CN111195696A - Processing technology for large-size forged caterpillar link and caterpillar link - Google Patents

Processing technology for large-size forged caterpillar link and caterpillar link Download PDF

Info

Publication number
CN111195696A
CN111195696A CN202010008887.4A CN202010008887A CN111195696A CN 111195696 A CN111195696 A CN 111195696A CN 202010008887 A CN202010008887 A CN 202010008887A CN 111195696 A CN111195696 A CN 111195696A
Authority
CN
China
Prior art keywords
forging
blank
forged
caterpillar
size forged
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
CN202010008887.4A
Other languages
Chinese (zh)
Inventor
文忠绘
文海清
张新东
文臣涛
胡友强
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.)
Jining Ning Run Wen Zheng Forge Co ltd
Original Assignee
Jining Ning Run Wen Zheng Forge 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 Jining Ning Run Wen Zheng Forge Co ltd filed Critical Jining Ning Run Wen Zheng Forge Co ltd
Priority to CN202010008887.4A priority Critical patent/CN111195696A/en
Publication of CN111195696A publication Critical patent/CN111195696A/en
Pending legal-status Critical Current

Links

Images

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
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/02Die forging; Trimming by making use of special dies ; Punching during forging
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D55/00Endless track vehicles
    • B62D55/08Endless track units; Parts thereof
    • B62D55/18Tracks
    • B62D55/20Tracks of articulated type, e.g. chains
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C22/00Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Heat Treatment Of Articles (AREA)
  • Forging (AREA)

Abstract

The invention belongs to the technical field of caterpillar link processing, and particularly relates to a processing technology for large-size forged caterpillar links and caterpillar links, which comprise the following processing steps: s1: annealing treatment, namely preparing annealing equipment; s2: blanking; s3: phosphorization and saponification treatment; s4: forging and forging the blank, namely placing the blank on a caterpillar track section die, fixing the die on large forging equipment, wherein the forging pressure of the forging equipment is more than 10000 tons, heating the blank to the range of 1200 +/-25 ℃ during forging, and the temperature difference between the core surface and the surface is less than or equal to 50 ℃; s5: punching and trimming; s6: quenching, namely quenching the large-size forged caterpillar track section, carrying out continuous induction quenching, continuously scanning the heating speed of 350-: tempering; the large-size forged caterpillar track section has the advantages of good surface quality, good mechanical property and difficulty in brittle fracture.

