CN109175179A - A kind of high temperature alloy forging process for fuel pulling method - Google Patents

A kind of high temperature alloy forging process for fuel pulling method Download PDF

Info

Publication number
CN109175179A
CN109175179A CN201811410369.4A CN201811410369A CN109175179A CN 109175179 A CN109175179 A CN 109175179A CN 201811410369 A CN201811410369 A CN 201811410369A CN 109175179 A CN109175179 A CN 109175179A
Authority
CN
China
Prior art keywords
forging
blank
mold
type groove
section
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.)
Pending
Application number
CN201811410369.4A
Other languages
Chinese (zh)
Inventor
江杨辉
朴学华
秦婷婷
李建军
左华付
张强
彭谦之
隆如军
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.)
AECC South Industry Co Ltd
Original Assignee
AECC South Industry 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 AECC South Industry Co Ltd filed Critical AECC South Industry Co Ltd
Priority to CN201811410369.4A priority Critical patent/CN109175179A/en
Publication of CN109175179A publication Critical patent/CN109175179A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/06Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J13/00Details of machines for forging, pressing, or hammering
    • B21J13/02Dies or mountings therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/02Die forging; Trimming by making use of special dies ; Punching during forging

Abstract

A kind of high temperature alloy forging process for fuel pulling method, being used to forge diameter is D1, length L1Cylindrical structure forging comprising following steps: step A, interception blank are placed in heating furnace and heat and keep the temperature, blank diameter D0, length L0.Step B, one mold is provided, the mold is composed of symmetrically arranged upper die and lower die, the mold that combination is formed includes a prismatic type groove and an arc-shaped type groove, blank after step A heat preservation is pulled out using the mold, firstly, in the prismatic type groove, blank is forged and pressed by 90 ° of spiral overturning chargings first, highly by D0It is depressed intoThen, in the prismatic type groove, blank is forged and pressed by the overturning charging of 45 ° of spirals, highly byIt is depressed into D1, finally, polygonal cross-section is rolled into circular cross-section in arc-shaped type groove, make diameter D1.Complete the forging of the forging.High temperature alloy forging process for fuel provided by the present invention pulls out method, can significantly improve the uniformity of material deformation.

