CN1710227A - Method for manufacturing lock shaft parts for container - Google Patents
Method for manufacturing lock shaft parts for container Download PDFInfo
- Publication number
- CN1710227A CN1710227A CN 200510027477 CN200510027477A CN1710227A CN 1710227 A CN1710227 A CN 1710227A CN 200510027477 CN200510027477 CN 200510027477 CN 200510027477 A CN200510027477 A CN 200510027477A CN 1710227 A CN1710227 A CN 1710227A
- Authority
- CN
- China
- Prior art keywords
- hour
- incubated
- insulations
- base part
- stove
- 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.)
- Granted
Links
Landscapes
- Mold Materials And Core Materials (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
The invention discloses a center shaft component for locks of cargo container production technique with investment moulding. The invention provides with a set of rational technique from material selecting, shell making, melting, and heat processing, resolving the many technique problems in center shaft component for locks of cargo container production with investment moulding, simplifying the production procedure and lowering the cost, enhancing productivity so to be more adaptive to mass production.
Description
Technical field
The present invention relates to a kind of lockset manufacture method, particularly a kind of manufacture method of container special lockset axis base part.
Background technology
Along with the development of international trade, the demand of container is very huge, and the respective episode vanning is also increasing with the demand of lockset.And as container with stressed maximum in the lockset, axle base part that requirement of strength is the highest, still follow at present the technology of using repeatedly forging and molding, reprocessing, because operation is many, workload is very big, the difficulty of producing in enormous quantities is bigger, causes product cost can not to be in any more.
Model casting claims " lost-wax casting " again.This method is that easy fusible pattern material is injected die mould (mould), makes fusible pattern, and it is assembled into module, and the liquid coating that is made into refractory material and cementing agent in the module surface applied spreads fire-resistant sand grains again on coating then, makes it to harden into shell subsequently.So repeated multiple times just forms the multilayer shell.With the shell heating, the fusible pattern fusing is flowed out, housing toward wherein pouring into liquid alloy, solidifies after operations such as cleaning promptly obtain foundry goods after roasting.Its main technique flow process following (referring to accompanying drawing):
A. wax-pattern is made
Comprise processing steps such as technological design, die mould design, die mould manufacturing, the preparation of mould material, system fusible pattern and running gate system (promptly make product wax sample and design and produce rational running gate system), fusible pattern combination according to products characteristics.
B. shell mould is made
Comprise coating preparation, hardener preparation, coat and stucco, shell sclerosis and dry (stucco and dry two steps repeat to have sufficient intensity with making for several times), the molten processing steps such as fusible pattern (dewaxing), shell roasting that lose;
C. alloyage material
Comprise furnace charge preparation and alloy melting;
D. alloy material melting, cast;
E. cleaning
Comprise shelling, remove processing steps such as dead head, cleaning, check, soldering;
F. heat treating castings;
G. put in storage
Comprise check and correction and warehouse-in.
This foundry goods once-forming, any surface finish, size are more accurate, can reach few cutting or not have the purpose of cutting, are particularly suitable in the production of middle-size and small-size, thin-walled class and the multiple alloy-steel casting of complex-shaped class.And in the manufacturing of container relatively complicated for shape, that requirement of strength is high,, do not use this method at present as yet owing to be subjected to the traditional handicraft restriction with lockset axle base part.
Summary of the invention
The objective of the invention is to provide a cover utilization investment casting method to produce the technology of container with lockset axis base part, full form casting process is replaced Forging Technology produce high-strength container with the many technological problemses in the lockset axis base part to solve, with simplify container with the production and processing operation of lockset axis base part, enhance productivity, reduce production costs, under the prerequisite of guaranteeing specified intensity and quality, produce in enormous quantities.