Description

Processing technology for large-size forged caterpillar link and caterpillar link
Technical Field
The invention relates to the technical field of caterpillar link processing, in particular to a processing technology for large-size forged caterpillar links and caterpillar links.
Background
Forging is a forging processing method which enables a blank or an ingot to generate plastic deformation under the action of forging equipment and a die so as to obtain a certain geometric shape and quality.
The casting is a processing method which comprises the steps of smelting metal into liquid meeting certain requirements, pouring the liquid into a casting mold, cooling, solidifying and cleaning to obtain a casting with a preset shape, size and performance.
The caterpillar track section with the maximum distance of 350mm in the world is one of large engineering machinery chassis parts and is commonly used on electric shovels and excavators with the distance of more than 250T. The track shoe produced by adopting the casting process has the defects of easy formation of air holes and shrinkage cavities, poor surface quality, poor mechanical property, easy brittle failure and the like, and cannot meet the use requirement. The mechanical property of a forged piece product produced by the existing forging process is much superior to that of a product produced by a casting process, and a special ultra-large forging device and a special ultra-large forging die for forging the caterpillar track link are required to be provided for applying the forging process to the production process of the caterpillar track link.
In order to solve the problems, the application provides a processing technology for forging the caterpillar track section in a large size and the caterpillar track section.
Disclosure of Invention
Objects of the invention
In order to solve the technical problems in the background art, the invention provides a processing technology of a large-size forged caterpillar track section and the caterpillar track section, and the processing technology has the characteristic of replacing the traditional casting production mode.
(II) technical scheme
In order to solve the problems, the invention provides a processing technology of a large-size forged caterpillar track section, which comprises the following processing steps:
s1: annealing treatment, namely preparing annealing equipment, and putting the blank into the annealing equipment, wherein the annealing equipment comprises an annealing furnace and a heat recovery box, a first temperature sensor is arranged on the annealing furnace, the detection end of the first temperature sensor extends into the annealing furnace, an S-shaped heat exchange tube is arranged in the heat recovery box, two ends of the S-shaped heat exchange tube are communicated with the inside of the annealing furnace, a water inlet tube and a water outlet tube are arranged on one side of the heat recovery box, a second temperature sensor is also arranged on the heat recovery box, and the detection end of the second temperature sensor extends into the heat recovery box;
s2: blanking, namely processing by adopting a centerless lathe, peeling the whole round steel, and then blanking by using a sawing machine;
s3: phosphating and saponifying, namely removing oxide skin on the surface of the blank by hydrochloric acid; after acid washing, a layer of phosphate film is generated on the surface of the blank through phosphating treatment, and the phosphated blank is put into a saponification cylinder to absorb soap liquid;
s4: forging and forging the blank, namely placing the blank on a caterpillar track section die, fixing the die on large forging equipment, wherein the forging pressure of the forging equipment is more than 10000 tons, heating the blank to the range of 1200 +/-25 ℃ during forging, and the temperature difference between the core surface and the surface is less than or equal to 50 ℃;
s5: punching and trimming, namely placing the formed workpiece in a high-speed machining center for machining, and punching and trimming the workpiece to obtain a formed large-size forged caterpillar link;
s6: quenching, namely quenching the large-size forged caterpillar track section, carrying out continuous induction quenching, continuously scanning the heating speed of 350-;
s7: and (4) tempering, namely heating the quenched large-size forged track section at the temperature of 230 ℃ and 250 ℃, and preserving the heat for 1-4 hours to obtain the finished large-size forged track section.
Preferably, the interior bottom of annealing stove is provided with first electric heating wire, the interior upper portion of annealing stove is provided with second electric heating wire, and the annealing stove inside that is located first electric heating wire top is fixed with the supporting network, the top of supporting network is fixed with the support frame, the top of support frame is provided with the tray, be provided with the stock in the tray.
Preferably, all the cooperation is installed the valve on inlet tube and the outlet pipe, the upper end of S-shaped heat exchange tube is connected with first connecting pipe, the upper portion at the annealing stove is connected to the other end of first connecting pipe, the lower extreme of S-shaped heat exchange tube is connected with the second connecting pipe, and the second connecting pipe is connected with turbofan 'S air inlet end, turbofan' S air-out end is connected with the third connecting pipe, the other end of third connecting pipe and the sub-unit connection of annealing stove.
Preferably, the first connecting pipe is provided with an electromagnetic valve.
Preferably, in S6, quenching the large-size forged track link, performing continuous induction quenching, continuously scanning and heating at 365mm/min, wherein the quenching medium is tap water and the water temperature is 30 ℃.
Preferably, in the step S7, tempering, heating the quenched large-size forged track link at 240 ℃, and preserving heat for 2.5 hours to obtain a finished large-size forged track link.
A large-size forged caterpillar track section is formed by processing a large-size forged caterpillar track section through a processing technology.
Preferably, the large size forged track section has a pitch of 350 mm.
The technical scheme of the invention has the following beneficial technical effects:
1. the large-size forged caterpillar track section obtained by the processing technology of the large-size forged caterpillar track section has good surface quality and mechanical property and is not easy to brittle fracture;
2. when annealing the stock, unnecessary heat according to the processing condition, can be appropriate discharge the heat to the heat recovery case, and the aquatic in heat transfer to the heat recovery case, water absorbs the heat, and hot water can supply people to use.
Drawings
FIG. 1 is a flow chart of the process of the present invention;
FIG. 2 is a schematic view of the structure of an annealing apparatus according to the present invention;
