CN1058757C - Method for nickel-base high-temp. alloy forging and bar acquiring uniform superfine crystalline grain - Google Patents

Method for nickel-base high-temp. alloy forging and bar acquiring uniform superfine crystalline grain Download PDF

Info

Publication number
CN1058757C
CN1058757C CN96115293A CN96115293A CN1058757C CN 1058757 C CN1058757 C CN 1058757C CN 96115293 A CN96115293 A CN 96115293A CN 96115293 A CN96115293 A CN 96115293A CN 1058757 C CN1058757 C CN 1058757C
Authority
CN
China
Prior art keywords
forging
blue
net
time
blank
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.)
Expired - Fee Related
Application number
CN96115293A
Other languages
Chinese (zh)
Other versions
CN1165204A (en
Inventor
陈宗霖
王少刚
姜兆群
刘秋生
陈桂梅
李伟红
刘润广
韩雪
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.)
LIMING ENGINE MANUFACTURE CO SHENYANG
Original Assignee
LIMING ENGINE MANUFACTURE CO SHENYANG
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 LIMING ENGINE MANUFACTURE CO SHENYANG filed Critical LIMING ENGINE MANUFACTURE CO SHENYANG
Priority to CN96115293A priority Critical patent/CN1058757C/en
Publication of CN1165204A publication Critical patent/CN1165204A/en
Application granted granted Critical
Publication of CN1058757C publication Critical patent/CN1058757C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Forging (AREA)

Abstract

The present invention relates to an even ultrafine grain obtaining method for GH4169 forged pieces and bars. The even ultrafine grain obtaining method is characterized in that an even reticular Widmanstatten delta-phase structure is obtained by pretreatment, and then a fresh fine-crystal nucleus surrounded by spherical delta-phases is obtained by deformation, the final state can be DA or have high quality and high strength, and the pretreatment, the deformation and the final molding can be carried out on common forging equipment. When the present invention is used for one item of grain refining, the physicochemical detection expense can be reduced by 24%; the present invention is suitable for directly producing fine-crystal bars of various specifications in aeronautical and astronautical engine plants, professional forge plants and steel plants.

