CN101791668B - Roll forming method of large and medium aluminum alloy solid disk forging - Google Patents

Roll forming method of large and medium aluminum alloy solid disk forging Download PDF

Info

Publication number
CN101791668B
CN101791668B CN2010101276326A CN201010127632A CN101791668B CN 101791668 B CN101791668 B CN 101791668B CN 2010101276326 A CN2010101276326 A CN 2010101276326A CN 201010127632 A CN201010127632 A CN 201010127632A CN 101791668 B CN101791668 B CN 101791668B
Authority
CN
China
Prior art keywords
solid disk
rolling
speed
aluminum alloy
forging
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
CN2010101276326A
Other languages
Chinese (zh)
Other versions
CN101791668A (en
Inventor
邹伟
叶俊青
崔一平
杨国平
邹善垚
莫尔云
刘成
何涛
吴昊
斯庆阳
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.)
AVIC Guizhou Anda Aviation Forging Co Ltd
Original Assignee
Guizhou Anda 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 Guizhou Anda Aviation Forging Co Ltd filed Critical Guizhou Anda Aviation Forging Co Ltd
Priority to CN2010101276326A priority Critical patent/CN101791668B/en
Publication of CN101791668A publication Critical patent/CN101791668A/en
Application granted granted Critical
Publication of CN101791668B publication Critical patent/CN101791668B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Forging (AREA)
  • Metal Rolling (AREA)

Abstract

The invention discloses a roll forming method of a large and medium aluminum alloy solid disk forging, which comprises the following steps of: firstly upsetting aluminum alloy bar materials, profiling into a solid disk blank; and rolling the disk blank in a rolling machine; when rolling within 20s, expanding the disk blank at a speed of 9-12mm/s under a 4000-4900KN axial rolling force with an axial feed speed of 1.9mm/s; when rolling in the time range of 20-40s, expanding the disk blank at a speed of 8-10mm/s under a 3000-3500KN axial rolling force with an axial feed speed of 0.9mm/s; and when rolling within the time range of 40-70s, expanding the disk blank at a speed of 5-8mm/s under a 2500-3000KN axial rolling force with an axial feed speed of 0.5mm/s; and finally rolling into the solid disk forging one one-grade fire. The method is mainly used for rolling the disk forging with excellent shape, dimension, organization and performance.