FIG. 3 is a schematic view of a large-sized forged track link according to the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the accompanying drawings in conjunction with the following detailed description. It should be understood that the description is intended to be exemplary only, and is not intended to limit the scope of the present invention. Moreover, in the following description, descriptions of well-known structures and techniques are omitted so as to not unnecessarily obscure the concepts of the present invention.
Example 1
As shown in fig. 1-3, the processing technology of the large-size forged track link provided by the invention comprises the following processing steps:
s1: annealing treatment, preparing annealing equipment, and putting the blank into the annealing equipment, wherein the annealing equipment comprises an annealing furnace 2 and a heat recovery box 3, a first temperature sensor 5 is arranged on the annealing furnace 2, the detection end of the first temperature sensor 5 extends into the annealing furnace 2, an S-shaped heat exchange tube 12 is arranged in the heat recovery box 3, two ends of the S-shaped heat exchange tube 12 are communicated with the inside of the annealing furnace 2, a water inlet tube 14 and a water outlet tube 15 are arranged on one side of the heat recovery box 3, a second temperature sensor 17 is also arranged on the heat recovery box 3, and the detection end of the second temperature sensor 17 extends into the heat recovery box 3;
s2: blanking, namely processing by adopting a centerless lathe, peeling the whole round steel, and then blanking by using a sawing machine;
s3: phosphating and saponifying, namely removing oxide skin on the surface of the blank by hydrochloric acid; after acid washing, a layer of phosphate film is generated on the surface of the blank through phosphating treatment, and the phosphated blank is put into a saponification cylinder to absorb soap liquid;
s4: forging and forging the blank, namely placing the blank on a caterpillar track section die, fixing the die on large forging equipment, wherein the forging pressure of the forging equipment is more than 10000 tons, heating the blank to the range of 1200 +/-25 ℃ during forging, and the temperature difference between the core surface and the surface is less than or equal to 50 ℃;
it is worth to be noted that when the die is produced and processed, a cavity of the die needs to be processed by a high-speed processing center so as to ensure the precision of the die, a blank of the die needs to be heated to be within the range of 1200 +/-25 ℃, and the temperature difference between the core surface and the surface is less than or equal to 50 ℃;
s5: punching and trimming, namely placing the formed workpiece in a high-speed machining center for machining, and punching and trimming the workpiece to obtain a formed large-size forged caterpillar link;
s6: quenching, namely quenching the large-size forged caterpillar track section, carrying out continuous induction quenching, continuously scanning the heating speed of 350-;
s7: and (4) tempering, namely heating the quenched large-size forged track section at the temperature of 230 ℃ and 250 ℃, and preserving the heat for 1-4 hours to obtain the finished large-size forged track section.
In this embodiment, it should be noted that the first electric heating wire 18 is disposed at the inner bottom of the annealing furnace 2, the second electric heating wire 4 is disposed at the inner upper portion of the annealing furnace 2, the supporting net 8 is fixed inside the annealing furnace 2 above the first electric heating wire 18, the supporting frame 6 is fixed at the top of the supporting net 8, the tray 7 is disposed at the top of the supporting frame 6, and the blank is disposed in the tray 7.
In this embodiment, it should be noted that valves 16 are respectively installed on the water inlet pipe 14 and the water outlet pipe 15 in a matching manner, the upper end of the S-shaped heat exchange pipe 12 is connected with a first connection pipe 11, the other end of the first connection pipe 11 is connected to the upper portion of the annealing furnace 2, the lower end of the S-shaped heat exchange pipe 12 is connected with a second connection pipe, the second connection pipe is connected with the air inlet end of the turbo fan 9, the air outlet end of the turbo fan 9 is connected with a third connection pipe 10, and the other end of the third connection pipe 10 is connected with the lower.
In this embodiment, it should be noted that the solenoid valve 13 is mounted on the first connecting pipe 11.
In this embodiment, in S6, quenching is performed, in which a large-sized forged track link is quenched, continuous induction quenching is performed, the heating speed is 365mm/min by continuous scanning, the quenching medium is tap water, and the water temperature is 30 ℃.
In this embodiment, it should be noted that in S7, the large-size forged track link after quenching is tempered, heated to 240 ℃, and then heat preserved for 2.5 hours, so as to obtain a finished large-size forged track link.
In the scheme of the invention, a first temperature sensor 5 is arranged on an annealing furnace 2, a detection end of the first temperature sensor 5 extends to the inside of the annealing furnace 2, an S-shaped heat exchange tube 12 is arranged in a heat recovery box 3, two ends of the S-shaped heat exchange tube 12 are communicated with the inside of the annealing furnace 2, a water inlet tube 14 and a water outlet tube 15 are arranged on one side of the heat recovery box 3, a second temperature sensor 17 is also arranged on the heat recovery box 3, a detection end of the second temperature sensor 17 extends to the inside of the heat recovery box 3, when blank materials are annealed, redundant heat can be properly discharged into the heat recovery box 3 according to the processing condition, the heat is transferred into water in the heat recovery box 3, the water absorbs the heat, and the hot water can be used by people;
example 2
As shown in fig. 3, a large-size forged track link 1 is formed by a machining process of the large-size forged track link.
In this embodiment, it should be noted that the pitch of the large-sized forged track link is 350 mm.
According to the invention, the large-size forged caterpillar track section is quenched, continuous induction quenching is carried out, the heating speed is continuously scanned at 365mm/min, the quenching medium is tap water, the water temperature is 30 ℃, the workpiece is integrally heated by controlling the heating speed and the heat preservation time of the workpiece, the full tempering of the caterpillar track section is ensured, the organization is better stabilized, the residual internal stress is reduced, the product quality is improved, and the large-size forged caterpillar track section has good surface quality, good mechanical property and is not easy to brittle fracture.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (8)

