CN104690198B - Forming method of large GH4169 alloy direct aging disc forging - Google Patents
Forming method of large GH4169 alloy direct aging disc forging Download PDFInfo
- Publication number
- CN104690198B CN104690198B CN201310666925.5A CN201310666925A CN104690198B CN 104690198 B CN104690198 B CN 104690198B CN 201310666925 A CN201310666925 A CN 201310666925A CN 104690198 B CN104690198 B CN 104690198B
- Authority
- CN
- China
- Prior art keywords
- forging
- die
- direct aging
- forming
- mould
- 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.)
- Active
Links
Landscapes
- Forging (AREA)
Abstract
The invention discloses a technology of 'die forging for blank forming plus die forging for forming plus direct aging' for the forming problem of the large GH4169 alloy direct aging disc forging. Since the traditional 'free forging for blank forming' is changed into the 'die forging for blank forming', uncontrollable factors of larger heating number and deformation in a free forging procedure are eliminated; the control of heating and the deformation in a forging technology are guaranteed; a forging after final direct aging treatment can stably meet requirements of a level ten grain size; the production efficiency is improved; and the cost is lowered.
Description
Technical field:
The present invention relates to the method for forging and molding of large-scale gh4169 alloy direct aging disk forging part, particularly projected area
More than 0.2m2And grain size requires 10 grades of disk forge piece.
Background technology:
Gh4169 alloy is the nickel-base high-temperature conjunction of a kind of γ " with body-centered tetragonal and face-centred cubic γ ' phase precipitation strength
Gold, is mainly used in the crucial load part of Aero-Space equipment, and these crucial load parts forging used when manufacturing is to property
Can there is very high requirement, the crucial load part for some engine core positions is it is desirable to the complete warm of gh4169 alloy forging
After grain size after process reaches 10 grades, and routine has been forged, the grain size that solid-solution and aging heat treatment does not almost reach 10 grades will
Ask, even if adopting direct aging Technology for Heating Processing, also due to the open die forging base moderate heat of routine time is more, deflection is uncontrollable
Former thus result in technique unstable (crystal grain refinement it is critical only that the control to heating and deflection in forging technology, and freely
Forging is difficult to control to), therefore according to the technique of traditional " open die forging base+die-forging forming+direct aging ", end product quality
Unstable it is impossible to stable reach 10 grades of grain sizes and require.
Traditional gh4169 alloy disc class takes the side of " open die forging base+die forging " in the forging part of direct aging before processing
Formula completes, and generally has following two typical process routes: Yi Zhongshi: upsetting cake → punching → horse expansion → reaming (ring billet) → die forging,
This technique is more due to forging technology link and fire time, and the multiple small deformation of horse expansion process can lead to the inequality of blank tissue
Even require it is more difficult to reach more than 8 grades grain sizes of ring billet.Second is: upsetting cake → punching → reaming (ring billet) → die forging, this side
Case advantage is to eliminate horse to expand operation, improves efficiency, simultaneously because the increase of reaming link deflection improves the tissue water of ring billet
Flat;Shortcoming is, after removal horse is expanded, to increased the difficulty of reaming, that is, reaming one fire completes more than 40% deflection, equipment energy
Power requirement is higher, and the operability of technique needs to consider;Both the above process program due to being related to free forging process, by artificial because
Element affects larger, unstable product quality, therefore is difficult to meet forging's block dimension and integrative organization's performance requirement.
The invention discloses a kind of technique of " die forging base+die-forging forming+direct aging ", by by traditional " freely
Forging base " is changed to " die forging base ", and it is time more to eliminate open die forging operation moderate heat, and the uncontrollable factor of deflection is it is ensured that forging
Make controlling it is ensured that the forging after final direct aging is processed can stably reach 10 grades of crystalline substance to heating and deflection in technique
Granularity requirements, improve production efficiency, reduce cost.
The technical problem of the present invention is:
For the forging molding of large-scale gh4169 alloy direct aging disk forging part, according to traditional " open die forging base+
The technique of die-forging forming+direct aging ", end product quality is unstable it is impossible to the stable 10 grades of grain sizes that reach require.
Technical scheme:
Step 1 prefabricated blank, is completed upsetting cake and punching operation by the way of die-forging forming, controls deflection by mould
Between 50% to 55%, to remove punching core material by machining, to improve ring billet size and metallurgical quality concordance;
Step 2 preforming, completes reaming operation using the swollen hole of die forging, controls deflection 20% to 25% by mould
Between;
Step 3 die-forging forming, using the fiery molding of finish-forging die one, by mould control deflection 30% to 35% it
Between;
Enter water in 30s after the completion of step 4 die-forging forming, be cooled to room temperature, complete direct aging and process.
