CN109434397A - A kind of preparation method of superalloy annular forging expanding die - Google Patents

A kind of preparation method of superalloy annular forging expanding die Download PDF

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Publication number
CN109434397A
CN109434397A CN201811516572.XA CN201811516572A CN109434397A CN 109434397 A CN109434397 A CN 109434397A CN 201811516572 A CN201811516572 A CN 201811516572A CN 109434397 A CN109434397 A CN 109434397A
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CN
China
Prior art keywords
ring
annular
forging
machine
bulging
Prior art date
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Pending
Application number
CN201811516572.XA
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Chinese (zh)
Inventor
秦卫东
廖毅
刘�东
赵兴东
吴娟利
甄小辉
王伟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shaanxi Hongyuan Aviation Forging Co Ltd
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Shaanxi Hongyuan Aviation Forging Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shaanxi Hongyuan Aviation Forging Co Ltd filed Critical Shaanxi Hongyuan Aviation Forging Co Ltd
Priority to CN201811516572.XA priority Critical patent/CN109434397A/en
Publication of CN109434397A publication Critical patent/CN109434397A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/24Making specific metal objects by operations not covered by a single other subclass or a group in this subclass dies

Abstract

The present invention relates to a kind of preparation methods of superalloy annular forging expanding die, it is characterized in that, the expanding die preparation process is as follows: jumping-up, punching are hollow ring billet after heating stainless steel bars to deformation temperature, after heating hollow ring billet to forging temperature, by hollow ring billet reaming for an outer profile and to the consistent annular element of superalloy annular forging inner ring facial contour of bulging;Annular element is heat-treated, anchor ring carries out after machine adds inside and outside it, divides valve for what annular element was cut into muti-piece same specification.The present invention adds the technique of cutting to prepare using looping mill rolling+machine, it is consistent with the inner ring surface section of high temperature alloy ring to bulging that an outer ring surface section is prepared for by looping mill rolling, and inner ring surface section is the special-shaped ring of rectangle, then thermally treated, internal outer ring surface carries out a small amount of machine and adds, and then carries out cutting.When greatly reducing machining using this technique and the waste of mold materials, the manufacturing cost of expanding die is reduced.

Description

A kind of preparation method of superalloy annular forging expanding die
Technical field
Reaming is rolled and machine adds the method for cutting to prepare for the forming of high temperature alloy ring heat expansion the present invention relates to a kind of Expanding die.
Background technique
The method for the expanding die for preparing superalloy annular forging at present has: directlying adopt biscuit machine and adds or pass through upsetting It is a rectangular section annular forging piece that the techniques such as cake, punching and reaming, which obtain, and then machine adds cutting.Using the technique, there are machines to add The problems such as working hour is long, mold materials utilization rate is low.It thus provides a kind of efficiently prepare anisotropic superalloy annular forging bulging The method of mold.
Summary of the invention
The object of the present invention is to provide a kind of using cerclage+machine, and to add the technique of cutting swollen to prepare high temperature alloy opposite sex ring The method of shape mold when can be shortened machining using this method, reduces the waste of mold materials, and is able to satisfy high temperature alloy ring The requirement of bulging.
To solve the above problems, the present invention efficiently prepares high temperature alloy expanding die method and adopts the following technical solutions It realizes:
A kind of preparation method of superalloy annular forging expanding die, the expanding die preparation process are as follows: heating Jumping-up, punching are hollow ring billet after stainless steel bars to deformation temperature, after heating hollow ring billet to forging temperature, by hollow ring billet Reaming is an outer profile and the consistent annular element 1 of superalloy annular forging inner ring facial contour to bulging;By annular element 1 into Row heat treatment, anchor ring carries out after machine adds inside and outside it, divides valve 2 for what annular element 1 was cut into muti-piece same specification.
Specific step is as follows: step 1: jumping-up is heated to deformation temperature according to the stainless steel bars of expanding die specification blanking Then degree carries out jumping-up in quick forging machine;Step 2: the biscuit after jumping-up is gone out centre bore with formed punch in quick forging machine and obtained by punching To hollow ring billet;Step 3: looping mill rolling, the hollow ring billet that step 2 is obtained are heated to place horizontal diameter axial direction looping mill rolling after deformation temperature Roll off on machine makes the continuous and local deformation that hollow ring billet carries out inner hole increase, wall thickness reduces, outer diameter increases, obtains an outer ring Face section with to the consistent annular element 1 in bulging superalloy annular forging inner ring surface section;Step 4: cutting, the annular that will be obtained 1 carry out machine of part adds, then divides valve 2 for what annular element 1 was cut into muti-piece same specification.
Preferably, the inner ring surface of annular element 1 described in step 3 is rectangle.The process of step 4 cutting is as follows: drawing one and ring The auxiliary circle that shape part 1 is with one heart, diameter is 100mm, 12 equal branches are then determined in auxiliary circle, are with each equal branch Point does the cutting line that two angles are 30 °, by the uniform cutting of annular element 1 is that 12 pieces of same specifications divide valve 2, and will divide valve 2 with to The superalloy annular forging of bulging is coupled in the bulging on shape expanding machine, for high-temperature alloy special-shaped ring.
It is compared with the prior art, beneficial effects of the present invention are as follows:
The preparation method of high temperature alloy ring expanding die of the present invention, using the work for adding cutting using looping mill rolling+machine Prepared by skill, it is with the inner ring surface section of high temperature alloy ring to bulging consistent to be prepared for an outer ring surface section by looping mill rolling, And inner ring surface section is the special-shaped ring of rectangle, then thermally treated, internal outer ring surface carries out a small amount of machine and adds, and is then cut Point.When greatly reducing machining using this technique and the waste of mold materials, the manufacturing cost of expanding die is reduced.
Detailed description of the invention
Invention is further described in detail with reference to the accompanying drawings and detailed description.
Fig. 1 is stainless steel annular element schematic diagram.
Fig. 2 carries out wire cutting cutting to stainless steel annular element.
Specific embodiment
Implement the preparation method of high-temperature alloy special-shaped annular forging piece heat expansion shaping dies of the present invention, it is desirable to provide forging Part heating furnace, quick forging machine, staving press and stainless steel bars.Fig. 1 is that machine adds expanding die schematic diagram.
Step 1: jumping-up.It is heated to deformation temperature according to the stainless steel bars of expanding die specification blanking, is then being forged fastly Machine carries out jumping-up.
Step 2: punching.Biscuit after jumping-up is rushed into thick centre bore with formed punch in quick forging machine and obtains hollow ring billet.
Step 3: looping mill rolling.The hollow ring billet that step 2 is obtained is heated to place horizontal diameter axial direction looping mill after deformation temperature Upper roll off makes the continuous and local deformation that hollow ring billet inner hole increases, wall thickness reduces, outer diameter increases, obtains an outer ring surface section It is consistent with to bulging ring inner ring surface section, and inner ring surface is the annular element 1 of rectangle.
Step 4: cutting.Obtained stainless steel ring is subjected to cutting.Dicing process are as follows: draw one with annular element 1 it is concentric, Diameter is the auxiliary circle of 100mm, then determines that 12 equal branches make two folders using each equal branch as starting point in auxiliary circle Angle is 30 ° of cutting line, by the uniform cutting of annular element 1 is that 12 pieces of same specifications divide valve 2, and will divide valve 2 with to the high temperature of bulging Alloy annular forging is coupled in the bulging on shape expanding machine, for high-temperature alloy special-shaped ring.