Description

A kind of high temperature alloy forging process for fuel pulling method
Technical field
The present invention relates to a kind of technical field of forging, especially a kind of high temperature alloy axis that can be improved aero-engine The draw out method of forging or disk bar one forging bar portion grain uniformity.
Background technique
In manufacturing fields such as automobile, aerospace, ships using very extensive, material is covered for shaft forgings or disk bar integral piece Structural steel, titanium alloy, high temperature alloy etc..The all too busy to get away pulling of forging and molding of shaft forgings, dish axle integral piece.Pulling is to make metal The basic forging process that cross-sectional area reduces, length increases.Wherein, forged shaft shapes its technical process are as follows: and blanking → Heating → draw out;The technical process of dish axle one forging forming are as follows: blanking → heating → forming bar portion (pull out by forging It is long) → forming pan portion.Flat anvil (hammer anvil that the scope of attack is plane) is to forge most simple most common tool, but carry out on flat anvil One significant disadvantage of draw out is exactly that the uniformity of forging bar portion crystal grain is difficult to control.Through analyzing, this defect is mainly It is related with the method for forging as caused by deforming unevenly.Fig. 1 is typical circular cross-section bar flat-anvils stretching Principle of Process Schematic diagram, shown in Figure 1, blank is forged between upper and lower hammer anvil and is constantly overturn, and section is by initial circular cross-section Square-section is forged into, cubic pulling is then carried out, finally further through chamfered edge and round as a ball becomes round section.In forming process, Bar sectional dimension reduces, elongated lengthwise.Fig. 2 is cubic pulling stage cross-sectional deformation Distribution Principle schematic diagram in Fig. 1, It is shown in Figure 2, it rubs since flat anvil and forge piece blank reheating surface exist, the friction effects distribution of stress causes not same district Area deformation degree is uneven.Easily-deformable area I, free deformation zone II and stagnant zone III can be successively divided by deflection size.Its Middle stagnant zone III deflection is minimum, and free deformation zone II deflection is smaller, and easily-deformable area I deflection is maximum.The unevenness of deformation Even influence Dynamic Recrystallization, to influence the uniformity of crystal grain, especially free deformation zone II and stagnant zone III become Shape amount is easy to fall into the critical strain area of metal, causes the abnormal growth of crystal grain, increases the inhomogeneities of crystal grain, so as to Final forging quality is had an impact.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of high temperature alloy forging process for fuel to pull out method, to be reduced or avoided The problem of being formerly mentioned.
In order to solve the above technical problems, the present invention provides a kind of high temperature alloy forging process for fuel to pull out method, it is used to forge Making diameter is D1, length L1Cylindrical structure forging comprising following steps:
Step A, interception blank, which is placed in heating furnace, to be heated and keeps the temperature, and the blank intercepted is cylindrical structure, diameter D0、 Length is L0
Step B provides a mold, and the mold is composed of symmetrically arranged upper die and lower die, combines formation The mold includes a prismatic type groove and an arc-shaped type groove, and the top and bottom of the prismatic type groove are symmetrical arranged oriented Interior arc convex is pulled out the blank after step A heat preservation using the mold, the first stage, in the prismatic type groove It is interior, blank is forged and pressed by 90 ° of spiral overturning chargings first, the length that forging is axially sent into every time is equal to mold thickness B, high Degree is by D0It is depressed intoThus circular cross-section is forged into the polygonal cross-section by multi-section circular arc and rectilinear(-al).Second-order Section is forged and pressed blank by 45 ° of spiral overturning chargings, the length etc. that forging is axially sent into every time in the prismatic type groove In mold thickness B, highly byIt is depressed into D1, obtain the polygonal cross-section being made of more circular arcs and straightway.Finally, in circle Polygonal cross-section is rolled into circular cross-section in arc type groove, makes diameter D1.Complete the forging of the forging.
Preferably, in step, the size of the blank intercepted meets following condition:
D0Meet simultaneouslyWithCondition, furthermore D0 2/D1 2Value less than 3.It L is obtained according to isometric conversion afterwards0Numerical value.
Preferably, in step, the size of the blank intercepted meets following condition: D0=1.5D1,
Preferably, in stepb, the size of the arc convex is calculated according to following formula:
In above formula
α is the cornerite of the prismatic type groove.
Preferably, α chooses within the scope of 110-140 °.
Preferably, α is set as 120 °.
Preferably, in stepb, thickness B=(0.4~0.8) D of the mold0,
Preferably, in step, the blank is placed in time of the temperature and heat preservation that heat in heating furnace according to being used The forging technology specification of material selected.
Preferably, in stepb, the prismatic type groove and the arc-shaped type groove are respectively two before and after with the mold The junction of a end face is provided with knuckle R.
Preferably, the knuckle R is designed by the general norm requirement of design of forging die.
A kind of high temperature alloy forging process for fuel provided by the present invention pulls out method, the forging as pulling process axis/bar Apparent " stagnant zone " be there will be no in the cross section of part, therefore can also significantly improve the uniformity of material deformation, to reach To the purpose for improving grain uniformity.In addition, using draw out method of the invention, the deep enough blank core of deformation energy makes Core has biggish deformation, is conducive to the microstructural defects for eliminating core.In conclusion the present invention is relative to prior art, With apparent technical effect, defect present in prior art is overcome.
