CN111215567A - Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring - Google Patents

Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring Download PDF

Info

Publication number
CN111215567A
CN111215567A CN201911241067.3A CN201911241067A CN111215567A CN 111215567 A CN111215567 A CN 111215567A CN 201911241067 A CN201911241067 A CN 201911241067A CN 111215567 A CN111215567 A CN 111215567A
Authority
CN
China
Prior art keywords
ring
forging
rolling
temperature
piece
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
CN201911241067.3A
Other languages
Chinese (zh)
Inventor
武茜宝
姚彦军
邹龙龙
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
Original Assignee
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 CN201911241067.3A priority Critical patent/CN111215567A/en
Publication of CN111215567A publication Critical patent/CN111215567A/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
    • B21J5/002Hybrid process, e.g. forging following casting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J1/00Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
    • B21J1/06Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00Making machine elements
    • B21K1/76Making machine elements elements not mentioned in one of the preceding groups
    • B21K1/761Making machine elements elements not mentioned in one of the preceding groups rings

Abstract

The invention relates to a forging method for improving the grain size of a GH4099 high-temperature alloy thin-wall ring piece, which is characterized by comprising the following steps: the method comprises the steps of primary ring blank forming, ring rolling forming and heat treatment, wherein the ring rolling forming step comprises the following steps: heating the primary ring blank in an electric furnace to a forging temperature of 1080-1110 ℃, putting the primary ring blank on a ring rolling mill for rolling and forming, wherein end rolling equipment is adopted in the rolling process, and the deformation of the primary ring blank is 27-42%, so that the ring forging is obtained. The end rolling equipment is characterized in that conical roller equipment is added in the reaming process to control the increase of the height direction size of the ring piece, so that the height direction size of the ring piece is within the tolerance range of the forge piece. According to the rolling forming method of the GH4099 high-temperature alloy thin-wall type ring forging, the high-temperature alloy ring forging with excellent thin-wall type structure performance can be obtained by controlling the forging heating temperature, the forging starting temperature, the finish forging temperature and the forging deformation.