The invention has the beneficial effects as follows:
Open die forging upsetting cake, punching are replaced using die-forging forming, improves technology stability;Ring is replaced using the swollen hole of die forging
Roll, reasonable distribution and control deflection, improve ring billet performance;
On the whole, by traditional " open die forging base " is changed to " die forging base ", eliminate open die forging operation moderate heat
Secondary more, the uncontrollable factor of deflection it is ensured that in forging technology to the control of heating and deflection it is ensured that finally directly when
The grain size that forging after effect process can stably reach 10 grades requires, and improves production efficiency, reduces manufacturing cost.
Concrete case embodiment
Below with reference to embodiment, technical solution of the present invention is further described:
Large-scale gh4169 alloy direct aging disk forging of the present invention, external diameter φ 681mm, internal diameter φ 374mm, projection
Area is about 0.25m2, all round properties index of forging and grain size require to meet the requirement of xx-0515 standard (grain size will
Ask 10 grades).
Its forging step is as follows in detail:
The first step designs the pattern of upsetting cake, increases drift in the centre up and down of pattern, bar is directly put into pattern
In, hammer to certain height, make blank just be full of die cavity (not going out burr), complete prefabricated blank molding.
The web portion extension set at prefabricated blank center is added to fall by second step by mach mode, so far realizes traditional handicraft
The work to be done of middle upsetting cake, two operations of punching, this operation deflection reaches more than 50%, and grain size can improve 2~2.5
Level.
3rd step design preforming tool, the lower mould of this mould has the fuse of a taper, and fuse has two kinds of gradients,
Top is 15 degree, and lower section is 10 degree it is therefore an objective to by the gradient of taper fuse in swollen hole, realize traditional reaming operation to be done
Work, this operation deflection is less, controls deflection between 20% to 25% by mould, mainly makes crystal grain no longer long
Greatly.
After 4th step completes preforming operation, waste base is directly placed in finish-forging die die cavity, completes die forging final molding,
This operation deflection reaches more than 30%, and crystal grain can refine 1~1.5 grade.
Enter water after the completion of 5th step die-forging forming in 30s, be cooled to room temperature, complete direct aging and process.
The homogeneous fire of forging process of this technique completes, and on the basis of meeting forging molding, after tested, finally can stablize
To the microscopic structure (10 grades of grain sizes) meeting standard requirement.
Claims (1)
1. a kind of forming method of large-scale gh4169 alloy direct aging disk forging is it is characterised in that comprise the steps,
Step 1 prefabricated blank, completes upsetting cake and punching operation by the way of die-forging forming, controls deflection 50% by mould
To between 55%, to remove punching core material by machining, to improve ring billet size and metallurgical quality concordance;
Step 2 preforming, completes reaming operation using the swollen hole of die forging, controls deflection between 20% to 25% by mould;
Step 3 die-forging forming, using the fiery molding of finish-forging die one, controls deflection between 30% to 35% by mould;
Enter water in 30s after the completion of step 4 die-forging forming, be cooled to room temperature, complete direct aging and process.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310666925.5A CN104690198B (en) | 2013-12-10 | 2013-12-10 | Forming method of large GH4169 alloy direct aging disc forging |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310666925.5A CN104690198B (en) | 2013-12-10 | 2013-12-10 | Forming method of large GH4169 alloy direct aging disc forging |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104690198A CN104690198A (en) | 2015-06-10 |
CN104690198B true CN104690198B (en) | 2017-02-01 |
Family
ID=53337960
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201310666925.5A Active CN104690198B (en) | 2013-12-10 | 2013-12-10 | Forming method of large GH4169 alloy direct aging disc forging |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104690198B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106111862B (en) * | 2016-08-29 | 2017-12-26 | 中航动力股份有限公司 | A kind of forging method of GH4901 sleeves spacer ring |
CN108160887A (en) * | 2016-12-07 | 2018-06-15 | 陕西宏远航空锻造有限责任公司 | A kind of forming method of large size GH4169 alloy annular forging |
CN107175306A (en) * | 2017-07-18 | 2017-09-19 | 中国第二重型机械集团德阳万航模锻有限责任公司 | The large-scale forging part forging method of fine grain AF1410 steel |