Claims (4)

1. a kind of preparation method of superalloy annular forging expanding die, which is characterized in that the expanding die preparation process As follows: jumping-up, punching are hollow ring billet after heating stainless steel bars to deformation temperature, after heating hollow ring billet to forging temperature, By hollow ring billet reaming for an outer profile and to the consistent annular element of superalloy annular forging inner ring facial contour of bulging (1);Annular element (1) is heat-treated, after anchor ring progress machine adds inside and outside it, annular element (1) is cut into muti-piece same specification Divide valve (2).
2. preparation method as described in claim 1, which is characterized in that specific step is as follows: step 1: jumping-up, according to bulging die The stainless steel bars of tool specification blanking are heated to deformation temperature, then carry out jumping-up in quick forging machine;Step 2: punching, after jumping-up Biscuit go out centre bore with formed punch in quick forging machine and obtain hollow ring billet;Step 3: looping mill rolling, the hollow ring billet that step 2 is obtained Roll off on horizontal diameter axial direction looping mill is placed after being heated to deformation temperature, so that hollow ring billet is carried out inner hole increase, wall thickness reduces, outer The continuous and local deformation that diameter increases, it is consistent with to bulging superalloy annular forging inner ring surface section to obtain an outer ring surface section Annular element (1);Step 4: cutting adds obtained annular element (1) carry out machine, then annular element (1) is cut into muti-piece with rule Lattice divide valve (2).
3. preparation method as claimed in claim 2, which is characterized in that the inner ring surface of annular element described in step 3 (1) is rectangle.
4. preparation method as claimed in claim 1 or 2, which is characterized in that the process of step 4 cutting is as follows: drawing one and ring The auxiliary circle that shape part (1) is with one heart, diameter is 100mm, 12 equal branches are then determined in auxiliary circle, are with each equal branch Point does the cutting line that two angles are 30 °, and by annular element (1), uniformly cutting is that 12 pieces of same specifications divide valve (2), and will divide valve (2) it is coupled with the superalloy annular forging to bulging in the bulging on shape expanding machine, for superalloy annular forging.
CN201811516572.XA 2018-12-11 2018-12-11 A kind of preparation method of superalloy annular forging expanding die Pending CN109434397A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811516572.XA CN109434397A (en) 2018-12-11 2018-12-11 A kind of preparation method of superalloy annular forging expanding die

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811516572.XA CN109434397A (en) 2018-12-11 2018-12-11 A kind of preparation method of superalloy annular forging expanding die