The present invention adopts full form casting process to replace Forging Technology, and associated process steps that wherein relates to and the technological parameter of choosing are as follows:
A. prepare a kind of high-strength alloy material, its composition be (weight percentage, unit: %):
C：0.35-0.45??????????????Si：0.30-0.60
Mn：0.70-1.50?????????????Cr：0.80-1.50
Mo：0.15-0.40；
Other are iron and impurity;
B. alloy material melting, cast;
Fusion temperature: 1580-1620 ℃, pouring temperature is 1530-1560 ℃;
C. heat treating castings, its technology is:
860 ℃-900 ℃ the insulation 1-3 hour after oil quenching,
500 ℃-600 ℃ insulations were cooled off with stove after 1-3 hour.
Adopt such cover full form casting process to produce container lockset axis base part, mechanical performance of products can reach:
Tensile strength sigma
b: 950-1000MPa
Elongation per unit length δ %: 〉=9%
Low temperature impact strength (27 ℃) A
Kv: 〉=27J
Like this, under the prerequisite that guarantees the product strength performance, adopt technology of the present invention obviously to simplify the manufacturing procedure of container with lockset axis base part, the product once-cast is shaped, exempt many cuttings, forged operation, improved the utilization rate of production efficiency and metal material, both simplified equipment, operation, also reduce cost of production, be convenient to form large-scale production ability in enormous quantities.Still be the production process angle from production equipment no matter, full form casting process all forges processing technology and has more advantage, more adapts to large-scale production; Thereby have significant technical advance, economy and a practicality.
And as a preferred embodiment of the present invention, the composition of described alloy material can be:
C：0.38-0.45????Si：0.30-0.60???Mn：0.80-1.00
Cr：0.80-1.20???Mo：0.20-0.30???S、P≤0.025；
Adopt this scheme, mechanical performance of products can reach:
Tensile strength sigma
b: 965-1000MPa
Elongation per unit length δ %: 〉=10.0%
Low temperature impact strength (27 ℃) A
Kv: 〉=30J
In the above-mentioned process program, described shell mould is made can use the sodium silicate binder process for making shell.Like this, under the prerequisite of the pi of strength of guaranteeing product, can drop to cost of production minimum.
As the further preferred version of the present invention, the Technology for Heating Processing in above-mentioned each scheme can adopt: 870 ℃-900 ℃ the insulation 1-3 hour after air cooling (normalizing); 860 ℃-900 ℃ the insulation 1-3 hour after oil quenching (modified); 500 ℃-600 ℃ insulations were cooled off (tempering) with stove after 1-3 hour.
Adopt this scheme, mechanical performance of products can further must reach:
Tensile strength sigma
b: about 1000MPa
About elongation per unit length δ %:11%
Low temperature impact strength (27 ℃) A
Kv: 〉=35J
Description of drawings
Accompanying drawing is the process chart of model casting.
The specific embodiment
Do further detailed description below in conjunction with accompanying drawing and exemplary embodiments:
Embodiment 1
A. wax-pattern is made;
Press the structure of mo(u)lded piece, the design running and feeding system.This wax-pattern possesses the design of rational running gate system, can guarantee the consecutive solidification of foundry goods; Can adopt the cast of column rising head multilayer.Also available sphere riser individual layer cast.Cast gate can be used single cast gate, also available double teeming mouth.
B. shell mould is made;
Make shell mould with water glass as cementing agent, comprise sclerosis, dewaxing and the roasting of shell mould.
C. prepare a kind of high-strength alloy material, its composition is:
C：0.38???????Si：0.33?????Mn：0.94
Cr：1.09??????Mo：0.27?????S、P≤0.025；
D. alloy material melting, cast:
The fusing of employing intermediate frequency furnace is adopted the non-oxidizing process process for making, and is selected rare earth ferrosilicon (FeSiRe45) deoxidation for use,
Fusion temperature: 1590 ℃; Casting pouring, pouring temperature is: 1530 ℃;
E. heat treating castings, its technology is:
Normalizing: 890 ℃ the insulation 1 hour after air cooling;
Modified: 860 ℃ the insulation 1.5 hours after oil quenching;
Tempering: 550 ℃ of insulations were cooled off with stove after 2 hours.