Detailed description of the invention
The following drawings are only intended to schematically illustrate and explain the present invention, not delimit the scope of the invention.Wherein,
Fig. 1 Fig. 1 is typical circular cross-section bar flat-anvils stretching Principle of Process schematic diagram;
Fig. 2 is cubic pulling stage cross-sectional deformation Distribution Principle schematic diagram in Fig. 1;
Fig. 3 is that a kind of high temperature alloy forging process for fuel of a specific embodiment according to the present invention pulls out the process original of method Manage schematic diagram;
Fig. 4 is the principle schematic diagram of the mold of Fig. 3;
Fig. 5 is the blank of Fig. 3 and the principle schematic diagram of forging;
Fig. 6 is the stereochemical structure schematic illustration of the mold of Fig. 4;
Fig. 7 is using process shown in Fig. 3 to forging cross section equivalent strain Distribution Principle schematic diagram after forging pulling.
Specific embodiment
For a clearer understanding of the technical characteristics, objects and effects of the present invention, this hair of Detailed description of the invention is now compareed Bright specific embodiment.Wherein, identical component uses identical label.
Fig. 3 is that a kind of high temperature alloy forging process for fuel of a specific embodiment according to the present invention pulls out the process original of method Manage schematic diagram;Fig. 4 is the principle schematic diagram of the mold of Fig. 2;Wherein left side is schematic view of the front view, and right side is left side A-A and B-B the schematic diagram of the section structure, the xy coordinate direction identified in Fig. 4 is for the schematic view of the front view on the left of indicating Coordinate system, 5 for Fig. 3 blank and forging principle schematic diagram;Fig. 6 is the stereochemical structure principle signal of the mold of Fig. 4 Figure.Referring to shown in Fig. 3-6, the present invention provides a kind of high temperature alloy forging process for fuel to pull out method, and the forging is cylindrical structure, Diameter is D1, length L1, described method includes following steps:
Step A, interception blank, which is placed in heating furnace, to be heated and keeps the temperature, and the blank intercepted is cylindrical structure, diameter D0、 Length is L0, the size of the blank intercepted meets following formula:
D0It should meet simultaneously firstWithCritical condition, can make so every time Critical strain amount needed for the deflection of forging and stamping is above metal dynamic recrystallization.On this basis, D0 2/D1 2Value should be less than 3.0.It is last that L is obtained according to isometric conversion0Numerical value, such as work as D0=1.5D1When,
The time that the blank is placed in the temperature and heat preservation that heat in heating furnace can be according to the forging skill of used material Art specification is selected.
Step B provides a mold, and the mold is composed of symmetrically arranged upper die and lower die, combines formation The mold includes a prismatic type groove and an arc-shaped type groove, as shown in the mark " calculated according to parametric equation " in Fig. 4, Inside arc convex is symmetrically arranged at the top and bottom of the prismatic type groove, the size of the arc convex is according to following public affairs Formula calculates:
In above formula
α be the prismatic type groove cornerite (α chooses within the scope of 110-140 °, in a preferred embodiment, α setting It is 120 °);
Thickness B=(0.4~0.8) D of the mold0,;The prismatic type groove and the arc-shaped type groove and the mold Former and later two end faces knuckle R by design of forging die general norm requirement design.
Blank after step A heat preservation is pulled out using the mold, it is the first stage, right in the prismatic type groove Blank is forged and pressed by the overturning charging of 90 ° of spirals first, and the length that forging is axially sent into every time is equal to mold thickness B, highly by D0It is depressed intoThus circular cross-section is forged into the polygonal cross-section by multi-section circular arc and rectilinear(-al).Second stage, In the prismatic type groove, blank is forged and pressed by 45 ° of spiral overturning chargings, the length that forging is axially sent into every time is equal to mold Thickness B, highly byIt is depressed into D1, obtain the polygonal cross-section being made of more circular arcs and straightway.Finally, in arc-shaped type Polygonal cross-section is rolled into circular cross-section in slot, makes diameter D1.Complete the forging of the forging.
Fig. 7 is using process shown in Fig. 3 to forging cross section equivalent strain distribution schematic diagram after forging pulling, referring to Fig. 7 Shown, using above-mentioned draw out method provided by the present invention, the cross section for pulling out forging as process axis/bar will not There is apparent " stagnant zone " again, therefore can also significantly improve the uniformity of material deformation, so that it is uniform to reach raising crystal grain The purpose of property.In addition, using draw out method of the invention, the deep enough blank core of deformation energy makes core have biggish change Shape is conducive to the microstructural defects for eliminating core.In conclusion the present invention has apparent technology relative to prior art Effect overcomes defect present in prior art.
It will be appreciated by those skilled in the art that although the present invention is described in the way of multiple embodiments, It is that not each embodiment only contains an independent technical solution.So narration is used for the purpose of for the sake of understanding in specification, The skilled in the art should refer to the specification as a whole is understood, and by technical solution involved in each embodiment Regard as and can be combined with each other into the modes of different embodiments to understand protection scope of the present invention.
The foregoing is merely the schematical specific embodiment of the present invention, the range being not intended to limit the invention.It is any Those skilled in the art, made equivalent variations, modification and combination under the premise of not departing from design and the principle of the present invention, It should belong to the scope of protection of the invention.

