CN106363115A - Novel ultrahigh taper ring rolling method - Google Patents
Novel ultrahigh taper ring rolling method Download PDFInfo
- Publication number
- CN106363115A CN106363115A CN201610788390.2A CN201610788390A CN106363115A CN 106363115 A CN106363115 A CN 106363115A CN 201610788390 A CN201610788390 A CN 201610788390A CN 106363115 A CN106363115 A CN 106363115A
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- CN
- China
- Prior art keywords
- aluminum alloy
- alloy blank
- heating furnace
- blank
- ring
- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21H—MAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
- B21H1/00—Making articles shaped as bodies of revolution
- B21H1/06—Making articles shaped as bodies of revolution rings of restricted axial length
Abstract
The invention relates to a novel ultrahigh taper ring rolling method. According to the method, a ring with internal and external straight walls is directly obtained after cogging, the aluminum alloy blank is changed to be in the shape with the exterior being taper and an inner hole being a straight round hole through drawing of a mandrel, and accordingly the height of the blank can be increased to the preset dimension. By means of the method, the material utilization rate can be increased, the production cost is reduced, the mechanical property of materials can be significantly improved, and the corrosion resistance of aluminum alloy is greatly improved.
Description
Technical field
The present invention relates to forging technology field, more particularly, to a kind of novel super-high Conical ring rolls ring method.
Background technology
With developing rapidly of China's aerospace industry, modern national defense industry and transportation, important stressed member and knot
The lightweight of component, promotes the cry more and more higher for steel with aluminum, the usage amount of aluminum alloy forge piece and demand just to incrementally increase.
When domestic at present each factory produces superelevation special-shaped forge parts, after all adopting production straight wall superelevation cylindrical member, by way of Vehicle Processing, plus
Work becomes special-shaped ring, so on the one hand reduces stock utilization, improves production cost；On the other hand also result in forging stream
Line is destroyed in follow-up machining process, reduces the mechanical property of material, also reduces the resistance to corrosion of aluminium alloy.
Currently available technology carries out changing forging punching for after ingot casting heating a period of time, after punching terminates, is air cooled to room temperature,
After machining hinders endoporus clearly, reheat and carry out saddle support reaming, after melting down insulation a period of time, then carry out fullering with the core bar, again
After melting down insulation a period of time, then carry out saddle support reaming, rolling ring to predetermined straight wall size, after being air cooled to room temperature, by forging from straight
Wall cylindrical member is machined to taper cylindrical member.But prior art one side reduces stock utilization, improves production cost；
On the other hand also result in forging flow lines to be destroyed in follow-up machining process, reduce the mechanical property of material, also drop
The low resistance to corrosion of aluminium alloy.
Content of the invention
The applicant is directed to above-mentioned existing issue, has carried out Improvement, provides a kind of novel super-high Conical ring to roll ring
Method, it not only increases stock utilization, also a saving production cost.
The technical solution adopted in the present invention is as follows:
A kind of novel super-high Conical ring rolls ring method, comprises the following steps:
The first step: blanking: one section of cutting is as aluminum alloy blank on aluminium alloy cast ingot；
Second step: heat for the first time: described aluminum alloy blank is put and is heated to 460 DEG C～500 DEG C to heating furnace, Ran Houbao
Take out from heating furnace after warm 20～30h；
3rd step: change forging: aluminum alloy blank is carried out changing with forging, then by described aluminum alloy blank punching, be cooled to room temperature
Afterwards endoporus is hindered clearly；
4th step: heat for second: described aluminum alloy blank is placed again in heating furnace being heated to 460～480 DEG C, so
Take out from heating furnace after insulation 10～15h afterwards；
5th step: fullering with the core bar: pulled out described aluminum alloy blank to more than 1200mm using mandrel, make described aluminium alloy
The outside of blank forms taper, and the endoporus of described aluminum alloy blank is straight section circular hole；
6th step: melt down for the first time: the 5th step gained aluminum alloy blank is placed again into after insulation 8～12h in heating furnace
Take out from heating furnace, the temperature of this heating furnace is 440～460 DEG C；
7th step: saddle support reaming: saddle support reaming is carried out to described aluminum alloy blank by straight plug and upper flat anvil, makes described
The endoporus of aluminum alloy blank forms the outside identical pyramidal structure with aluminum alloy blank.
8th step: melt down for the second time: the inside and outside aluminum alloy blank being taper is put into after insulation 5～8h in heating furnace
Take out from heating furnace；
9th step: roll over ring: aluminum alloy blank is carried out roll over ring using core roller and home roll, make described aluminum alloy blank roll over ring extremely
Preliminary dimension.