Description

Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring
Technical Field
The invention belongs to the technical field of forging, and relates to a forging method for improving the grain size of a GH4099 high-temperature alloy material.
Background
GH4099 is a high-alloying nickel-based aging plate alloy, which is comprehensively strengthened by cobalt, tungsten, molybdenum, aluminum and titanium elements, so that the alloy has higher heat strength, can be used for a long time below 900 ℃, and has the maximum working temperature of 1000 ℃. The alloy has stable structure and satisfactory cold and hot processing forming and welding process performance, thereby being widely applied to large plate structural members.
GH4099 can be used as it is without aging treatment after solution treatment. The heating of the forging and the control of the forming process are difficult points of the forging of the material, and have important influence on the internal structure and the performance. The grain size of the forging piece also influences the welding performance of the material, so that the grain size level of the forging piece is controlled, and the tendency of generating cracks on the surface of the material in the welding process can be effectively reduced.
The GH4099 high-temperature alloy is heated to 1140 ℃ by a natural gas furnace, a prefabricated blank is produced by a free forging hammer, after the surface quality of a forged piece is checked by cooling, the prefabricated blank is heated to 1140 ℃ and then is rolled on a ring rolling machine to obtain a ring product, the physical and chemical properties are checked, the data is in a standard range, but the margin is not large, the grain size of the forged piece is checked, and the result is 2-3 grade, the grain structure is large, and the performance of the forged piece is influenced to a certain extent. The microstructure of the forging is sensitive to the influence of temperature, and the uniformity of the microstructure can also be realized by controlling the heating temperature and the heat preservation time of forging and increasing the deformation of forging.
Reducing the forging heating temperature can effectively reduce the growth rate of the internal structure of the blank in the heating and heat preservation process, but the reduction of the temperature can increase the tendency of forging cracks, and under the condition of ensuring less damage, the grain size level after forging can reach more than 4.5 grade by reducing the forging temperature. Therefore, the key problem of forging the GH4099 superalloy ring-rolled forgings is to accurately control the forging temperature and process and obtain the expected structure.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: the deformation performance of the GH4099 high-temperature alloy material is improved under the action of multidirectional compressive stress, forging cracks of the forging caused by low temperature and multidirectional stress are avoided, and the hole expanding method with stable and uniform forging structure is obtained. The stable physical and chemical performance is obtained, and the structure reliability of the GH4099 superalloy component is improved.
The technical scheme adopted by the invention is a forging method for improving the grain size of a GH4099 high-temperature alloy thin-wall ring piece, which comprises the following steps:
1. one-step ring blank forming
Heating a specification blanking GH4099 bar to a forging temperature of 1100-1140 ℃, upsetting, punching, machining an inner hole on a free forging hammer to remove inner hole burrs and defects, and expanding the size of the inner hole on a prefabricated blank on a horse device through the free forging hammer to obtain a primary ring blank;
2. ring rolling and expanding forming
Heating the primary ring blank in an electric furnace to a forging temperature of 1080-1110 ℃, then putting the primary ring blank on a ring rolling mill for rolling and forming, wherein an end rolling technology is adopted in the rolling process, the deformation is 27% -42%, and a ring forging is obtained. The end rolling technology is characterized in that a conical roller is added in the reaming process to control the increase of the height direction size of the ring piece, so that the height direction size of the ring piece is within the allowable tolerance range of a forged piece.
3. Thermal treatment
And (3) carrying out solution heat treatment on the GH4099 ring forging, wherein the solution treatment is to heat the GH4099 ring forging to 1080-1100 ℃, water-cool the GH4099 ring forging for 30 minutes, fish out the GH4099 ring forging, and air-cool the GH4099 ring forging to room temperature.
Further, in the step 1, a 3t free forging hammer is used for producing 20 Kg-60 Kg of blank, and the process is completed by 2-4 fires.
Further, in step 2, thermocouple strip temperature measurement is adopted for furnace temperature control, and feedback control is performed.
Further, in steps 1 and 2, the equipment, the tool and the used tool are preheated to 200-300 ℃.
Further, in the step 2, a forged piece with the final wall thickness of the ring piece of 20-40 mm can be formed, and the height dimension of the ring piece is controlled within the tolerance range required by the forged piece by applying an end rolling technology.
The invention has the beneficial effects that: according to the rolling forming method of the GH4099 high-temperature alloy thin-wall type ring forging, the high-temperature alloy ring forging with excellent thin-wall type structure performance can be obtained by controlling the forging heating temperature, the forging starting temperature, the finish forging temperature and the forging deformation.
Detailed Description
The main chemical element contents (weight percentage) of the GH4099 superalloy are as follows: content of C: less than or equal to 0.08, Cr content: 17% -20%, Co content: 5% -8%, W content: 5-7%, Mo content: 3.5% -4.5%, Al content: 1.7-2.4%, Ti content: 1.0% -1.5%, Fe content: less than or equal to 2 percent, Mn content: less than or equal to 0.4 percent, Si content: less than or equal to 0.5 percent, P content: less than or equal to 0.015 percent, and the balance: ni
Heating a specification blanking GH4099 bar to a forging temperature of 1100-1140 ℃, putting the bar on a hammer anvil of a 3t free forging hammer, upsetting, punching, mechanically turning an inner hole to remove inner hole burrs and defects, and expanding the size of the inner hole on a pre-forming blank on a horse device through a free forging hammer to obtain a primary ring blank; and heating the primary ring blank in an electric furnace to a forging temperature of 1080-1110 ℃, putting the primary ring blank on a ring rolling mill for rolling and forming, wherein an end rolling technology is adopted in the rolling process, and the deformation amount is 27% -42%, so that the ring forging is obtained. The end rolling equipment is characterized in that a conical roller is added in the reaming process to control the increase of the height direction size of the ring piece, so that the height direction size of the ring piece is within the allowable tolerance range of the forged piece. And (3) carrying out solution heat treatment on the GH4099 ring forging, wherein the solution treatment is to heat the GH4099 ring forging to 1080-1100 ℃, water-cool the GH4099 ring forging for 30 minutes, fish out the GH4099 ring forging, and air-cool the GH4099 ring forging to room temperature.
Through visual inspection, the surface of the GH4099 ring forging is smooth and has visual microcracks, and the GH4099 ring forging can be removed after being polished by a wind grinding wheel, so that the dimension meets the requirement; through detection, the room-temperature mechanical property, the high-temperature tensile property, the durability and the hardness of the GH4099 ring forging completely meet the requirements; through detection, the macrostructure of the GH4099 ring forging is uniform; and the grain size of the GH4099 ring forging is detected to be 5 grade.