1. A processing technology for large-size forged caterpillar track sections is characterized by comprising the following processing steps:
s1: annealing, preparing annealing equipment, and putting the blank into the annealing equipment, wherein the annealing equipment comprises an annealing furnace (2) and a heat recovery box (3), a first temperature sensor (5) is arranged on the annealing furnace (2), the detection end of the first temperature sensor (5) extends into the annealing furnace (2), an S-shaped heat exchange tube (12) is arranged in the heat recovery box (3), two ends of the S-shaped heat exchange tube (12) are communicated with the inside of the annealing furnace (2), a water inlet tube (14) and a water outlet tube (15) are arranged on one side of the heat recovery box (3), a second temperature sensor (17) is further arranged on the heat recovery box (3), and the detection end of the second temperature sensor (17) extends into the heat recovery box (3);
s2: blanking, namely processing by adopting a centerless lathe, peeling the whole round steel, and then blanking by using a sawing machine;
s3: phosphating and saponifying, namely removing oxide skin on the surface of the blank by hydrochloric acid; after acid washing, a layer of phosphate film is generated on the surface of the blank through phosphating treatment, and the phosphated blank is put into a saponification cylinder to absorb soap liquid;
s4: forging and forging the blank, namely placing the blank on a caterpillar track section die, fixing the die on large forging equipment, wherein the forging pressure of the forging equipment is more than 10000 tons, heating the blank to the range of 1200 +/-25 ℃ during forging, and the temperature difference between the core surface and the surface is less than or equal to 50 ℃;
s5: punching and trimming, namely placing the formed workpiece in a high-speed machining center for machining, and punching and trimming the workpiece to obtain a formed large-size forged caterpillar link;
s6: quenching, namely quenching the large-size forged caterpillar track section, carrying out continuous induction quenching, continuously scanning the heating speed of 350-;
s7: and (4) tempering, namely heating the quenched large-size forged track section at the temperature of 230 ℃ and 250 ℃, and preserving the heat for 1-4 hours to obtain the finished large-size forged track section.
2. The processing technology of the large-size forged caterpillar track section according to claim 1, wherein a first electric heating wire (18) is arranged at the inner bottom of the annealing furnace (2), a second electric heating wire (4) is arranged at the inner upper portion of the annealing furnace (2), a supporting net (8) is fixed inside the annealing furnace (2) above the first electric heating wire (18), a supporting frame (6) is fixed at the top of the supporting net (8), a tray (7) is arranged at the top of the supporting frame (6), and a blank is arranged in the tray (7).
3. The machining process of the large-size forged caterpillar track section according to claim 2, wherein valves (16) are installed on the water inlet pipe (14) and the water outlet pipe (15) in a matched mode, a first connecting pipe (11) is connected to the upper end of the S-shaped heat exchange pipe (12), the other end of the first connecting pipe (11) is connected to the upper portion of the annealing furnace (2), a second connecting pipe is connected to the lower end of the S-shaped heat exchange pipe (12), the second connecting pipe is connected with the air inlet end of the turbofan (9), the air outlet end of the turbofan (9) is connected with a third connecting pipe (10), and the other end of the third connecting pipe (10) is connected with the lower portion of the annealing furnace (2).
4. A process for machining a large-size forged track link as claimed in claim 3, wherein said first connecting pipe (11) is provided with a solenoid valve (13).
5. The processing technology of the large-size forged track link as claimed in claim 1, wherein in step S6, quenching is performed, the large-size forged track link is quenched and is subjected to continuous induction quenching, the heating speed is continuously scanned at 365mm/min, the quenching medium is tap water, and the water temperature is 30 ℃.
6. The processing technology of the large-size forged track link as claimed in claim 1, wherein in the step S7, the large-size forged track link after quenching is tempered, heated to 240 ℃ and kept warm for 2.5 hours to obtain the finished large-size forged track link.
7. A large size forged track link, characterized in that said large size forged track link (1) is formed by a process of any one of claims 1 to 6.
8. The oversized forged track section as claimed in claim 7, wherein the oversized forged track section has a pitch of 350 mm.
CN202010008887.4A 2020-01-06 2020-01-06 Processing technology for large-size forged caterpillar link and caterpillar link Pending CN111195696A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010008887.4A CN111195696A (en) 2020-01-06 2020-01-06 Processing technology for large-size forged caterpillar link and caterpillar link

