CN1319731C - Thermo shaping method of composite material component port surface - Google Patents
Thermo shaping method of composite material component port surface Download PDFInfo
- 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
- Authority
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 20
- 239000002131 composite material Substances 0.000 title claims abstract description 17
- 238000007493 shaping process Methods 0.000 title claims description 9
- 239000000463 material Substances 0.000 claims abstract description 25
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 8
- 239000002245 particle Substances 0.000 claims abstract description 8
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 238000010438 heat treatment Methods 0.000 claims description 5
- 238000005245 sintering Methods 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 238000003892 spreading Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 7
- 239000007769 metal material Substances 0.000 abstract description 2
- 230000002349 favourable effect Effects 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 5
- 238000003754 machining Methods 0.000 description 5
- 238000005452 bending Methods 0.000 description 2
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009499 grossing Methods 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
- 238000010792 warming Methods 0.000 description 1
Images
Landscapes
- Powder Metallurgy (AREA)
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
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 ℃.
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 |
Family
ID=35930427
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2005100602350A Expired - Fee Related CN1319731C (en) | 2005-08-01 | 2005-08-01 | Thermo shaping method of composite material component port surface |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1319731C (en) |
Families Citing this family (1)
| 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)
| 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 |
-
2005
- 2005-08-01 CN CNB2005100602350A patent/CN1319731C/en not_active Expired - Fee Related
Patent Citations (4)
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1718429A (en) | 2006-01-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101434026B (en) | High-melting metal arc spraying rapid die-manufacturing method | |
| CN104001811B (en) | A kind of TC4 titanium alloy dihedral thin-walled parts hot forming tool and forming method | |
| CN104707931A (en) | Manufacturing method for large high-temperature alloy disk-type die forging parts | |
| CN104589005A (en) | Molding process for straight bevel gear | |
| CN101367103B (en) | Magnesium alloy sheet material flow forming and molding process | |
| CN1319731C (en) | Thermo shaping method of composite material component port surface | |
| CN104384428B (en) | A kind of hollow wheel gear axis blank temperature finish forge forming method | |
| CN103056369A (en) | Process for producing part by powder metallurgy | |
| CN103834884A (en) | Method and mold for manufacturing die forging and eliminating residual stress | |
| CN104646976A (en) | Quick profile manufacturing method of composite material thin-shell mold for aircraft | |
| CN103706741A (en) | Hot forging and molding process for oxygen free copper material | |
| CN109465369B (en) | Ring rolling forming device for rolling and bending single integral ring of special-shaped joint | |
| CN103769454A (en) | High-temperature forming method of fine-grain TC21 titanium alloy plate | |
| CN103628108B (en) | Die casting surface treatment method and products thereof | |
| CN103060730A (en) | Preparation method of aluminum alloy with excellent comprehensive property | |
| CN103071690B (en) | Cold and hot extrusion molding method of rotary thick-walled shell part for vehicle | |
| CN104162670A (en) | Powder metallurgy technology | |
| CN115338410A (en) | High-entropy alloy and aluminum alloy composite material with high wear resistance and preparation method thereof | |
| CN100491122C (en) | Production of laminated composite plate without copper powder sintering layer | |
| CN1364669A (en) | Fine forging technology for automobile claw pole forging | |
| CN107571527A (en) | A kind of production technology of automobile rare earth oil-containing modified MC nylon casting bushing and its application | |
| JP2017202519A (en) | Hot stamping processing of age hardening type aluminum alloy plate | |
| CN111688301A (en) | Ultrathin high-relief aluminum-based composite gold foil product and processing technology thereof | |
| CN101623761A (en) | Method for manufacturing thermometal-powder compound sintering lateral plate of hydraulic pump | |
| CN104646926A (en) | Manufacturing technique for bimetallic lateral plate of hydraulic pump |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| 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 |