Description

The method of a kind of nickel base superalloy forging and bar acquiring uniform superfine crystalline grain
The present invention relates to a kind of each forging of nickel base superalloy GH4169 alloy, as dish, impeller, ring, axle and blade; All kinds of bars, as forge rod, roll rod, the method for the above uniform superfine crystalline grain of ASTM10 level obtained.
As everyone knows, the GH4169 alloy is widely used in the key components and parts manufacturing in Aeronautics and Astronautics, Nuclear power plants and the petrochemical industry, such as the turbine disk on the gas-turbine engine, compressor disc, annular element, turboshaft and compressor blade or the like.And, then require the even refinement of grain fineness number of this alloy to reach more than the ASTM10 level in order to improve high and low all fatigue propertys of the above-mentioned strength member of internal combustion turbine.U.S. Pat 3660177 has proposed a kind of 1N718 alloy forged piece that adopts hot mechanical workout to produce to have even small grains and the method for bar.But, the ins and outs deficiency that this method discloses, especially forging temperature is lower, and the metallographic structure of separating out is short and thick needle-like Wei Shi body δ phase, thereby finish-forging is required relatively harsher.Adopt general thin brilliant technology, this alloy is at the uniform superfine crystalline grain that is difficult on the general forging equipment reach more than the ASTM10 level.
The object of the present invention is to provide a kind of at common forging equipment, on hammer, pressing machine, hydropress and common rolling mill, looping mill, just can make GH4169 superalloy forging or bar obtain the method for the easy handling of the above uniform superfine crystalline grain of ASTM10 level.
Technical solution of the present invention is after the blanking blank to be separated out the δ phase, by to the hot mechanical workout of blank, finally shaping and thermal treatment, makes alloy obtain uniform superfine crystalline grain.Be characterized in separating out the blue shape Wei Shi of uniform net body δ phase by following step: a. is at 1010 ℃--1030 ℃ of distortion of carrying out greater than 25% of giving, b. carry out blue processing of the net first time, processing parameter 880--900 ℃ of insulation 8--10h air cooling, c. jacket and forging or rolling after carry out that second time net is blue to be handled, processing parameter is handled with net is blue for the first time.In addition, net for the first time blue handle and jacket after, blank is out of shape greater than 30% forging or rolling at 1010 ℃-1030 ℃.Secondly, net is blue for the second time handle after, blank is out of shape finish-forging or the finish to gauge greater than 25% on common forging equipment, processing parameter is got 980 ℃-1010 ℃ and look the blank size and specific requirement employing air cooling, oil cooling or water-cooled.At last, 720 ℃ of-620 ℃ of direct aging or 970 ℃ of 1h solid solutions, then 720 ℃ of-620 ℃ of ageing treatment.Like this, can obtain the forging and the bar of the above uniform superfine crystalline grain of the high-strength state of DA state (the former) or high-quality (latter) ASTM10 level.Certainly when the blank grain size is relatively more even, in the step of separating out the δ phase, can not carry out predeformation, promptly directly carry out blue processing of the net first time after the blanking.When the grain size of the blue processing of net first time back blank compares uniform tissue, in the step of separating out the δ phase, can not carry out directly carrying out finish-forging or finish to gauge after the blue processing of the net second time is jacket.In addition, when ausforming equipment was adopted in final shaping, blank carried out needn't can carrying out finish-forging or finish to gauge by jacket after blue processing of the net first time.
See embodiment below in conjunction with accompanying drawing.
Accompanying drawing 1 is a process flow sheet of the present invention.Wherein, by the blanking operation to forging or rollingly being called pre-treatment for the first time, to finish-forging or finish to gauge, be called pre-treatment for the second time, the two adds can unite together and is referred to as pre-treatment, its objective is and obtain the blue shape Wei Shi of more equally distributed net body δ phase constitution structure earlier, be out of shape being lower than under the δ phased soln temperature then, it is broken mutually to net blue shape Wei Shi body δ, obtain spherical δ phase constitution, surround new net orchid mutually by spherical δ, form new close grain circumference, make in heat treatment process subsequently that thin crystalline substance is further perfect, crystal grain is further even.Accompanying drawing 2 is the metallographic structure figure after a kind of embodiment blanking.Its chemical ingredients sees Table one, and wherein, alloy is non-timeliness state, and chemical ingredients is not strict with, and does not have obvious niobium segregation, and grain fineness number is the ASTM5-7 level, is that typical crystal grain skewness example is a chain.Institute's material down press the processing of figure one flow process, and net is blue for the first time obtains the blue shape Wei Shi of more equally distributed net body δ phase (seeing accompanying drawing 3) after handling, and forging or rolling behind the sticking and 1Cr18Ni9Ti plate jacket obtains spherical δ phase constitution (seeing accompanying drawing 4) with aluminum silicate fiber.At last, mould is through just direct finish-forging on ordinary press of preheating.In heat treatment step, DA has obtained uniform superfine crystalline grain tissue (seeing accompanying drawing 5) and δ phase constitution structure (seeing accompanying drawing 6) after handling; After handling, solid solution aging obtained uniform superfine crystalline grain tissue (seeing accompanying drawing 7) and δ phase constitution structure (seeing accompanying drawing 8).Accompanying drawing 9 is the situation of another kind of embodiment, i.e. the metallograph that grain structure is evenly distributed after the blanking.Its Chemical Composition sees Table 2, alloy state wherein, and grain size numbers etc. are all identical with last example.At this moment, not carrying out predeformation handles and directly enters the blue treatment process of net and can obtain the blue shape Wei Shi of equally distributed as shown in Figure 3 net body δ phase.Press Fig. 1 flow process and continue processing, finally still can obtain uniform superfine crystalline grain as accompanying drawing 5 and accompanying drawing 7.
The invention has the advantages that it is that pre-treatment or final shaping all were not limited to conventional extruding and known extrusion ratio 4: 1, but can select to forge according to the product processing requirement, forming technology such as rolling or extruding.Simultaneously, select easy handling, cheap sheathing process, proposed a pre-treatment and twice pretreatment technology more flexibly, can on common hammer, pressing machine, hydropress, milling train and looping mill, be shaped.At last, can obtain under direct aging and the solid solution aging two states equally distributed ultrafine-grained (UFG) microstructure more than the ASTM10 level through thermal treatment.It should be the blue shape Wei Shi of equally distributed net body δ phase that the present invention has disclosed the middle blank tissue that obtains superfine crystal particle.In addition, without pretreated blank, though utilize the isothermal extruding also to can not get uniform superfine crystalline grain, and after pre-treatment, utilize common forging and pressing all can obtain the illustration of uniform superfine crystalline grain in the foregoing description, show that pre-treatment of the present invention is the prerequisite that GH4169 forging, bar obtain superfine grained structure.In a word,,, adopt the present invention, alloy property is stablized, improved quality product significantly, improved the tired and anti-ability that ruptures of high and low week than common thin brilliant technology because alloy recrystallization is abundant owing to separate out the blue shape Wei Shi body δ phase of net.And because homogeneous microstructure can significantly reduce the production testing project, only this item can increase economic efficiency 24%.The present invention promptly can be used for common forging, can be used for again that isothermal is super moulds forging, workable, be not only applicable to each Aeronautics and Astronautics engine works, professional forge works, and can extend to steel mill, direct production all size high-quality thin brilliant GH4169 forging and bar.The present invention is simple and easy, reasonable, practical, is suitable for China's enterprise present situation, has very considerable economic and promotional value.
Table 1
C S P Si Fe Cr Ni Mo Ti Al B Nb
0.02 <0.015 <0.015 <0.35 Surplus 17.00 50.00 2.80 0.75 0.70 <0.006 5.00
Table 2
C S P Si Fe Cr Ni Mo Ti Al B Nb
0.04 <0.002 <0.015 <0.14 Surplus 18.77 52.31 2.92 1.01 0.61 <0.006 5.09