Its further technical scheme is::
Described mandrel roller one end diameter is less than other end diameter, the stage casing of described core roller along described core roller periphery to extension
Stretch formation tapered flanges；Also form tapering in one end of described home roll.
Beneficial effects of the present invention are as follows:
The inventive method is directly inside and outside straight wall ring after cogging, blank enabled aluminum alloy to by fullering with the core bar be changed into outside be
Taper, endoporus are straight circular hole, so that the height of blank can pull out to preliminary dimension, the inventive method can not only improve material
Utilization rate, save production cost, the mechanical property of material can also be increased substantially simultaneously, substantially increase the anti-corruption of aluminium alloy
Erosion ability.
Brief description
Fig. 1 is structural representation after punching for the aluminum alloy blank in the present invention.
Fig. 2 is structural representation after fullering with the core bar for the aluminum alloy blank in the present invention.
Fig. 3 is structural representation after saddle support reaming for the aluminum alloy blank in the present invention.
Fig. 4 is structural representation after rolling over ring for the aluminum alloy blank in the present invention.
Fig. 5 is aluminum alloy blank and core roller, the structural representation of home roll in the present invention.
Wherein: 1, aluminum alloy blank；2nd, endoporus；3rd, core roller；301st, tapered flanges；4th, home roll；401st, tapering.
Specific embodiment
The specific embodiment of the present invention is described below.
Embodiment 1:
A kind of novel super-high Conical ring rolls ring method and comprises the following steps:
The first step: blanking: one section of cutting is as aluminum alloy blank 1 on aluminium alloy cast ingot；
Second step: heat for the first time: aluminum alloy blank 1 is put and is heated to 480 DEG C to heating furnace, then after insulation 20h from
Heating furnace takes out；
3rd step: change forging: as shown in figure 1, carrying out changing forging to aluminum alloy blank 1, then aluminum alloy blank 1 punching is cooled down
To room temperature, and clear up endoporus 2；
4th step: heat for second: aluminum alloy blank 1 is placed again in heating furnace being heated to 450 DEG C, is then incubated
Take out from heating furnace after 10h；
5th step: fullering with the core bar: pulled out aluminum alloy blank to 1250mm using mandrel, enable aluminum alloy to base as shown in Figure 2
The outside of material 1 forms taper, and the endoporus 2 of aluminum alloy blank 1 is straight section circular hole；
6th step: melt down for the first time: the 5th step gained aluminum alloy blank 1 is placed again into after insulation 8～12h in heating furnace
Take out from heating furnace, the temperature of this heating furnace is 450 DEG C.
7th step: saddle support reaming: the internal-and external diameter of aluminum alloy blank 1 is formed and aluminium alloy base using straight plug and upper flat anvil
The outside identical pyramidal structure of material.
8th step: melt down for the second time: by the inside and outside aluminum alloy blank 1 being taper put in heating furnace after insulation 5h from
Take out in heating furnace；
9th step: roll over ring: as shown in figure 4, carrying out rolling over ring using special taper die, above-mentioned particular manufacturing craft includes home roll 4
And core roller 3, one end formation tapering 401 of home roll 4, it is used for enabling aluminum alloy to the outline of blank 1 and forms taper, in core roller 3
Extend centrally out formation tapered flanges 301, the Internal periphery that this tapered flanges 301 is used for being formed aluminum alloy blank 1 forms taper,
Described aluminum alloy blank 1 is made to roll over ring to following size: aluminum alloy blank 1 endoporus 2 one end microcephaly internal diameter a is 830mm, external diameter a1 is
1030mm, aluminum alloy blank 1 endoporus 2 other end major part internal diameter b are 1000mm, and external diameter b1 is 1200mm, and height h is 1300mm.
Above description is explanation of the invention, is not the restriction to invention, limited range of the present invention is referring to right
Require, in the case of the basic structure without prejudice to the present invention, the present invention can make any type of modification.
Claims (2)
1. a kind of novel super-high Conical ring rolls ring method it is characterised in that comprising the following steps:
The first step: blanking: one section of cutting is as aluminum alloy blank on aluminium alloy cast ingot；
Second step: heat for the first time: described aluminum alloy blank is put and is heated to 460 DEG C～500 DEG C to heating furnace, be then incubated 20
Take out from heating furnace after～30h；
3rd step: change forging: aluminum alloy blank is carried out changing with forging, then by described aluminum alloy blank punching, be cooled to right after room temperature
Endoporus is hindered clearly；
4th step: heat for second: described aluminum alloy blank is placed again in heating furnace being heated to 460～480 DEG C, Ran Houbao
Take out from heating furnace after warm 10～15h；
5th step: fullering with the core bar: pulled out described aluminum alloy blank to more than 1200mm using mandrel, make described aluminum alloy blank
Outside form taper, and the endoporus of described aluminum alloy blank is straight section circular hole；
6th step: melt down for the first time: by the 5th step gained aluminum alloy blank be placed again in heating furnace after insulation 8～12h from plus
Take out in hot stove, the temperature of this heating furnace is 440～460 DEG C；
7th step: saddle support reaming: saddle support reaming is carried out to described aluminum alloy blank by straight plug and upper flat anvil, makes described aluminum close
The endoporus of golden blank forms the outside identical pyramidal structure with aluminum alloy blank；
8th step: melt down for the second time: by the inside and outside aluminum alloy blank being taper put in heating furnace after insulation 5～8h from plus
Take out in hot stove；
9th step: roll over ring: aluminum alloy blank is carried out roll over ring using core roller and home roll, make described aluminum alloy blank roll over ring extremely predetermined
Size.