Claims (10)

1. a kind of high temperature alloy forging process for fuel pulls out method, being used to forge diameter is D1, length L1Cylindrical structure forging, It is characterized in that, it includes the following steps:
Step A, interception blank, which is placed in heating furnace, to be heated and keeps the temperature, and the blank intercepted is cylindrical structure, diameter D0, length For L0
Step B provides a mold, and the mold is composed of symmetrically arranged upper die and lower die, combines the described of formation Mold includes a prismatic type groove and an arc-shaped type groove, is symmetrically arranged at the top and bottom of the prismatic type groove inside Arc convex pulls out the blank after step A heat preservation using the mold, the first stage, right in the prismatic type groove Blank is forged and pressed by the overturning charging of 90 ° of spirals first, and the length that forging is axially sent into every time is equal to mold thickness B, highly by D0It is depressed intoThus circular cross-section is forged into the polygonal cross-section by multi-section circular arc and rectilinear(-al).Second stage, In the prismatic type groove, blank is forged and pressed by 45 ° of spiral overturning chargings, the length that forging is axially sent into every time is equal to mold Thickness B, highly byIt is depressed into D1, obtain the polygonal cross-section being made of more circular arcs and straightway.Finally, in arc-shaped type Polygonal cross-section is rolled into circular cross-section in slot, makes diameter D1.Complete the forging of the forging.
2. the method according to claim 1, wherein in step, the size of the blank intercepted meets as follows Condition:
D0Meet simultaneouslyWithCondition, furthermore D0 2/D1 2Value less than 3.Root later L is obtained according to isometric conversion0Numerical value.
3. the method according to claim 1, wherein in step, the size of the blank intercepted meets as follows Condition: D0=1.5D1,
4. the method according to claim 1, wherein in stepb, the size of the arc convex is according to as follows Formula calculates:
In above formula
α is the cornerite of the prismatic type groove.
5. according to the method described in claim 4, it is characterized in that, α chooses within the scope of 110-140 °.
6. according to the method described in claim 4, it is characterized in that, α is set as 120 °.
7. the method according to claim 1, wherein in stepb, the thickness B=of the mold (0.4~ 0.8)D0,.
8. the method according to claim 1, wherein in step, the blank is placed in be heated in heating furnace The time of temperature and heat preservation is selected according to the forging technology specification of used material.
9. the method according to claim 1, wherein in stepb, the prismatic type groove and the arc-shaped type Slot is provided with knuckle R in the junction of former and later two end faces with the mold respectively.
10. according to the method described in claim 9, it is characterized in that, the knuckle R is wanted by the general norm of design of forging die Seek design.
CN201811410369.4A 2018-11-23 2018-11-23 A kind of high temperature alloy forging process for fuel pulling method Pending CN109175179A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811410369.4A CN109175179A (en) 2018-11-23 2018-11-23 A kind of high temperature alloy forging process for fuel pulling method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811410369.4A CN109175179A (en) 2018-11-23 2018-11-23 A kind of high temperature alloy forging process for fuel pulling method

Publications (1)

Publication Number Publication Date
CN109175179A true CN109175179A (en) 2019-01-11

Family

ID=64937902

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811410369.4A Pending CN109175179A (en) 2018-11-23 2018-11-23 A kind of high temperature alloy forging process for fuel pulling method

Country Status (1)

Country Link
CN (1) CN109175179A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111001744A (en) * 2019-12-23 2020-04-14 安徽省瑞杰锻造有限责任公司 Forging process and forging device for arch bridge pull rod
CN113486477A (en) * 2021-08-20 2021-10-08 中国航发沈阳黎明航空发动机有限责任公司 Method for designing prefabricated blank of high-temperature-resistant alloy complex single-tenon blade forging
CN115950371A (en) * 2023-02-27 2023-04-11 中国矿业大学 One-point strain measurement method based on optical microscopy

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61103637A (en) * 1984-10-26 1986-05-22 Kawasaki Steel Corp Forging method of metallic material
JPS62284053A (en) * 1986-06-03 1987-12-09 Nippon Steel Corp Method for forging titanium alloy material
WO2007080750A1 (en) * 2006-01-13 2007-07-19 Osaka Titanium Technologies Co., Ltd. Process for production of titanium material for sputtering
CN101513664A (en) * 2009-04-01 2009-08-26 燕山大学 Efficient forging method using curved-surface swage blocks