Its mechanical performance is as follows:
Tensile strength sigma
b: 1031MPa
Elongation per unit length δ %:10.5%
Low temperature impact strength (27 ℃) A
Kv: 43J
Embodiment 2 to 10 does following adjustment to material composition, fusion temperature, pouring temperature and process of thermal treatment parameter respectively,
| Embodiment | ??C | ??Si | ??Mn | ??Cr | ??Mo | ??S、P | Fusion temperature | Pouring temperature | Technology for Heating Processing | ||
| Normalizing | Modified | Tempering | |||||||||
| ??2 | ??0.35 | ??0.39 | ??0.73 | ??0.80 | ??0.15 | ? ?? ? ? ??≤0.025 | ??1580 | ??1550 | 900 ℃ are incubated 1 hour. oil quenching | 600 ℃ are incubated 1 hour. and stove is cold | |
| ??3 | ??0.38 | ??0.42 | ??0.80 | ??0.92 | ??0.20 | ??1580 | ??1540 | 880 ℃ are incubated 2 hours. oil quenching | 550 ℃ are incubated 2 hours. and stove is cold | ||
| ??4 | ??0.40 | ??0.30 | ??0.88 | ??1.06 | ??0.25 | ??1590 | ??1550 | 900 ℃ are incubated 3 hours. oil quenching | 600 ℃ are incubated 3 hours. and stove is cold | ||
| ??5 | ??0.38 | ??0.50 | ??0.84 | ??0.80 | ??0.30 | ??1600 | ??1560 | 900 ℃ are incubated 1 hour. air cooling | 900 ℃ are incubated 2 hours. oil quenching | 550 ℃ are incubated 3 hours. and stove is cold | |
| ??6 | ??0.42 | ??0.40 | ??0.80 | ??1.05 | ??0.23 | ??1610 | ??1530 | 880 ℃ are incubated 2 hours. air cooling | 865 ℃ are incubated 3 hours. oil quenching | 550 ℃ are incubated 3 hours. and stove is cold | |
| ??7 | ??0.41 | ??0.30 | ??0.85 | ??1.20 | ??0.25 | ??1580 | ??1530 | 880 ℃ are incubated 3 hours. oil quenching | 500 ℃ are incubated 2 hours. and stove is cold | ||
| ??8 | ??0.45 | ??0.32 | ??1.00 | ??0.93 | ??0.26 | ??1620 | ??1560 | 860 ℃ are incubated 3 hours. air cooling | 880 ℃ are incubated 3 hours. oil quenching | 600 ℃ are incubated 3 hours. and stove is cold | |
| ??9 | ??0.40 | ??0.60 | ??0.70 | ??0.80 | ??0.20 | ??1610 | ??1550 | 870 ℃ are incubated 2 hours. air cooling | 860 ℃ are incubated 1 hour. oil quenching | 550 ℃ are incubated 1 hour. and stove is cold | |
| ??1 ??0 | ??0.42 | ??0.35 | ??1.50 | ??1.50 | ??0.40 | ??1580 | ??1560 | 900 ℃ are incubated 3 hours. air cooling | 880 ℃ are incubated 2 hours. oil quenching | 600 ℃ are incubated 2 hours. and stove is cold | |
The mechanical performance such as the following table of the foundry goods of embodiment 1 to 10:
| Embodiment | Tensile strength sigma b | Elongation per unit length δ % | Low temperature impact strength (27 ℃) A kv |
| ??1 | ??1031 | ??10.5 | ??43 |
| ??2 | ??953 | ??9.8 | ??31 |
| ??3 | ??966 | ??10.6 | ??31.8 |
| ??4 | ??970 | ??11.5 | ??36 |
| ??5 | ??1078 | ??13.5 | ??36 |
| ??6 | ??1000 | ??11 | ??35 |
| ??7 | ??1017 | ??11.1 | ??30 |
| ??8 | ??998 | ??12.5 | ??32.8 |
| ??9 | ??1007 | ??11.5 | ??33.5 |
| ??10 | ??1000 | ??9.3 | ??38 |
Claims (4)
1. a method of making container with lockset axis base part is characterized in that this method adopts full form casting process, and wherein the technological parameter chosen of associated process steps is as follows:
A. prepare a kind of high-strength alloy material, its composition (weight percentage, unit: %) be:
C：0.35-0.45????????????Si：0.30-0.60
Mn：0.70-1.50???????????Cr：0.80-1.50
Mo：0.15-0.40
Other are iron and impurity;
B. alloy material melting, cast:
Fusion temperature: 1580-1620 ℃, pouring temperature is 1530-1560 ℃;
C. heat treating castings, its technology is:
860 ℃-900 ℃ insulations oil quenching after 1-3 hour, 500 ℃-600 ℃ insulations were cooled off with stove after 1-3 hour.