CN108246947A (en) * | 2017-12-07 | 2018-07-06 | 陕西宏远航空锻造有限责任公司 | A kind of GH4169 alloy die forgings improve the forging method of flaw detection bottom damage |
CN107913963B (en) * | 2017-12-07 | 2019-06-28 | 陕西宏远航空锻造有限责任公司 | A kind of GH4169 alloy annular forging forming method |
CN110976740B (en) * | 2019-12-19 | 2022-02-08 | 陕西宏远航空锻造有限责任公司 | Method for manufacturing drum shaft forging |
CN111659842B (en) * | 2020-05-27 | 2022-05-31 | 四川工程职业技术学院 | Die forging processing method for variable-section titanium alloy frame type forge piece |
CN112719180B (en) * | 2020-12-18 | 2023-07-21 | 陕西宏远航空锻造有限责任公司 | Forming method of large GH4169 alloy disc-shaped forging |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5759305A (en) * | 1996-02-07 | 1998-06-02 | General Electric Company | Grain size control in nickel base superalloys |
CN101036931A (en) * | 2007-03-05 | 2007-09-19 | 贵州安大航空锻造有限责任公司 | Near-isothermal forging method of GH4169 alloy disc-shaped forging in air |
CN101181730A (en) * | 2007-12-07 | 2008-05-21 | 江阴隆澄钻采机械制造有限公司 | Drill pipe joint precision die forging process |
CN101332484A (en) * | 2007-06-25 | 2008-12-31 | 宝山钢铁股份有限公司 | Die forging method of high-temperature alloy |
CN102764837A (en) * | 2012-07-05 | 2012-11-07 | 无锡市钻通工程机械有限公司 | Method for forging GH4169 disc-shaped piece |
CN103341586A (en) * | 2013-06-07 | 2013-10-09 | 北京科技大学 | Method for achieving forming of GH4738 nickel-base superalloy turbine discs |
-
2013
- 2013-12-10 CN CN201310666925.5A patent/CN104690198B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5759305A (en) * | 1996-02-07 | 1998-06-02 | General Electric Company | Grain size control in nickel base superalloys |
CN101036931A (en) * | 2007-03-05 | 2007-09-19 | 贵州安大航空锻造有限责任公司 | Near-isothermal forging method of GH4169 alloy disc-shaped forging in air |
CN101332484A (en) * | 2007-06-25 | 2008-12-31 | 宝山钢铁股份有限公司 | Die forging method of high-temperature alloy |
CN101181730A (en) * | 2007-12-07 | 2008-05-21 | 江阴隆澄钻采机械制造有限公司 | Drill pipe joint precision die forging process |
CN102764837A (en) * | 2012-07-05 | 2012-11-07 | 无锡市钻通工程机械有限公司 | Method for forging GH4169 disc-shaped piece |
CN103341586A (en) * | 2013-06-07 | 2013-10-09 | 北京科技大学 | Method for achieving forming of GH4738 nickel-base superalloy turbine discs |
Also Published As
Publication number | Publication date |
---|---|
CN104690198A (en) | 2015-06-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104690198B (en) | Forming method of large GH4169 alloy direct aging disc forging | |
CN108160887A (en) | A kind of forming method of large size GH4169 alloy annular forging | |
CN106363352B (en) | A kind of manufacturing process of high-strength aluminum alloy ring forging | |
CN103469136B (en) | The preparation method of the TC11 titanium alloy cake material that a kind of fatigue strength is high | |
CN106475500B (en) | A kind of Heavy Pan Forgings forging technology | |
CN104722702B (en) | Supercritical unit high temperature steam pipeline forging molding process | |
CN102500733A (en) | Forging method for efficiently healing internal hole-type defects of steel ingot | |
CN102172815B (en) | Hot extrusion forming method for inner hexagonal bolt blank of titanium alloy | |
CN105170865B (en) | A kind of crystal grain control method of explosive valve GH690 alloys shearing lid | |
CN106541064A (en) | A kind of hammer cogging process of super large-scale aluminium alloy ingot casting | |
CN102784877B (en) | Heading process of stainless steel rivet nut | |
CN107186139B (en) | The H profile steel manufacturing method of nuclear fusion stack magnet support | |
CN108890218A (en) | A kind of high strength heat resistant alloy forge piece manufacturing process | |
CN104139145A (en) | Method for forging guide horn mouth forge pieces applied to internal components of nuclear reactor | |
CN104707927B (en) | A kind of improve variable cross-section aluminum alloy die forgings tissue and the hot-working method of performance | |
CN105177264A (en) | Manufacturing method for stainless steel forged round steel | |
CN104907472A (en) | Forging forming method for high temperature alloy frame-shaped piece | |
CN104338882A (en) | Forming method of motor enclosure forging of third-generation nuclear power coolant pump | |
CN104338879B (en) | The method for forging and molding of generation Ⅲ nuclear power cooling medium pump pump case | |
CN109622866A (en) | The manufacturing process of large-scale GH4169 alloy forged piece | |
CN107012415A (en) | A kind of preparation method of wrought aluminium alloy high solid fractions semi solid slurry applied to semi-solid die casting | |
CN103056260B (en) | A kind of major axis class big inclination angle flange forge piece manufacturing process | |
CN204035446U (en) | The mould of nuclear power hydraulic damper cylinder body forging | |
CN107214283A (en) | The H profile steel manufacture mould of nuclear fusion stack magnet support | |
CN108220562B (en) | A kind of mould steel phase transformation heat treatment method |
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 |