. 2 is the vertical view of Fig. 1;
Fig. 3 is the front view of slideway base material;
Fig. 4 is the front view behind the slideway sintered copper powder;
Fig. 5 is the schematic diagram that slideway is processed in mould.
Wherein: 1, slideway; 2, upper surface; 3, base material; 4, copper powder; 5, nonmetallic materials anti-attrition particle; 6, patrix; 7, counterdie.
The specific embodiment
With the example that is processed as of part slideway, the invention will be further described in conjunction with the accompanying drawings below.
As shown in Figure 1 and Figure 2, it is to be used in slideway 1 parts pattern that the gate two sides are used to lead, and upper surface 2 is anti-attrition surfaces of arch, is coated with composite.Its processing method:
Require to process shape such as Fig. 3 that steel is a base material 3 according to slideway 1 part; Secondly at friction surface sintered, spherical copper powder 4 as Fig. 4; Nonmetallic materials anti-attrition particle 5 is spread on the surface of copper powder in the cooling back, part is put into baking oven heat, and is warming up to 250 ℃ of heat penetrations.
In addition, make corresponding patrix 6 and counterdie 7 according to the shape of upper surface 2, patrix 6 and counterdie 7 are heated between 230 ℃-280 ℃, slideway 1 blank after putting into heating in the middle of patrix 6 and the counterdie 7, the processing of slideway 1 part is promptly finished in matched moulds pressurization molding after 3 minutes after the demoulding.
The temperature that above-mentioned part heats in baking oven can be selected between 200 ℃-300 ℃, as 220 ℃, 240 ℃, 250 ℃, 260 ℃, 270 ℃ etc.
The mold temperature of above-mentioned heat can be between 200 ℃-300 ℃, as 220 ℃, 240 ℃, 250 ℃, 260 ℃, 270 ℃ etc.
Can in the mould of heat, directly pressurize for little part and to finish processing, needn't preheating.

Claims (4)

1, a kind of thermo shaping method of composite material component port surface comprises at first that according to part it is the shape of base material that requirement processes with the steel; Secondly at the friction surface sintered copper powder; Spread nonmetallic materials anti-attrition particles sintering at friction surface again, it is characterized in that at the sintering of spreading nonmetallic materials anti-attrition particle it being to finish under the condition of in mould, pressurizeing in heating or heating back the mould in heat.
2, the thermo shaping method of composite material component port surface according to claim 1 is characterized in that described heating-up temperature is 200 ℃-300 ℃.
3, the thermo shaping method of composite material component port surface according to claim 1 is characterized in that described pressurization is meant and keep after 1 minute the just demoulding after part pressurizes at least in mould.
4, the thermo shaping method of composite material component port surface according to claim 1 is characterized in that the mould of described heat is meant that mold temperature is between 200 ℃-300 ℃.
CNB2005100602350A 2005-08-01 2005-08-01 Thermo shaping method of composite material component port surface Expired - Fee Related CN1319731C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB2005100602350A CN1319731C (en) 2005-08-01 2005-08-01 Thermo shaping method of composite material component port surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB2005100602350A CN1319731C (en) 2005-08-01 2005-08-01 Thermo shaping method of composite material component port surface

Publications (2)

Publication Number Publication Date
CN1718429A CN1718429A (en) 2006-01-11
CN1319731C true CN1319731C (en) 2007-06-06

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CNB2005100602350A Expired - Fee Related CN1319731C (en) 2005-08-01 2005-08-01 Thermo shaping method of composite material component port surface

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Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109849371A (en) * 2019-03-27 2019-06-07 成都联科航空技术有限公司 The variable cross-section hollow structure composite material parts forming method of high-precision inner surface

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0442052A1 (en) * 1990-02-14 1991-08-21 AlliedSignal Bremsbelag GmbH Disc brakes friction lining, especially for road vehicles and railway vehicles
CN1079034A (en) * 1993-02-11 1993-12-01 李安国 High revolution composite bearing material without lubrication
CN2573755Y (en) * 2002-07-26 2003-09-17 嘉善长盛滑动轴承有限公司 Self-lubricating leadless bearing
CN1488865A (en) * 2002-10-10 2004-04-14 嘉善长盛滑动轴承有限公司 Self-bubricating lead-free bearing and manufacture method thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0442052A1 (en) * 1990-02-14 1991-08-21 AlliedSignal Bremsbelag GmbH Disc brakes friction lining, especially for road vehicles and railway vehicles
CN1079034A (en) * 1993-02-11 1993-12-01 李安国 High revolution composite bearing material without lubrication
CN2573755Y (en) * 2002-07-26 2003-09-17 嘉善长盛滑动轴承有限公司 Self-lubricating leadless bearing
CN1488865A (en) * 2002-10-10 2004-04-14 嘉善长盛滑动轴承有限公司 Self-bubricating lead-free bearing and manufacture method thereof

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CN1718429A (en) 2006-01-11

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C06 Publication
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C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
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ASS Succession or assignment of patent right

Owner name: XINJIALIAN ELECTRONIC CO., LTD., ZHEJIANG

Free format text: FORMER OWNER: JIE ZHAOKUI

Effective date: 20081024

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20081024

Address after: No. 36 Dongsheng Road, Jiashan Economic Development Zone, Zhejiang

Patentee after: Zhejiang New Jialian Electronics Co., Ltd.

Address before: Zhejiang province Jiashan dry kiln town dry kiln village 7 team

Patentee before: Jie Chaokui

EE01 Entry into force of recordation of patent licensing contract

Assignee: Zhejiang New Jialian Electronics Co., Ltd.

Assignor: Jie Chaokui

Contract fulfillment period: 2007.7.1 to 2013.7.1 contract change

Contract record no.: 2008330001147

Denomination of invention: Thermo shaping method of composite material component port surface

Granted publication date: 20070606

License type: Exclusive license

Record date: 20081017

LIC Patent licence contract for exploitation submitted for record

Free format text: EXCLUSIVE LICENSE; TIME LIMIT OF IMPLEMENTING CONTACT: 2007.7.1 TO 2013.7.1; CHANGE OF CONTRACT

Name of requester: XINJIALIAN ELECTRONIC CO., LTD., ZHEJIANG

Effective date: 20081017

C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20070606