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010008887.4A CN111195696A (en) 2020-01-06 2020-01-06 Processing technology for large-size forged caterpillar link and caterpillar link

Publications (1)

Publication Number Publication Date
CN111195696A true CN111195696A (en) 2020-05-26

Family

ID=70741765

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010008887.4A Pending CN111195696A (en) 2020-01-06 2020-01-06 Processing technology for large-size forged caterpillar link and caterpillar link

Country Status (1)

Country Link
CN (1) CN111195696A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112475163A (en) * 2020-12-08 2021-03-12 徐州徐工履带底盘有限公司 Full-automatic caterpillar track section forging process adopting multi-station die
CN112496675A (en) * 2020-11-06 2021-03-16 青岛征和工业股份有限公司 Machining process for low-speed high-power marine engine transmission chain plate
CN113000778A (en) * 2021-04-08 2021-06-22 苏州九源机械有限公司 Caterpillar track link processing technology based on trimming die
CN113000777A (en) * 2021-04-06 2021-06-22 苏州九源机械有限公司 Forging process of excavator caterpillar link

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101314812A (en) * 2008-06-05 2008-12-03 南京汽车锻造有限公司 Smithing exhaust heat quenching process for caterpillar track node with node pitch more than 200mm
CN102527909A (en) * 2012-01-16 2012-07-04 彭亦楚 Continuous forging furnace
CN202519297U (en) * 2012-03-01 2012-11-07 瓦房店市鑫海节能电炉厂 Non-oxidation spheroidizing annealing forced air cooling and waste heat recycling device
CN103540716A (en) * 2013-09-22 2014-01-29 徐州徐工铁路装备有限公司 Processing method of tread thermal treatment for caterpillar link
CN104858344A (en) * 2015-05-19 2015-08-26 第一拖拉机股份有限公司 Manufacturing method for large driving wheel forged pieces
CN107805694A (en) * 2017-11-18 2018-03-16 双威大昌锻造(安徽)有限公司 The quenching unit and its operating method of a kind of Chain Link
CN107828953A (en) * 2017-08-22 2018-03-23 徐州徐工履带底盘有限公司 A kind of Chain Link quenching unit and processing technology
CN108026606A (en) * 2016-08-19 2018-05-11 普锐特冶金技术日本有限公司 Continuous annealing apparatus
CN207435503U (en) * 2017-11-18 2018-06-01 双威大昌锻造(安徽)有限公司 It is a kind of to be used for Chain Link axis, the heating unit of axle sleeve

