CN111036820A - Press-in type free forging forming method - Google Patents

Press-in type free forging forming method Download PDF

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Publication number
CN111036820A
CN111036820A CN201911357437.XA CN201911357437A CN111036820A CN 111036820 A CN111036820 A CN 111036820A CN 201911357437 A CN201911357437 A CN 201911357437A CN 111036820 A CN111036820 A CN 111036820A
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CN
China
Prior art keywords
punch
forging
press
forge piece
forming method
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
CN201911357437.XA
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Chinese (zh)
Inventor
舒勇
敖坤
万剑平
王志录
吴金
张元东
陈小虎
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.)
Jiangxi Jinghang Aviation Forging & Casting Co ltd
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Jiangxi Jinghang Aviation Forging & Casting Co ltd
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Application filed by Jiangxi Jinghang Aviation Forging & Casting Co ltd filed Critical Jiangxi Jinghang Aviation Forging & Casting Co ltd
Priority to CN201911357437.XA priority Critical patent/CN111036820A/en
Publication of CN111036820A publication Critical patent/CN111036820A/en
Pending legal-status Critical Current

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    • 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
    • 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
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K29/00Arrangements for heating or cooling during processing

Abstract

The invention discloses a forming method of press-in free forging, which aims to solve the problem of the existing high-strength alloy free forging. The method comprises the following specific steps: calculating the deformation process of the forge piece, selecting a punch and preheating the punch; forging the forged piece with the size of the allowance obtained by subtracting the press-in punch according to the pre-calculated deformation process and the size requirement of the forged piece; step three, judging and positioning the pressing position of a punch in the forge piece, and pressing the punch in; and step four, shaping the forge piece until the forge piece is finished, wherein the punch pressed in the shaping process is subjected to compressive stress and can be gradually discharged out of the forge piece. The invention is easy to master, has strong operability, does not need punching, reduces the blanking weight of the high-strength alloy forging by using the tool, greatly improves the material utilization rate and the forging yield, simultaneously can ensure the comprehensive performance of the forging and reduces the use cost of the high-strength alloy product.