2. as claimed in claim 1 a kind of novel super-high Conical ring roll ring method it is characterised in that: described mandrel roller one end
Diameter is less than other end diameter, and the stage casing of described core roller stretches out formation tapered flanges along the periphery of described core roller；Described
One end of home roll also forms tapering.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610788390.2A CN106363115A (en) | 2016-08-31 | 2016-08-31 | Novel ultrahigh taper ring rolling method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610788390.2A CN106363115A (en) | 2016-08-31 | 2016-08-31 | Novel ultrahigh taper ring rolling method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106363115A true CN106363115A (en) | 2017-02-01 |
Family
ID=57899149
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610788390.2A Pending CN106363115A (en) | 2016-08-31 | 2016-08-31 | Novel ultrahigh taper ring rolling method |
Country Status (1)
| Country | Link |
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| CN (1) | CN106363115A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112475806A (en) * | 2020-11-20 | 2021-03-12 | 西安航天发动机有限公司 | QCr0.8 alloy large-size conical-cylindrical ring forming process |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS52131967A (en) * | 1976-03-19 | 1977-11-05 | Thyssen Ag | Method of fabricating annular work materials such as blind flanges having remarkably formed cross section and rolling machine for practicing the method |
| CN202105953U (en) * | 2011-05-23 | 2012-01-11 | 山东美陵美力达风机有限公司 | Rolling-ring shaping device for a digital-control horizontal ring rolling machine |
| US8820043B2 (en) * | 2011-09-16 | 2014-09-02 | Rozanne E Adams | Method for heatless manufacture of horseshoes |
| CN104607580A (en) * | 2015-01-23 | 2015-05-13 | 无锡市派克重型铸锻有限公司 | Forging forming technology of aluminum alloy straight-flanked ring with extra-large specification |
| CN104759850A (en) * | 2015-04-03 | 2015-07-08 | 无锡市派克重型铸锻有限公司 | Processing technique of high aluminum alloy cylinder |
| CN105363823A (en) * | 2015-12-02 | 2016-03-02 | 贵州安大航空锻造有限责任公司 | Method for rolling aluminum alloy sheet forge pieces |
| CN105689629A (en) * | 2016-03-09 | 2016-06-22 | 无锡市派克重型铸锻有限公司 | Free forging method of novel ultrahigh conical ring part |
-
2016
- 2016-08-31 CN CN201610788390.2A patent/CN106363115A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS52131967A (en) * | 1976-03-19 | 1977-11-05 | Thyssen Ag | Method of fabricating annular work materials such as blind flanges having remarkably formed cross section and rolling machine for practicing the method |
| CN202105953U (en) * | 2011-05-23 | 2012-01-11 | 山东美陵美力达风机有限公司 | Rolling-ring shaping device for a digital-control horizontal ring rolling machine |
| US8820043B2 (en) * | 2011-09-16 | 2014-09-02 | Rozanne E Adams | Method for heatless manufacture of horseshoes |
| CN104607580A (en) * | 2015-01-23 | 2015-05-13 | 无锡市派克重型铸锻有限公司 | Forging forming technology of aluminum alloy straight-flanked ring with extra-large specification |
| CN104759850A (en) * | 2015-04-03 | 2015-07-08 | 无锡市派克重型铸锻有限公司 | Processing technique of high aluminum alloy cylinder |
| CN105363823A (en) * | 2015-12-02 | 2016-03-02 | 贵州安大航空锻造有限责任公司 | Method for rolling aluminum alloy sheet forge pieces |
| CN105689629A (en) * | 2016-03-09 | 2016-06-22 | 无锡市派克重型铸锻有限公司 | Free forging method of novel ultrahigh conical ring part |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112475806A (en) * | 2020-11-20 | 2021-03-12 | 西安航天发动机有限公司 | QCr0.8 alloy large-size conical-cylindrical ring forming process |
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