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61103637A (en) * 1984-10-26 1986-05-22 Kawasaki Steel Corp Forging method of metallic material
JPS62284053A (en) * 1986-06-03 1987-12-09 Nippon Steel Corp Method for forging titanium alloy material
WO2007080750A1 (en) * 2006-01-13 2007-07-19 Osaka Titanium Technologies Co., Ltd. Process for production of titanium material for sputtering
CN101513664A (en) * 2009-04-01 2009-08-26 燕山大学 Efficient forging method using curved-surface swage blocks

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
付强等: "不同型砧下大型轴类锻件倒棱滚圆过程的数值模拟研究", 《模具技术》 *
王以华等: "型砧几何尺寸对大锻件锻造孔隙闭合的影响 ", 《金属加工(热加工)》 *
赵玲玲等: "大锻件锻造拔长砧型", 《塑性工程学报》 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111001744A (en) * 2019-12-23 2020-04-14 安徽省瑞杰锻造有限责任公司 Forging process and forging device for arch bridge pull rod
CN113486477A (en) * 2021-08-20 2021-10-08 中国航发沈阳黎明航空发动机有限责任公司 Method for designing prefabricated blank of high-temperature-resistant alloy complex single-tenon blade forging
CN113486477B (en) * 2021-08-20 2023-06-09 中国航发沈阳黎明航空发动机有限责任公司 Design method of high-temperature-resistant alloy complex single-tenon blade forging preform
CN115950371A (en) * 2023-02-27 2023-04-11 中国矿业大学 One-point strain measurement method based on optical microscopy
CN115950371B (en) * 2023-02-27 2023-10-03 中国矿业大学 Optical microscopy-based one-point strain measurement method

Similar Documents

Publication Publication Date Title
CN109175179A (en) A kind of high temperature alloy forging process for fuel pulling method
CN100500881C (en) Process of making ring fine crystal blank of GH4169 alloy for near constant temperature forging
CN104841711B (en) A kind of crimp processing mold preparing Ultra-fine Grained beta-titanium alloy and technique
CN106868436A (en) A kind of fast footpath forging Joint Production GH4169 alloy fine grain bar manufacture method
CN106854742B (en) The preparation method of silk material is justified in a kind of cold-heading with TC16 alloy discs
CN107282688B (en) A kind of preparation method of Ti45Nb alloy disc circle silk material
CN107252866B (en) The multiple protrusion ozzle large-sized end enclosure forging integral forging and forming methods of nuclear reactor band
CN109079072A (en) Large-scale TC4 alloy rings structural homogenity forging method
CN103341580B (en) Free forging method for medium-pressure combined regulation valve stem workblank of supercritical turbine
Zhbankov et al. Rational parameters of profiled workpieces for an upsetting process
CN108446478A (en) A kind of design method of multicomponent high strength titanium alloy
CN104174685B (en) Turbine rotor groove is carved by profiled bar and processing method thereof
CN105073295A (en) Ring-rolling blank
Shimoyama et al. Effect of grooved roll profiles on microstructure evolutions of AZ31 sheets in Periodical Straining Rolling process
CN112948986A (en) Titanium alloy forging process parameter optimization method combined with finite element numerical simulation program
CN107127282A (en) A kind of isothermal forging method of the high muscle thin web plate class part of magnesium alloy
CN117161277A (en) Rolling forming process for shell flange
CN107755607A (en) Manufacturing process on a kind of band angle stock forging flat-die hammer
CN110014106A (en) Large-size titanium alloy hollow blank preparation method
CN1285249A (en) Method for forming fan-shape polygon frame forge piece
CN107761062B (en) Method for manufacturing target blank and target assembly
CN101782531A (en) Method for judging metallurgical quality of titanium alloy blade
CN112692203A (en) Forging method of Nb47Ti alloy large-size bar for superconducting wire
CN114029438A (en) Preparation method for improving structure uniformity of TC4 special-grade disc type forge piece
CN106111871B (en) A kind of convex recessed swage block of circular arc dentation

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20190111