Description

Press-in type free forging forming method
Technical Field
The invention relates to the field of high-strength alloy free forging, in particular to a forming method of press-in type free forging.
Background
The titanium alloy has the excellent performances of small specific gravity, high strength, high temperature resistance, corrosion resistance and the like, and is currently applied in the military field of aerospace and the like on a large scale. In the field of aviation, the dosage of the third generation (B-747, A-300) titanium alloy of Boeing company accounts for more than 9 percent; the consumption of the titanium alloy structural part threo-27 in the third generation fighter plane is 15 percent, and the consumption of the titanium alloy structural part in the fourth generation fighter plane F-22 accounts for 41 percent of the total structure of the main body. At present, TC4-DT titanium alloy structural parts are mostly obtained by forging and then machining. Titanium alloy and superalloy are difficult to realize forge piece punching, other defects such as tensile fracture and the like caused by severe deformation can occur to the surrounding tissues of the forge piece after the forge piece is punched, and the utilization rate of the forge piece is high without punching.
Disclosure of Invention
An object of an embodiment of the present invention is to provide a press-in type free forging method to solve the above problems in the background art.
In order to achieve the above purpose, the embodiments of the present invention provide the following technical solutions:
a press-in type free forging forming method comprises the following specific steps:
calculating the deformation process of the forge piece, selecting a punch and preheating the punch;
forging the forging with the size of the allowance obtained by subtracting the pressing punch according to the pre-calculated deformation process and the size requirement of the forging, so as to obtain the basic shape of the forging;
judging and positioning the pressing position of a punch in the forge piece, pressing the punch in, wherein the pressing process is required to be stable and slow, and the temperature rise of the forge piece caused by severe deformation is avoided;
and step four, shaping the forge piece until the forge piece is finished, wherein the punch pressed in the shaping process is subjected to compressive stress and can be gradually discharged out of the forge piece.
As a further scheme of the embodiment of the invention: and in the first step, different punches are selected according to the shape and the use requirement of the forging.
As a further scheme of the embodiment of the invention: in the first step, the punch is required to be tapered.
As a further scheme of the embodiment of the invention: and in the third step, the pressing position of the punch in the forge piece is manually judged.
As a further scheme of the embodiment of the invention: and in the second step, the forging is fixed on the lower anvil block.
As a further scheme of the embodiment of the invention: the temperature for preheating the punch in the first step is 380-420 ℃.
As a further scheme of the embodiment of the invention: in the first step, the preheating mode of the punch is electric furnace preheating and heat preservation.
Compared with the prior art, the embodiment of the invention has the beneficial effects that:
the invention has reasonable design, easy mastering and strong operability, does not need punching, reduces the blanking weight of the high-strength alloy forging by using the tool, greatly improves the material utilization rate and the forging yield, simultaneously can ensure the comprehensive performance of the forging and reduces the use cost of the high-strength alloy product.
Drawings
Fig. 1 is a schematic flow chart of a press-in type free forging forming method.
Detailed Description
The technical solution of the present patent will be described in further detail with reference to the following embodiments.
Example 1
A press-in type free forging forming method comprises the following specific steps:
step one, calculating the deformation process of the forging, selecting a punch, wherein the punch is required to be subjected to taper drawing, and preheating the punch, wherein the preheating temperature of the punch is 380 ℃;
forging the forging with the size of the allowance obtained by subtracting the pressing punch according to the pre-calculated deformation process and the size requirement of the forging, so as to obtain the basic shape of the forging;
judging and positioning the pressing position of a punch in the forge piece, pressing the punch in, wherein the pressing process is required to be stable and slow, and the temperature rise of the forge piece caused by severe deformation is avoided;
and step four, shaping the forge piece until the forge piece is finished, wherein the punch pressed in the shaping process is subjected to compressive stress and can be gradually discharged out of the forge piece.
As a further scheme of the embodiment of the invention: and in the first step, different punches are selected according to the shape and the use requirement of the forging.
Example 2
365Kg of weight of the punch is not pressed in, 330Kg of weight of the forging pressed in the punch, and about 10% of material is saved. The production process of the press-in punch will be described below.
1. Selecting a punch: selecting a punch with the diameter of 160 multiplied by 200, wherein the punch material is H13 (the material is 4Cr5MoSiV1 which is common hot die steel), the preheating temperature of the punch is 400 ℃ (the preheating mode of the punch is a preheating mode of an electric furnace preheating furnace, and the temperature is kept for 60 minutes.)
2. Designing the shape of the forging pressing punch: according to the punch pressing amount, the allowance of 5mm is reduced in the length direction and the width direction of the forge piece respectively, the allowance of 5mm is the amount of outward expansion of metal after the punch is pressed in, and the thickness dimension of the forge piece is consistent with that of a finished forge piece.
3. Pressing in a punch: placing the punch at a selected position by a manual bench worker, wherein the requirement on the placing time cannot be overlong, then applying pressure to the punch by equipment to press the punch into the forge piece, wherein the pressing amount of the punch is 2/3 of the thickness of the forge piece, and the pressing speed is selected to be 3 mm/s.
4. Micro-shaping of the forged piece: after the punch is pressed in, the metal of the pressing part of the forging piece flows outwards and produces bulging degree at the edge, the forging piece is erected, the bulging degree position is slightly pressed, and the punch is outwards discharged along the taper direction of the drawing die due to the fact that the punch is subjected to the force in the pressing direction. The forging process only comprises the steps of micro-shaping a forge piece and taking out a punch, and the forging pressing amount is selected to be less than or equal to 5 mm.
5. Cooling the punch for later use: because the punch is pressed into the high-temperature forging, continuous production cannot be realized, the strength of the punch is reduced due to the temperature rise in the continuous production, and the punch deforms when pressed again. In this case 5 punches were kept in reserve.
The detection requirement of the forge piece is that one piece is extracted from each batch to detect the mechanical property, the forge piece product of the batch is qualified and delivered to manufacturers for use, and compared with the prior method, the method saves 10 percent of raw materials and can directly reduce the blanking weight of the forge piece. The punch can be repeatedly used for many times, and the use cost is low. The die forging can also greatly improve the yield of the forged piece product, but a large amount of die cost needs to be invested. And the tonnage of the required forging equipment is larger, about 2 ten thousand tons of friction press is required for producing the die forging piece of the embodiment 2, and the use limit is larger.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims (7)