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101314812A (en) * 2008-06-05 2008-12-03 南京汽车锻造有限公司 Smithing exhaust heat quenching process for caterpillar track node with node pitch more than 200mm
CN102527909A (en) * 2012-01-16 2012-07-04 彭亦楚 Continuous forging furnace
CN202519297U (en) * 2012-03-01 2012-11-07 瓦房店市鑫海节能电炉厂 Non-oxidation spheroidizing annealing forced air cooling and waste heat recycling device
CN103540716A (en) * 2013-09-22 2014-01-29 徐州徐工铁路装备有限公司 Processing method of tread thermal treatment for caterpillar link
CN104858344A (en) * 2015-05-19 2015-08-26 第一拖拉机股份有限公司 Manufacturing method for large driving wheel forged pieces
CN108026606A (en) * 2016-08-19 2018-05-11 普锐特冶金技术日本有限公司 Continuous annealing apparatus
CN107828953A (en) * 2017-08-22 2018-03-23 徐州徐工履带底盘有限公司 A kind of Chain Link quenching unit and processing technology
CN107805694A (en) * 2017-11-18 2018-03-16 双威大昌锻造(安徽)有限公司 The quenching unit and its operating method of a kind of Chain Link
CN207435503U (en) * 2017-11-18 2018-06-01 双威大昌锻造(安徽)有限公司 It is a kind of to be used for Chain Link axis, the heating unit of axle sleeve

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112496675A (en) * 2020-11-06 2021-03-16 青岛征和工业股份有限公司 Machining process for low-speed high-power marine engine transmission chain plate
CN112475163A (en) * 2020-12-08 2021-03-12 徐州徐工履带底盘有限公司 Full-automatic caterpillar track section forging process adopting multi-station die
CN112475163B (en) * 2020-12-08 2022-05-10 徐州徐工履带底盘有限公司 Full-automatic caterpillar track section forging process adopting multi-station die
CN113000777A (en) * 2021-04-06 2021-06-22 苏州九源机械有限公司 Forging process of excavator caterpillar link
CN113000778A (en) * 2021-04-08 2021-06-22 苏州九源机械有限公司 Caterpillar track link processing technology based on trimming die

Similar Documents

Publication Publication Date Title
CN111195696A (en) Processing technology for large-size forged caterpillar link and caterpillar link
CN109433924B (en) Die for realizing rapid forming and quenching in die
CN109093048B (en) Large-scale machine brake type forging die and forging method
CN107282839A (en) A kind of forging technology of forging
CN101590596B (en) Method for manufacturing extra-thick plate blank by accumulative roller welding process
CN111496050B (en) Cold-hot composite stamping forming device and stamping method for aluminum alloy plate
CN106964948A (en) A kind of processing technology of marine gear
CN108188659A (en) A kind of manufacturing process of steel billet
CN110193580A (en) A kind of H13 material forging mold technique
CN109909315B (en) Processing technology of high-precision thin-wall pure aluminum or aluminum alloy pipe
CN104999037A (en) Concreting system for thin-walled cylindrical part and precision casting formation method
CN104174807B (en) The manufacture method of a kind of heavy caliber titanium thick-wall tube
CN111112527A (en) Forging method of large tube plate type forge piece
CN102689159B (en) Liquid die forging and rolling compound formation method for 6061 aluminum alloy irregular-section large ring piece
CN110541888A (en) Oil-cooled bearing seat and machining method thereof
CN113828678B (en) Controllable gas-assisted light alloy metal plate cold die hot forming method
CN114346605A (en) Anti-cracking machining process for F91 large valve body die forging
CN111230430B (en) Manufacturing process of front die of hub forging
CN110052595B (en) Automobile steering knuckle with anti-transgranular fracture failure mode and manufacturing method thereof
CN102689152B (en) Liquid die forging rolling compound forming method for 2014 aluminium alloy large ring member with different cross sections
CN113020276A (en) Method for repairing roll shape of section steel roll
CN102689162B (en) Liquid die forging and rolling compound formation method for 7050 aluminum alloy irregular-section large ring piece
CN108838206A (en) Improve the method and al stainless steel composite board of al stainless steel composite board performance
JP2005146415A (en) Forging manufacturing method, hardening strain suppressing tool, and forging production system
CN102689160B (en) Liquid die forging rolling compound forming method for 2A70 aluminium alloy large ring member with different cross sections

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: 20200526