Description

The roll-forming method of big-and-middle-sized aluminum alloy solid disk forging
Technical field
The present invention relates to the roll-forming method of a kind of roll-forming method of forging, particularly big-and-middle-sized aluminum alloy solid disk forging.
Background technology
On June 13rd, 2007, disclosed Chinese invention patent specification CN1978125A disclosed a kind of roll-forming method of big-and-middle-sized solid disk forging, this method is metal bar material heating after jumping-up, die mould become solid disk, solid disk heating afterloading unit location, axially rolled one-tenth solid disk forging.This method has only solved the roll forming technical problem of big-and-middle-sized solid disk forging.When adopting the rolling big-and-middle-sized aluminum alloy solid disk forging of this method, when the epicone roller of elongator is made the rolling dish base of axial feed motion towards the dish base, if its feed speed is excessive, will cause coiling base temperature when rolling and raise, be easy to generate defectives such as overheated, burning and tissue variation; If its feed speed is too small, it is too fast that the dish base dispel the heat when rolling, cause rolling motionless, or increase rolling time and rolling number of times, reduce rolling efficiency, and can cause on the disk forge piece card and fill defectives such as discontented near the peripheral position of the ring wedge angle of outer ring surface.And when adopting the rolling disk forge piece of this method, need reach requirement through changeing the rolling shape and size of disk forge piece that just can make repeatedly more, so not only increase production cost, reduced productivity ratio, and rolling technology and the quality control increase difficulty of also can giving of repeated multiple times.
Summary of the invention
The technical problem to be solved in the present invention provides the roll-forming method that a kind of axial feed velocity that uses variation is realized big-and-middle-sized aluminum alloy solid disk forging, the variation that this method axial feed velocity when rolling is descending is also adjusted roll-force thereupon, makes the solid disk forging of roll forming possess excellent tissue and performance.
For solving the problems of the technologies described above, the roll-forming method of the big-and-middle-sized aluminum alloy solid disk forging of the present invention is realized by the following technical solutions:
Aluminium alloy bar by the specification blanking is heated to deformation temperature after jumping-up, die mould become aluminum alloy solid dish base, puts into the elongator location after more described solid disk being heated to deformation temperature;
Start elongator, handle its epicone roller and make axial feed motion with the speed of 1.9mm/s towards described solid disk direction, thus the epicone roller of described elongator and down the awl roller along described solid disk axially with rolling its card of the roll-force of 4000KN~4900KN and outside its radial level, move the axially rolled of realization dish base; Described solid disk is with the speed broadening of 9mm/s~12mm/s;
When the operation of rolling proceeds to 20s, the feed speed of adjusting described epicone roller makes its rolling solid disk of speed axial feed with 0.9mm/s, the axial rolling force that described solid disk is subjected to upper and lower awl roller at this moment is 3000KN~3500KN, described solid disk under the effect of axial rolling force with the speed broadening of 8mm/s~10mm/s;
When the operation of rolling proceeds to 40s, the feed speed of adjusting described epicone roller makes the rolling described solid disk of its speed axial feed with 0.5mm/s, at this moment, the roll-force that described solid disk is subjected to upper and lower awl roller is 2500KN~3000KN, described solid disk is with the speed broadening of 5mm/s~8mm/s, finish when the operation of rolling proceeds to 70s, heating once and rolling becomes aluminum alloy solid disk forging.
Described aluminum alloy solid disk forging rolls after quench and adds the artificial aging processing; Described quenching be described solid disk forging be heated to 460 ℃~490 ℃ the insulation 9h~12h after water-cooled; Described artificial aging be described solid disk forging be heated to 150 ℃~160 ℃ the insulation 20h~22h after air cooling.
Compared with prior art, beneficial effect of the present invention is as follows:
The present invention makes its speed broadening with 9mm/s~12mm/s with axial feed velocity axial rolling solid disk under the roll-force of 4000KN~4900KN of 1.9mm/s in the rolling 20s of beginning; In rolling 20s~40s, make its speed broadening with 8mm/s~10mm/s with axial feed velocity rolling solid disk under the axial rolling force of 3000KN~3500KN of 0.9mm/s; In rolling 40s~70s, make its speed broadening with 5mm/s~8mm/s with axial feed velocity rolling solid disk under the axial rolling force of 2500KN~3000KN of 0.5mm/s; Heating once and rolling is configured as solid disk forging.
Adopt such process route, can avoid coiling base temperature when rolling and raise, produce defectives such as overheated, burning and tissue variation; Can also avoid coiling base when rolling, dispel the heat too fast, cause rolling motionless, reduce rolling efficiency and on the disk forge piece card ring wedge angle periphery position near outer ring surface fill defectives such as discontented.And adopt this method to realize the heating once and rolling shaping, and reduced rolling time and rolling number of times, be easy to technology and quality are controlled, reduced production cost, improved productivity ratio.
The size and dimension of this aluminum alloy solid disk forging has reached the design drawing requirement after testing.
The aluminum alloy materials that with the trade mark is LC52 is an example:
The room temperature tensile performance of this aluminum alloy solid disk forging after testing: tangential tensile strength is 446MPa~451MPa (greater than the 410MPa of design instructions for use), high to tensile strength be 431MPa~445MPa (greater than the 400MPa of design instructions for use), horizontal tensile strength is 435MPa~439MPa (greater than the 400MPa of design instructions for use); Its percentage elongation is that 0.2% o'clock tangential yield strength is 381MPa~391MPa (greater than the 345MPa of design instructions for use), percentage elongation be 0.2% o'clock height to yield strength be 373MPa~381MPa, percentage elongation is that 0.2% o'clock horizontal yield strength is 378MPa~379MPa; Tangential elongation after fracture be 15%~16% (greater than the design instructions for use 9%), high to elongation after fracture be 11%~13% (greater than the design instructions for use 5%), horizontal elongation after fracture be 11%~12% (greater than the design instructions for use 5%); Brinell hardness is 140HB~143HB.
The specific embodiment
The aluminum alloy materials that with the trade mark is LC52 below is that example illustrates concrete processing step of the present invention:
Step 1: the aluminium alloy bar by the LC52 of specification blanking is heated to 450 ℃~470 ℃ deformation temperature after obtain aluminum alloy solid dish base behind the jumping-up, die mould;
Step 2: described solid disk is heated to puts into elongator and location after the above-mentioned deformation temperature;
Step 3: start elongator, handle its epicone roller and make axial feed motion with the speed of 1.9mm/s towards described solid disk direction, thus the epicone roller of described elongator and down the awl roller along described solid disk axially with rolling its card of the roll-force of 4000KN~4900KN and outside its radial level, move the axially rolled of realization dish base; Described solid disk is with the speed broadening of 9mm/s~12mm/s.
Step 4: when the operation of rolling proceeds to 20s, the feed speed of adjusting described epicone roller makes its rolling solid disk of speed axial feed with 0.9mm/s, the axial rolling force that described solid disk is subjected to upper and lower awl roller at this moment is 3000KN~3500KN, described solid disk under the effect of axial rolling force with the speed broadening of 8mm/s~10mm/s.
Step 5: when the operation of rolling proceeds to 40s, the feed speed of adjusting described epicone roller makes the rolling described solid disk of its speed axial feed with 0.5mm/s, at this moment, the roll-force that described solid disk is subjected to upper and lower awl roller is 2500KN~3000KN, described solid disk is with the speed broadening of 5mm/s~8mm/s, finish when the operation of rolling proceeds to 70s, heating once and rolling becomes aluminum alloy solid disk forging.
The finish-forging of the aluminum alloy materials of above-mentioned LC52 or finishing temperature are greater than 350 ℃.
Step 6: described aluminum alloy solid disk forging rolls after quench and adds the artificial aging processing; Described quenching be described solid disk forging be heated to 460 ℃~490 ℃ the insulation 9h~12h after water-cooled; Described artificial aging be described solid disk forging be heated to 150 ℃~160 ℃ the insulation 20h~22h after air cooling.
The size and dimension of this aluminum alloy solid disk forging has reached the design drawing requirement after testing.
After testing, the performance of this aluminum alloy solid disk forging is as follows:
The room temperature tensile performance: tangential tensile strength is 446MPa~451MPa, and is high to being that tensile strength is 431MPa~445MPa, laterally is that tensile strength is 435MPa~439MPa; Its percentage elongation is that 0.2% o'clock tangential yield strength is 381MPa~391MPa, percentage elongation be 0.2% o'clock height to yield strength be 373MPa~381MPa, percentage elongation is that 0.2% o'clock horizontal yield strength is 378MPa~379MPa; Tangential elongation after fracture is 15%~16%, high to elongation after fracture be 11%~13%, horizontal elongation after fracture is 11%~12%; Brinell hardness is 140HB~143HB.