1. A press-in type free forging forming method is characterized by comprising the following specific steps:
calculating the deformation process of the forge piece, selecting a punch and preheating the punch;
forging the forging with the size of the allowance obtained by subtracting the pressing punch according to the pre-calculated deformation process and the size requirement of the forging, so as to obtain the basic shape of the forging;
judging and positioning the pressing position of the punch in the forge piece, and stably and slowly pressing the punch in;
and step four, shaping the forge piece until the forging is finished.
2. The press-in free forging forming method as claimed in claim 1, wherein in the first step, different punches are selected according to the shape and use requirements of the forging.
3. The press-in free forging forming method as set forth in claim 1, wherein the punch is further tapered in the first step.
4. The press-in type free forging forming method according to claim 1, wherein the pressing-down position of the punch in the forging is manually judged in the third step.
5. The method of claim 1, wherein in step two the forging is secured to a lower anvil.
6. The press-in type free forging forming method as claimed in claim 1, wherein the temperature for preheating the punch in the first step is 380-420 ℃.
7. The press-in type free forging forming method according to claim 1 or 6, wherein the preheating mode of the punch in the first step is electric furnace preheating and heat preservation.
CN201911357437.XA 2019-12-25 2019-12-25 Press-in type free forging forming method Pending CN111036820A (en)

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Application Number Priority Date Filing Date Title
CN201911357437.XA CN111036820A (en) 2019-12-25 2019-12-25 Press-in type free forging forming method

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Application Number Priority Date Filing Date Title
CN201911357437.XA CN111036820A (en) 2019-12-25 2019-12-25 Press-in type free forging forming method

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CN111036820A true CN111036820A (en) 2020-04-21

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Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU816646A1 (en) * 1978-10-30 1981-03-30 Предприятие П/Я А-3686 Method of producing articles with throgh hole
JPS62168626A (en) * 1986-01-20 1987-07-24 Yamaha Motor Co Ltd Gear shaft of speed changer
SU1337180A1 (en) * 1984-10-30 1987-09-15 Завод-ВТУЗ при Карагандинском металлургическом комбинате Method of open broaching of billet
RU2063838C1 (en) * 1994-10-24 1996-07-20 Басюк Семар Тимофеевич Method or wheel type pieces production
CN101184562A (en) * 2005-05-26 2008-05-21 昭和电工株式会社 Method and apparatus for hole punching
CN102319757A (en) * 2011-08-18 2012-01-18 中国兵器工业第五二研究所 Preparation method of magnesium alloy variable-section cylindrical member by composite extrusion deformation
CN104308056A (en) * 2014-08-20 2015-01-28 二重集团(德阳)重型装备股份有限公司 Hot forging forming method for cylindrical forged piece
CN105057539A (en) * 2015-09-14 2015-11-18 通裕重工股份有限公司 Forging mold and method for blind hole forge piece
CN105397001A (en) * 2015-12-02 2016-03-16 贵州安大航空锻造有限责任公司 Isothermal forging forming method of titanium alloy complex sheet forged piece
CN105522087A (en) * 2016-01-19 2016-04-27 溧阳市金昆锻压有限公司 Die forging process of granulator press roll
CN105598335A (en) * 2014-11-03 2016-05-25 徐杰 Forging technology of deep blind hole processing with impact method
CN105618652A (en) * 2014-11-03 2016-06-01 徐杰 Forging punch for machining deep blind hole through static pressure impact method
CN105618649A (en) * 2014-11-03 2016-06-01 徐杰 Forging technique for machining deepened blind hole through impact method
CN105880447A (en) * 2016-06-17 2016-08-24 二十二冶集团精密锻造有限公司 Closed forging process for drilling tool wire-lifting forge pieces
CN105921672A (en) * 2016-05-17 2016-09-07 山东大学 Isothermal forging method of straight bevel gear
CN106670374A (en) * 2016-12-01 2017-05-17 贵州安大航空锻造有限责任公司 Near-isothermal forging forming method for Ti6242 titanium alloy hollow shaft journal forged piece
CN106825344A (en) * 2017-02-16 2017-06-13 哈尔滨汽轮机厂有限责任公司 A kind of free forging method that male sportsman sealing ring is realized using 1 ton of flat-die hammer
CN106862452A (en) * 2015-12-14 2017-06-20 陕西宏远航空锻造有限责任公司 A kind of isothermal β forging methods of TC17 titanium alloys blisk
CN106862473A (en) * 2015-12-14 2017-06-20 陕西宏远航空锻造有限责任公司 A kind of processing method of titanium alloy basin shape Forging
CN108405788A (en) * 2018-04-23 2018-08-17 陕西宏远航空锻造有限责任公司 A kind of forging method of TiB/7050 aluminum matrix composites forging
CN109226622A (en) * 2018-09-18 2019-01-18 西安三角防务股份有限公司 A kind of TA15 titanium alloy forging forging forming method with high-intensity and high-tenacity