2. manufacturing container according to claim 1 is characterized in that with the method for lockset axis base part, described high-strength alloy material, and its composition is:
C：0.38-0.45??????Si：0.30-0.60?????Mn：0.60-1.00
Cr：0.80-1.20?????Mo：0.20-0.30?????S、P≤0.025；
3. manufacturing container according to claim 1 and 2 is characterized in that described heat treating castings technology is with the method for lockset axis base part: 870 ℃-900 ℃ insulations air cooling after 2-3 hour; 860 ℃-880 ℃ the insulation 2-3 hour after oil quenching; 550 ℃-600 ℃ insulations were cooled off with stove after 2-3 hour.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200510027477 CN1710227B (en) | 2005-07-04 | 2005-07-04 | Method for manufacturing lock shaft parts for container |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200510027477 CN1710227B (en) | 2005-07-04 | 2005-07-04 | Method for manufacturing lock shaft parts for container |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1710227A true CN1710227A (en) | 2005-12-21 |
| CN1710227B CN1710227B (en) | 2010-12-15 |
Family
ID=35706514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200510027477 Expired - Fee Related CN1710227B (en) | 2005-07-04 | 2005-07-04 | Method for manufacturing lock shaft parts for container |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1710227B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101818234A (en) * | 2010-04-20 | 2010-09-01 | 广州市型腔模具制造有限公司 | Quenching process of H13 steel for compression molds |
| CN102260778A (en) * | 2010-05-31 | 2011-11-30 | 宁波吉威熔模铸造有限公司 | Container lockset product as well as thermal treatment process and equipment thereof |
| CN102260777A (en) * | 2010-05-31 | 2011-11-30 | 宁波吉威熔模铸造有限公司 | Heat processing process for lockset material and equipment thereof |
| CN103252449A (en) * | 2013-05-08 | 2013-08-21 | 青岛钰鑫车辆工程有限公司 | Production method of composite material stirring wing |
| CN109158543A (en) * | 2018-09-26 | 2019-01-08 | 天长市兴宇铸造有限公司 | A kind of casting method of vehicle centre of pull steel-casting |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1019030B (en) * | 1989-12-30 | 1992-11-11 | 清华大学 | Bainite/martensite multi-phase steel with air-cooled high hardenability |
| CN1037699C (en) * | 1995-05-09 | 1998-03-11 | 宝山钢铁(集团)公司 | Stainless corrosion-resistant conductive rolle rsleeve and making method thereof |
| CN1114714C (en) * | 2000-09-16 | 2003-07-16 | 江苏江河集团电力工程公司 | Centrifugal casting technology for manufacturing cold drawn seamless pipe of ultralow-carbon dual-phase stainless steel |
| US6814131B2 (en) * | 2000-11-10 | 2004-11-09 | Buntrock Industries, Inc. | Investment casting mold and method of manufacture |
-
2005
- 2005-07-04 CN CN 200510027477 patent/CN1710227B/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101818234A (en) * | 2010-04-20 | 2010-09-01 | 广州市型腔模具制造有限公司 | Quenching process of H13 steel for compression molds |
| CN101818234B (en) * | 2010-04-20 | 2011-07-13 | 广州市型腔模具制造有限公司 | Quenching process of H13 steel for compression molds |
| CN102260778A (en) * | 2010-05-31 | 2011-11-30 | 宁波吉威熔模铸造有限公司 | Container lockset product as well as thermal treatment process and equipment thereof |