Claims (3)

1. the roll-forming method of a big-and-middle-sized aluminum alloy solid disk forging, comprise being heated to deformation temperature after jumping-up, die mould become aluminum alloy solid dish base, put into the elongator localization step after more described solid disk being heated to deformation temperature by the aluminium alloy bar of specification blanking; It is characterized in that this method is further comprising the steps of:
Start elongator, handle its epicone roller and make axial feed motion with the speed of 1.9mm/s towards described solid disk direction, thus the epicone roller of described elongator and down the awl roller along described solid disk axially with rolling its card of the roll-force of 4000KN~4900KN and outside its radial level, move the axially rolled of realization dish base; Described solid disk is with the speed broadening of 9mm/s~12mm/s;
When the operation of rolling proceeds to 20s, the feed speed of adjusting described epicone roller makes its rolling solid disk of speed axial feed with 0.9mm/s, the axial rolling force that described solid disk is subjected to upper and lower awl roller at this moment is 3000KN~3500KN, described solid disk under the effect of axial rolling force with the speed broadening of 8mm/s~10mm/s;
When the operation of rolling proceeds to 40s, the feed speed of adjusting described epicone roller makes the rolling described solid disk of its speed axial feed with 0.5mm/s, at this moment, the roll-force that described solid disk is subjected to upper and lower awl roller is 2500KN~3000KN, described solid disk is with the speed broadening of 5mm/s~8mm/s, finish when the operation of rolling proceeds to 70s, heating once and rolling becomes aluminum alloy solid disk forging.
2. the roll-forming method of big-and-middle-sized aluminum alloy solid disk forging according to claim 1 is characterized in that: described aluminum alloy solid disk forging rolls after quench and add artificial aging and handle.
3. the roll-forming method of big-and-middle-sized aluminum alloy solid disk forging according to claim 2, it is characterized in that: described quenching is that described solid disk forging is heated to water-cooled behind 460 ℃~490 ℃ insulation 9h~12h, and described artificial aging is described solid disk forging to be heated to 150 ℃~160 ℃ be incubated air cooling behind 20h~22h.
CN2010101276326A 2010-03-19 2010-03-19 Roll forming method of large and medium aluminum alloy solid disk forging Expired - Fee Related CN101791668B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010101276326A CN101791668B (en) 2010-03-19 2010-03-19 Roll forming method of large and medium aluminum alloy solid disk forging