Patent Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU816646A1 (en) * 1978-10-30 1981-03-30 Предприятие П/Я А-3686 Method of producing articles with throgh hole
SU1337180A1 (en) * 1984-10-30 1987-09-15 Завод-ВТУЗ при Карагандинском металлургическом комбинате Method of open broaching of billet
JPS62168626A (en) * 1986-01-20 1987-07-24 Yamaha Motor Co Ltd Gear shaft of speed changer
RU2063838C1 (en) * 1994-10-24 1996-07-20 Басюк Семар Тимофеевич Method or wheel type pieces production
CN101184562A (en) * 2005-05-26 2008-05-21 昭和电工株式会社 Method and apparatus for hole punching
CN102319757A (en) * 2011-08-18 2012-01-18 中国兵器工业第五二研究所 Preparation method of magnesium alloy variable-section cylindrical member by composite extrusion deformation
CN104308056A (en) * 2014-08-20 2015-01-28 二重集团(德阳)重型装备股份有限公司 Hot forging forming method for cylindrical forged piece
CN105598335A (en) * 2014-11-03 2016-05-25 徐杰 Forging technology of deep blind hole processing with impact method
CN105618649A (en) * 2014-11-03 2016-06-01 徐杰 Forging technique for machining deepened blind hole through impact method
CN105618652A (en) * 2014-11-03 2016-06-01 徐杰 Forging punch for machining deep blind hole through static pressure impact method
CN105057539A (en) * 2015-09-14 2015-11-18 通裕重工股份有限公司 Forging mold and method for blind hole forge piece
CN105397001A (en) * 2015-12-02 2016-03-16 贵州安大航空锻造有限责任公司 Isothermal forging forming method of titanium alloy complex sheet forged piece
CN106862452A (en) * 2015-12-14 2017-06-20 陕西宏远航空锻造有限责任公司 A kind of isothermal β forging methods of TC17 titanium alloys blisk
CN106862473A (en) * 2015-12-14 2017-06-20 陕西宏远航空锻造有限责任公司 A kind of processing method of titanium alloy basin shape Forging
CN105522087A (en) * 2016-01-19 2016-04-27 溧阳市金昆锻压有限公司 Die forging process of granulator press roll
CN105921672A (en) * 2016-05-17 2016-09-07 山东大学 Isothermal forging method of straight bevel gear
CN105880447A (en) * 2016-06-17 2016-08-24 二十二冶集团精密锻造有限公司 Closed forging process for drilling tool wire-lifting forge pieces
CN106670374A (en) * 2016-12-01 2017-05-17 贵州安大航空锻造有限责任公司 Near-isothermal forging forming method for Ti6242 titanium alloy hollow shaft journal forged piece
CN106825344A (en) * 2017-02-16 2017-06-13 哈尔滨汽轮机厂有限责任公司 A kind of free forging method that male sportsman sealing ring is realized using 1 ton of flat-die hammer
CN108405788A (en) * 2018-04-23 2018-08-17 陕西宏远航空锻造有限责任公司 A kind of forging method of TiB/7050 aluminum matrix composites forging
CN109226622A (en) * 2018-09-18 2019-01-18 西安三角防务股份有限公司 A kind of TA15 titanium alloy forging forging forming method with high-intensity and high-tenacity

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
张如华等: "孔径比为2.50~3.00的自由锻冲孔坯料形状研究", 《锻压技术》 *
机械工人应知考核题解丛书编审委员会: "《锻压工应知考核题解》", 31 March 1994, 机械工业出版社 *
汪大年: "《高等学校试用教材 金属塑性成形原理》", 30 June 1982, 机械工业出版社 *
莫畏: "《钛》", 30 June 2008, 冶金工业出版社 *

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Application publication date: 20200421