Claims (8)

1. The forging method for improving the grain size of the GH4099 high-temperature alloy thin-wall ring is characterized by comprising the following steps of: the method comprises the steps of primary ring blank forming, ring rolling forming and heat treatment, wherein the ring rolling forming step comprises the following steps: heating the primary ring blank in an electric furnace to a forging temperature of 1080-1110 ℃, putting the primary ring blank on a ring rolling mill for rolling and forming, wherein end rolling equipment is adopted in the rolling process, and the deformation of the end rolling equipment is 27-42%, so that a ring forging is obtained; the end rolling equipment is characterized in that a conical roller is added in the reaming process to control the increase of the height direction size of the ring piece, so that the height direction size of the ring piece is within the allowable tolerance range of the forged piece.
2. The forging method as recited in claim 1, wherein the heat treatment step is: and carrying out solution heat treatment on the GH4099 ring forging.
3. The heat treatment method of claim 2, wherein the solution heat treatment is to heat the GH4099 ring forging to 1080-1100 ℃, water cool for 30 minutes, fish out, air cool to room temperature.
4. The forging method as recited in claim 1, wherein the primary ring blank forming step is: the method comprises the steps of heating a specification blanking GH4099 bar to a forging temperature of 1100-1140 ℃, upsetting, punching, machining an inner hole on a free forging hammer to remove inner hole burrs and defects, and expanding the size of the inner hole on a prefabricated blank on a horse device through the free forging hammer to obtain a primary ring blank.
5. The forging method as recited in claim 4, wherein: in the primary ring blank forming step, 20 Kg-60 Kg of GH4099 blank is forged by a 3t free forging hammer over 2-4 fires.
6. The forging method as recited in claim 1, wherein: in the step of forming the ring rolled piece, the furnace temperature is controlled by adopting thermocouple strip material for temperature measurement, and feedback control is carried out.
7. The forging method as recited in claim 1, wherein: the method as claimed in claim 1, wherein the equipment, the tool and the tools are preheated to 200-300 ℃ in the steps of one-time ring blank forming and ring rolling forming.
8. The method of claim 1, wherein: in the step of ring rolling and expanding, a forged piece with the final wall thickness of the ring piece of 20-40 mm can be formed, and meanwhile, the height dimension of the ring piece is controlled within the tolerance range required by the forged piece by using end rolling equipment.
CN201911241067.3A 2019-12-06 2019-12-06 Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring Pending CN111215567A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911241067.3A CN111215567A (en) 2019-12-06 2019-12-06 Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911241067.3A CN111215567A (en) 2019-12-06 2019-12-06 Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring

Publications (1)

Publication Number Publication Date
CN111215567A true CN111215567A (en) 2020-06-02

Family

ID=70829095

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911241067.3A Pending CN111215567A (en) 2019-12-06 2019-12-06 Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring

Country Status (1)

Country Link
CN (1) CN111215567A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111604448A (en) * 2020-06-05 2020-09-01 重庆钢铁研究所有限公司 Forging method of high-temperature alloy GH4099
CN112122543A (en) * 2020-09-03 2020-12-25 豪梅特航空机件(苏州)有限公司 Forging method for refining crystal grains of In783 alloy thick-wall ring forging
CN112122542A (en) * 2020-09-02 2020-12-25 豪梅特航空机件(苏州)有限公司 Forging method for improving local coarse grains of In 783-based ring forging
CN112296245A (en) * 2020-09-17 2021-02-02 豪梅特航空机件(苏州)有限公司 Forging method for improving creep property of Wasp ring forging
CN114160722A (en) * 2021-12-15 2022-03-11 陕西宏远航空锻造有限责任公司 Method for forming high-temperature alloy forging internal structure influence of hot material system on forging
CN114289676A (en) * 2021-12-15 2022-04-08 陕西宏远航空锻造有限责任公司 Flaw detection horizontal forging method for improving high-temperature alloy free forging
CN114507832A (en) * 2022-02-17 2022-05-17 无锡派克新材料科技股份有限公司 Fine grain strengthening method for GH99 alloy for aerospace

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102085556A (en) * 2010-12-10 2011-06-08 贵州航宇科技发展有限公司 Roll forming method of GH4033 high-temperature alloy thin-wall ring piece
CN104191166A (en) * 2014-08-04 2014-12-10 贵州航宇科技发展股份有限公司 Rolling forming method of aluminum alloy high-tube thin-wall rings
CN105081678A (en) * 2014-05-13 2015-11-25 陕西宏远航空锻造有限责任公司 Rolling forming method for nickel-base superalloy high-cylindrical ring piece
CN106552894A (en) * 2016-12-01 2017-04-05 贵州安大航空锻造有限责任公司 The enclosed hole-punching method of the high cylinder ring of GH99 alloys