Claims (5)

1, a kind of nickel base superalloy GH4169 forging and bar obtain the method for the above uniform superfine crystalline grain of ASTM10 level, and wherein alloying constituent does not have more than obvious niobium segregation, the grain fineness number ASTM4 level and is non-timeliness state, it by
---after the blanking blank separated out the δ phase
---blank is carried out hot mechanical workout
---the final shaping
---thermal treatment is formed, and it is characterized in that:
---separate out the blue shape Wei Shi of uniform net body δ phase by following step:
A. at 1010 ℃--1030 ℃ of distortion of carrying out greater than 25% of giving:
B. carry out the blue processing of the net first time, 880 ℃ of processing parameters--900 ℃, insulation 8~10h air cooling;
C. jacket and forging or rolling after carry out that second time net is blue to be handled, processing parameter is handled with net is blue for the first time;
---for the first time net blue handle and jacket after, blank is out of shape greater than 30% forging or rolling at 1010 ℃~1030 ℃;
---for the second time net is blue handle after, blank is out of shape finish-forging or the finish to gauge greater than 25% on common forging equipment, processing parameter is got 980 ℃~1010 ℃ and look the blank size and air cooling, oil cooling or water-cooled are adopted in specific requirement;
---thermal treatment can be adopted 720 ℃ then of 720 ℃~620 ℃ direct aging or 970 ℃ of 1h solid solutions--620 ℃ of ageing treatment:
2, nickel base superalloy GH4169 forging according to claim 1, bar obtain the method for the above uniform superfine crystalline grain of ASTM10 level, it is characterized in that: when the grain size of blank relatively evenly the time, in the step of separating out the δ phase, can not give distortion, promptly directly carry out blue processing of the net first time after the blanking.
3, nickel base superalloy GH4169 forging according to claim 1 and 2, bar obtain the method for the above uniform superfine crystalline grain of ASTM10 level, it is characterized in that: when the grain size of blank is relatively more even after netting blue processing the first time, in the step of separating out the δ phase, can carry out netting the second time and directly carry out finish-forging or finish to gauge after blue processing is jacket.
4, nickel base superalloy GH4169 forging according to claim 1 and 2, bar obtain the method for the above uniform superfine crystalline grain of ASTM10 level, it is characterized in that: when ausforming equipment was adopted in final shaping, blank carried out needn't can carrying out finish-forging or finish to gauge by jacket after blue processing of the net first time.
5, nickel base superalloy GH4169 forging according to claim 3, bar obtain the method for the above uniform superfine crystalline grain of ASTM10 level, it is characterized in that: when ausforming equipment is adopted in final shaping, blank carries out first time and needn't can carry out finish-forging or finish to gauge by jacket after the processing of net orchid.
CN96115293A 1996-05-09 1996-05-09 Method for nickel-base high-temp. alloy forging and bar acquiring uniform superfine crystalline grain Expired - Fee Related CN1058757C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN96115293A CN1058757C (en) 1996-05-09 1996-05-09 Method for nickel-base high-temp. alloy forging and bar acquiring uniform superfine crystalline grain