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010101276326A CN101791668B (en) 2010-03-19 2010-03-19 Roll forming method of large and medium aluminum alloy solid disk forging

Publications (2)

Publication Number Publication Date
CN101791668A CN101791668A (en) 2010-08-04
CN101791668B true CN101791668B (en) 2011-11-02

Family

ID=42584708

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010101276326A Expired - Fee Related CN101791668B (en) 2010-03-19 2010-03-19 Roll forming method of large and medium aluminum alloy solid disk forging

Country Status (1)

Country Link
CN (1) CN101791668B (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1978125A (en) * 2006-12-06 2007-06-13 贵州安大航空锻造有限责任公司 Rolling formation method for large and medium size solid plate-shape forge piece
CN101020284A (en) * 2007-03-05 2007-08-22 贵州安大航空锻造有限责任公司 Making process of large irregular ring blank of high temperature alloy

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60124427A (en) * 1983-12-08 1985-07-03 Agency Of Ind Science & Technol Controlling method of rolling mill
JPS62227540A (en) * 1986-03-29 1987-10-06 Sumitomo Metal Ind Ltd Rolling method for metal cylindrical member

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1978125A (en) * 2006-12-06 2007-06-13 贵州安大航空锻造有限责任公司 Rolling formation method for large and medium size solid plate-shape forge piece
CN101020284A (en) * 2007-03-05 2007-08-22 贵州安大航空锻造有限责任公司 Making process of large irregular ring blank of high temperature alloy

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
JP昭60-124427A 1985.07.03
JP昭62-227540A 1987.10.06

Also Published As

Publication number Publication date
CN101791668A (en) 2010-08-04

Similar Documents

Publication Publication Date Title
CN103465027B (en) The thin brilliant dish base manufacture method of a kind of GH4169 alloy
CN101439350B (en) Method for producing seamless steel pipe for producing gas cylinder with heavy caliber for hauled vehicle
CN106975719A (en) A kind of forging method of cogging
CN101767106B (en) Hot rolling process of stainless plate strip coil
CN101758150B (en) Rolling formation method of large and medium high-temperature alloy hollow disc-shaped forge piece
CN101758151B (en) Rolling formation method of large and medium titanium alloy solid disc-shaped forge piece
CN101773972A (en) Pre-forming technology of high-strength aluminum alloy stock
CN104762460B (en) Rolling and deep-processing short-process integrated manufacturing method of high-strength steel automobile sheet
CN101020191A (en) Hot rolling process of seamless steel pipe
CN101804438B (en) Roll forming method of large and medium-size aluminum alloy hollow disk-shaped forgings
CN110153199A (en) A kind of controlled rolling method of large scale rod bar
CN104368621A (en) Manufacturing method of metal plate
CN101020192A (en) Hot rolling process of seamless steel pipe
CN108326072B (en) Magnesium alloy seamless pipe diameter forging and piercing rolling process
CN101791668B (en) Roll forming method of large and medium aluminum alloy solid disk forging
CN101791669B (en) Roll forming method of large and medium structural steel solid disk forging
CN108237197A (en) A kind of forging method for improving the flaw detection of structural steel large-sized ring part
CN101804439B (en) Roll forming method of large and medium-size structural steel hollow disk-shaped forgings
CN101758152B (en) Rolling formation method of large and medium hollow titanium alloy disc-shaped forge piece
CN101632998A (en) Target plasticity deformation method
CN101428291A (en) Production process for large weight soldering-free molybdenum wire pole stock
CN106064221A (en) A kind of Forging Technology of GCr15 roller shell
CN101758153B (en) Rolling formation method of large and medium stainless steel hollow disc-shaped forge piece
RU2381296C1 (en) METHOD OF RECEIVING OF SHEETS FROM TITANIUM ALLOY Ti-6Al-4V
CN108746440B (en) A kind of high cylindrical forged piece segmentation milling method of large-sized high-temperature alloy

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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20111102

Termination date: 20190319

CF01 Termination of patent right due to non-payment of annual fee