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CN109434397A true CN109434397A (en) 2019-03-08

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110936110A (en) * 2019-11-29 2020-03-31 中国航发沈阳黎明航空发动机有限责任公司 Machining process method for semi-ring parts
CN111024918A (en) * 2019-12-30 2020-04-17 西北工业大学 Method for evaluating residual stress distribution uniformity of annular forging
CN111644556A (en) * 2020-06-12 2020-09-11 无锡派克新材料科技股份有限公司 Manufacturing method of Ti64 alloy casing forging inclined-plane ring blank

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101279343A (en) * 2008-04-23 2008-10-08 贵州安大航空锻造有限责任公司 Method for rolling and shaping stainless steel special-shaped ring forging
CN102441604A (en) * 2011-11-24 2012-05-09 贵州安大航空锻造有限责任公司 Thermal bulging method for aluminum alloy special-shaped ring-rolled piece
CN103056230A (en) * 2013-01-15 2013-04-24 哈尔滨东安发动机(集团)有限公司 Cylinder bulging forming die
CN203955917U (en) * 2014-07-17 2014-11-26 山东华锐波纹管有限公司 A kind of reinforcement U-shaped bellows machinery bulging equipment
CN104801598A (en) * 2015-04-23 2015-07-29 西北工业大学 Bulging die for titanium-alloy thin-walled complicated irregular annular workpieces
CN204996929U (en) * 2015-04-23 2016-01-27 西北工业大学 Bulging die utensil of annular work piece
CN105290160A (en) * 2015-11-24 2016-02-03 哈尔滨工业大学 Sizing device for titanium alloy cylindrical spun part
CN105363975A (en) * 2015-12-02 2016-03-02 贵州安大航空锻造有限责任公司 Method for forming high-temperature alloy flange for aeroengine
CN105396938A (en) * 2015-12-02 2016-03-16 贵州安大航空锻造有限责任公司 Partial bulging device of high-temperature alloy flange for aircraft engine
CN106216538A (en) * 2016-08-04 2016-12-14 中南大学 A kind of major diameter ring mechanical expansion equipment
CN206373294U (en) * 2016-11-29 2017-08-04 贵州航宇科技发展股份有限公司 A kind of combined type shape expanding machine frock
CN107363154A (en) * 2017-07-11 2017-11-21 武汉理工大学 A kind of swollen extrusion forming method of complex mesh muscle ring

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101279343A (en) * 2008-04-23 2008-10-08 贵州安大航空锻造有限责任公司 Method for rolling and shaping stainless steel special-shaped ring forging
CN102441604A (en) * 2011-11-24 2012-05-09 贵州安大航空锻造有限责任公司 Thermal bulging method for aluminum alloy special-shaped ring-rolled piece
CN103056230A (en) * 2013-01-15 2013-04-24 哈尔滨东安发动机(集团)有限公司 Cylinder bulging forming die
CN203955917U (en) * 2014-07-17 2014-11-26 山东华锐波纹管有限公司 A kind of reinforcement U-shaped bellows machinery bulging equipment
CN104801598A (en) * 2015-04-23 2015-07-29 西北工业大学 Bulging die for titanium-alloy thin-walled complicated irregular annular workpieces
CN204996929U (en) * 2015-04-23 2016-01-27 西北工业大学 Bulging die utensil of annular work piece
CN105290160A (en) * 2015-11-24 2016-02-03 哈尔滨工业大学 Sizing device for titanium alloy cylindrical spun part
CN105363975A (en) * 2015-12-02 2016-03-02 贵州安大航空锻造有限责任公司 Method for forming high-temperature alloy flange for aeroengine
CN105396938A (en) * 2015-12-02 2016-03-16 贵州安大航空锻造有限责任公司 Partial bulging device of high-temperature alloy flange for aircraft engine
CN106216538A (en) * 2016-08-04 2016-12-14 中南大学 A kind of major diameter ring mechanical expansion equipment
CN206373294U (en) * 2016-11-29 2017-08-04 贵州航宇科技发展股份有限公司 A kind of combined type shape expanding machine frock
CN107363154A (en) * 2017-07-11 2017-11-21 武汉理工大学 A kind of swollen extrusion forming method of complex mesh muscle ring

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110936110A (en) * 2019-11-29 2020-03-31 中国航发沈阳黎明航空发动机有限责任公司 Machining process method for semi-ring parts
CN110936110B (en) * 2019-11-29 2022-03-18 中国航发沈阳黎明航空发动机有限责任公司 Machining process method for semi-ring parts
CN111024918A (en) * 2019-12-30 2020-04-17 西北工业大学 Method for evaluating residual stress distribution uniformity of annular forging
CN111644556A (en) * 2020-06-12 2020-09-11 无锡派克新材料科技股份有限公司 Manufacturing method of Ti64 alloy casing forging inclined-plane ring blank
CN111644556B (en) * 2020-06-12 2021-12-07 无锡派克新材料科技股份有限公司 Manufacturing method of Ti64 alloy casing forging inclined-plane ring blank

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