| CN102260777A (en) * | 2010-05-31 | 2011-11-30 | 宁波吉威熔模铸造有限公司 | Heat processing process for lockset material and equipment thereof |
| CN102260777B (en) * | 2010-05-31 | 2013-06-19 | 宁波吉威熔模铸造有限公司 | Heat processing process for lockset material and equipment thereof |
| CN103252449A (en) * | 2013-05-08 | 2013-08-21 | 青岛钰鑫车辆工程有限公司 | Production method of composite material stirring wing |
| CN103252449B (en) * | 2013-05-08 | 2015-12-02 | 青岛钰鑫车辆工程有限公司 | Composite stirs wing production method |
| CN109158543A (en) * | 2018-09-26 | 2019-01-08 | 天长市兴宇铸造有限公司 | A kind of casting method of vehicle centre of pull steel-casting |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1710227B (en) | 2010-12-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106011621B (en) | A kind of preparation technology of harmonic reducer flexible wheel | |
| CN106735225B (en) | A method of being injected into shape forging aluminium alloy brake disc brake drum | |
| CN101538667B (en) | High-strength and wear-resistant cocrystallized Al-Si alloy forging stock material and preparation method thereof | |
| CN102861873A (en) | Casting method of gear | |
| CN103451510A (en) | Manufacturing method of vermicular cast iron piston ring | |
| CN101120894B (en) | Technology method relating to component in manufacturing artificial limb knee-joint | |
| CN1710227A (en) | Method for manufacturing lock shaft parts for container | |
| CN102899589A (en) | High-strength non-tempered bainite steel and preparation method thereof | |
| CN100371483C (en) | Aluminum alloy for plastic working and manufacture thereof | |
| CN104439940B (en) | Clamp nut casting technology based on casting and rolling combined forming | |
| CN109468485A (en) | A kind of preparation method of nanometer of endogenous TiC particle reinforced aluminum alloy plate | |
| CN111690840A (en) | Amorphous phase silicate particle and SiC particle reinforced aluminum matrix composite material and preparation | |
| CN112481517A (en) | Preparation method of ceramic particle reinforced aluminum alloy | |
| CN1278802C (en) | Process for extrusion casting piston blank of internal combustion engine with local feinforcing of metal base composite material | |
| CN107052226A (en) | A kind of end cap casting technique | |
| CN109084008A (en) | Magnesium alloy gear box casing and preparation method thereof | |
| CN104060183B (en) | A kind of oscillating arm bracket and production method thereof | |
| CN1180117C (en) | Novel casting and hot work tool steel | |
| CN100337775C (en) | Method for producing large-sized blank of wrought magnesium alloys | |
| CN1597223A (en) | Manufacturing method of electrode cap used for welding automobile coated steel plate | |
| CN107790633B (en) | Investment precision casting process for aluminum alloy doors and windows | |
| CN104060153B (en) | A kind of HT200 foundry goods and production method thereof | |
| CN103008581B (en) | Hot-top and multi-mold casting device for aluminum alloy cast ingot | |
| JP3829164B2 (en) | Semi-melt molding material manufacturing method | |
| DE102009054315A1 (en) | Method for producing a motor vehicle component |
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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101215 Termination date: 20180704 |