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102085556A (en) * 2010-12-10 2011-06-08 贵州航宇科技发展有限公司 Roll forming method of GH4033 high-temperature alloy thin-wall ring piece
CN105081678A (en) * 2014-05-13 2015-11-25 陕西宏远航空锻造有限责任公司 Rolling forming method for nickel-base superalloy high-cylindrical ring piece
CN104191166A (en) * 2014-08-04 2014-12-10 贵州航宇科技发展股份有限公司 Rolling forming method of aluminum alloy high-tube thin-wall rings
CN106552894A (en) * 2016-12-01 2017-04-05 贵州安大航空锻造有限责任公司 The enclosed hole-punching method of the high cylinder ring of GH99 alloys

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
《中国航空材料手册》编辑委员会: "《中国航空材料手册 第2卷 变形高温合金 铸造高温合金》", 31 May 2002, 北京:中国标准出版社 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111604448A (en) * 2020-06-05 2020-09-01 重庆钢铁研究所有限公司 Forging method of high-temperature alloy GH4099
CN112122542A (en) * 2020-09-02 2020-12-25 豪梅特航空机件(苏州)有限公司 Forging method for improving local coarse grains of In 783-based ring forging
CN112122543A (en) * 2020-09-03 2020-12-25 豪梅特航空机件(苏州)有限公司 Forging method for refining crystal grains of In783 alloy thick-wall ring forging
CN112296245A (en) * 2020-09-17 2021-02-02 豪梅特航空机件(苏州)有限公司 Forging method for improving creep property of Wasp ring forging
CN114160722A (en) * 2021-12-15 2022-03-11 陕西宏远航空锻造有限责任公司 Method for forming high-temperature alloy forging internal structure influence of hot material system on forging
CN114289676A (en) * 2021-12-15 2022-04-08 陕西宏远航空锻造有限责任公司 Flaw detection horizontal forging method for improving high-temperature alloy free forging
CN114507832A (en) * 2022-02-17 2022-05-17 无锡派克新材料科技股份有限公司 Fine grain strengthening method for GH99 alloy for aerospace

Similar Documents

Publication Publication Date Title
CN111215567A (en) Forging method for improving grain size of GH4099 high-temperature alloy thin-wall ring
CN108246948B (en) Forging method for improving GH901 die forging structure
CN106623743B (en) A kind of GH4738 alloy die forgings and preparation method thereof
CN104907470A (en) 13Cr9Mo2Co1NiVNbNB steel forged piece manufacturing method
CN105689613A (en) Special forging method suitable for super duplex stainless steel bars
CN108555223B (en) A kind of GH901 alloy diskware manufacturing method
CN110614338B (en) Forging method of GH4169 alloy steel round bar
CN107345290B (en) A kind of manufacturing method of TC4 titanium alloy thin wall ring
CN112846015B (en) GH536 high-temperature alloy annular forging forming method
CN103774061A (en) Blade ring forged piece and fabrication technology thereof
CN107695266A (en) Steam turbine high temperature resistant forging and its forging method
CN112718910A (en) Manufacturing method of large-caliber TC4 titanium alloy thick-wall pipe
CN106906340A (en) A kind of fine grain heat treatment method
CN107866660A (en) A kind of die steel processing technology
CN109396759B (en) Forging-rolling combined manufacturing method for 980 steel large-diameter cylinder for deep submergence
JP5284555B2 (en) Manufacturing method of large forgings
CN112536406B (en) Forging drawing method for avoiding surface cracking
CN113084061A (en) Nickel-based superalloy GH3536 die forging and forming method thereof
CN108642410A (en) A kind of process improving aluminum alloy plate materials comprehensive mechanical property
CN111451425A (en) Forging method for controlling white point defect
CN112496037B (en) Nickel-based alloy plate rolling method
CN106048455B (en) A kind of processing method of mold materials for high intensity forging
CN109967672B (en) Forging method of CuAl10Fe5Ni5 copper alloy
CN106424497B (en) A kind of forging method and forging of Cr18Mn18N steel forge piece
CN105256242A (en) Manufacturing method for forge piece blanks for marine oil exploitation equipment

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
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20200602