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN96115293A CN1058757C (en) 1996-05-09 1996-05-09 Method for nickel-base high-temp. alloy forging and bar acquiring uniform superfine crystalline grain

Publications (2)

Publication Number Publication Date
CN1165204A CN1165204A (en) 1997-11-19
CN1058757C true CN1058757C (en) 2000-11-22

Family

ID=5122568

Family Applications (1)

Application Number Title Priority Date Filing Date
CN96115293A Expired - Fee Related CN1058757C (en) 1996-05-09 1996-05-09 Method for nickel-base high-temp. alloy forging and bar acquiring uniform superfine crystalline grain

Country Status (1)

Country Link
CN (1) CN1058757C (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100351403C (en) * 2005-01-12 2007-11-28 山东泰山钢铁有限公司 Prevention method for deformed high-temperature alloy low-power coarse grains
CN100500881C (en) * 2007-03-05 2009-06-17 贵州安大航空锻造有限责任公司 Method for preparing fine-grain ring blank for GH4169 alloy near-isothermal forging
CN101412066B (en) * 2007-10-17 2012-10-03 沈阳黎明航空发动机(集团)有限责任公司 Hammer forging technique of GH4169 alloy dish
CN102126121B (en) * 2010-12-08 2013-02-27 扬州诚德重工有限公司 New process combining forging and rolling
CN102312118B (en) * 2011-09-21 2013-04-03 北京科技大学 Hot-working method for GH864 Waspaloy with accurately controlled structure
CN102357633B (en) * 2011-09-27 2013-11-06 上海宏钢电站设备铸锻有限公司 Method for manufacturing nickel-based high-temperature alloy forge piece
CN105583251B (en) * 2014-10-24 2017-11-10 中国科学院金属研究所 A kind of forging method of big specification Inconel690 alloy bar materials
CN104801645B (en) * 2015-05-12 2017-01-25 无锡派克新材料科技股份有限公司 Forging method for high-temperature alloy GH3617M forged pieces
CN104947014B (en) * 2015-07-10 2017-01-25 中南大学 Cyclic loading and unloading deformation refinement GH 4169 alloy forge piece grain organization method
CN105170865B (en) * 2015-10-09 2017-06-13 大连理工大学 A kind of crystal grain control method of explosive valve GH690 alloys shearing lid
CN106541069B (en) * 2016-12-07 2018-11-16 陕西宏远航空锻造有限责任公司 A kind of Integral die-forged method of large size GH4169 turbine wheel shaft
CN106734795A (en) * 2016-12-14 2017-05-31 西部超导材料科技股份有限公司 A kind of preparation method of niobium GH4169 alloy bar materials high
CN106929652B (en) * 2017-02-15 2018-07-24 贵州大学 Heat treatment method is precipitated to connecting bolt second-phase dispersion in a kind of GH4169
CN107377841A (en) * 2017-09-14 2017-11-24 上海怀德机电有限公司 A kind of forging method of GH4169 alloys Ultra-fine Grained forging
CN109457201A (en) * 2018-11-14 2019-03-12 中南大学 A method of refinement nickel-base alloy forging crystal grain simultaneously improves structural homogenity
CN110592505B (en) * 2019-09-12 2020-10-20 中国航发北京航空材料研究院 Solution treatment method for accurately controlling structural properties of GH720Li alloy
CN111575620B (en) * 2020-07-01 2021-11-16 中南大学 Method for obtaining GH4169 alloy superfine crystal forging
CN112680679B (en) * 2020-11-25 2021-12-17 河南航天精工制造有限公司 Heat treatment method of GH4169 alloy for pull rod

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3660177A (en) * 1970-05-18 1972-05-02 United Aircraft Corp Processing of nickel-base alloys for improved fatigue properties
JPS59229474A (en) * 1983-06-08 1984-12-22 Hitachi Metals Ltd Method for controlling grain of precipitation strengthening ni alloy
WO1994013849A1 (en) * 1992-12-14 1994-06-23 United Technologies Corporation Superalloy forging process and related composition

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3660177A (en) * 1970-05-18 1972-05-02 United Aircraft Corp Processing of nickel-base alloys for improved fatigue properties
JPS59229474A (en) * 1983-06-08 1984-12-22 Hitachi Metals Ltd Method for controlling grain of precipitation strengthening ni alloy
WO1994013849A1 (en) * 1992-12-14 1994-06-23 United Technologies Corporation Superalloy forging process and related composition

Also Published As

Publication number Publication date
CN1165204A (en) 1997-11-19

Similar Documents

Publication Publication Date Title
CN1058757C (en) Method for nickel-base high-temp. alloy forging and bar acquiring uniform superfine crystalline grain
CN102492906B (en) Forging method of high-temperature alloy fine-grained bars
CN1329139C (en) Constant-temp. forging in the air for nickel-base super heat-resistant alloy
CN111906225B (en) Forging method of oversized Ti80 titanium alloy forging stock
CN107999687A (en) A kind of aluminium alloy vane forging and preparation method thereof
WO2008106858A1 (en) A quasi-isothermal forging method of a disk shaped forging of nickel-base superalloys in air
CN102560295B (en) Thermal processing method for improving aluminum alloy stamping forming
CN105088118A (en) Grain ultra-fining method for nickel-based superalloy board
CN109500330A (en) A kind of cogging method of the big size ingot-casting of nickel-base alloy
CN109622837B (en) Preparation method and device of TC11 titanium alloy cake blank with high flaw detection level
CN103302214A (en) Difficultly-deformed nickel-based superalloy superplastic forming method
CN105177478A (en) Cogging method for large GH4738 high-temperature alloy ingot
CN104175068A (en) Method for forging special-shaped alloy ring used for aviation
CN103341580A (en) Free forging method for medium-pressure combined regulation valve stem workblank of supercritical turbine
CN112589022A (en) Method for manufacturing high-quality low-segregation fine-grain high-temperature alloy bar difficult to deform
CN112264565A (en) Manufacturing method of high-performance aluminum alloy cylindrical forging for spaceflight
CN109079067A (en) High-strength aluminum alloy ring parts rolling forming method
CN114160746A (en) Preparation method of titanium alloy cake with high flaw detection level TC25/TC25G
CN114178454A (en) Preparation method of magnesium-lithium alloy hollow component with complex section
CN111659894B (en) Preparation method of powder high-temperature alloy bar and disc
CN111659846A (en) Forging method for homogenizing GH141 special-shaped ring forging grains
CN1233483C (en) Constant temperature toughness rolling method for GH4049 alloy
CN109570432A (en) A kind of aluminum alloy forging ring manufacturing method based on punching shearing die
CN115722628A (en) Preparation method of high-alloying difficult-deformation high-temperature alloy GH4151 disc forging
CN110756613B (en) Preparation method of small-ingot-shaped GH3128 alloy bar

Legal Events

Date Code Title Description
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C06 Publication
PB01 Publication
C14 Grant of patent or utility model
GR01 Patent grant
C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee