CN114799760A - Method for manufacturing insert pin - Google Patents

Method for manufacturing insert pin Download PDF

Info

Publication number
CN114799760A
CN114799760A CN202210501930.XA CN202210501930A CN114799760A CN 114799760 A CN114799760 A CN 114799760A CN 202210501930 A CN202210501930 A CN 202210501930A CN 114799760 A CN114799760 A CN 114799760A
Authority
CN
China
Prior art keywords
round bar
bar structure
insert pin
less
manufacturing
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
CN202210501930.XA
Other languages
Chinese (zh)
Inventor
李勇
邓荣辉
冯静
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.)
Guangdong Junchang Technology Co ltd
Original Assignee
Guangdong Junchang Technology 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 Guangdong Junchang Technology Co ltd filed Critical Guangdong Junchang Technology Co ltd
Priority to CN202210501930.XA priority Critical patent/CN114799760A/en
Publication of CN114799760A publication Critical patent/CN114799760A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

The invention discloses a method for manufacturing an insert pin, which comprises the following steps: s10: cutting a steel wire into a round bar structure with a preset size; s20: roughly processing the round bar structure; s30: carrying out heat treatment on the round rod structure to ensure that the surface hardness of the round rod structure is HRC40-55 and the internal hardness of the round rod structure is HRC 40-55; s40: grinding the round bar structure by using a white corundum grinding wheel with the mesh number less than 200#, and reserving grinding allowance with a single side less than 0.05 mm; s50: grinding the round bar structure by using a white steel jade grinding wheel with the mesh number not less than 200 #; s60: observing the round bar structure by using a magnifying lens which is not less than 40 times, wherein if the surface of the round bar structure is smooth and has no concave-convex mark, the round bar structure is qualified, otherwise, the round bar structure is unqualified; s70: the qualified round bar structure is annealed, so that the service life of the insert pin is prolonged, and the production efficiency is improved.

Description

Method for manufacturing insert pin
Technical Field
The invention relates to the field of dies, in particular to a method for manufacturing an insert pin.
Background
As is known, in the existing aluminum alloy die casting production, an insert pin is required to form a hole or exhaust a gas, but the insert pin belongs to the most common vulnerable part, and the insert pin manufactured by the existing manufacturing method may deform or break after about 400 times of production using an aluminum alloy die casting mold, and thus needs to be repaired or replaced, which seriously affects the production efficiency and cost, and the insert pin of the existing manufacturing method generally only can be formed with a small aperture and has a shallow depth, and cannot meet the design requirements.
Therefore, there is a need for a method of manufacturing an insert that improves the useful life of the insert to overcome the above-mentioned disadvantages.
Disclosure of Invention
The invention aims to provide a method for manufacturing an insert pin, which can prolong the service life of the insert pin.
In order to achieve the above object, the insert pin manufacturing method of the present invention includes the steps of:
s10: cutting a steel wire into a round bar structure with a preset size;
s20: roughly processing the round bar structure;
s30: carrying out heat treatment on the round rod structure to ensure that the surface hardness of the round rod structure is HRC40-55 and the internal hardness of the round rod structure is HRC 40-55;
s40: grinding the round bar structure by using a white corundum grinding wheel with the mesh number less than 200#, and reserving grinding allowance with a single side less than 0.05 mm;
s50: grinding the round bar structure by using a white steel jade grinding wheel with the mesh number not less than 200 #;
s60: observing the round bar structure by using a magnifying lens which is not less than 40 times, wherein if the surface of the round bar structure is smooth and has no concave-convex mark, the round bar structure is qualified, otherwise, the round bar structure is unqualified;
s70: and annealing the qualified round bar structure.
Preferably, in S10, the steel material is 8407 special steel.
Preferably, in S20, the roughing is a combination of one or more of rough turning, rough planing, rough milling, drilling and rasping.
Preferably, at S20, the surface hardness of the round bar structure differs from the internal hardness of the round bar structure by HRC 5.
Preferably, in S20, the surface hardness of the round bar structure is HRC 47-48.
Preferably, in S20, the internal hardness of the round bar structure is HRC 47-48.
Preferably, in S40, the white corundum grinding wheel has a mesh number greater than 80# and less than 200 #; in S50, the white corundum grinding wheel has a mesh number of 200# or more and 500# or less.
Preferably, in S40, the mesh number of the white corundum grinding wheel is 120 #; in S50, the white corundum grinding wheel has a mesh number of 240 #.
Preferably, in S40, the reserved one-side grinding margin is 0.01 mm.
Preferably, in S60, the magnification of the magnifier is 50 times.
Compared with the prior art, the insert pin manufacturing method comprises the following steps: s10: cutting a steel wire into a round bar structure with a preset size; s20: roughly processing the round bar structure; s30: carrying out heat treatment on the round rod structure to ensure that the surface hardness of the round rod structure is HRC40-55 and the internal hardness of the round rod structure is HRC 40-55; s40: grinding the round bar structure by using a white corundum grinding wheel with the mesh number less than 200#, and reserving grinding allowance with a single side less than 0.05 mm; s50: grinding the round bar structure by using a white steel jade grinding wheel with the mesh number not less than 200 #; s60: observing the round bar structure by using a magnifying lens which is not less than 40 times, wherein if the surface of the round bar structure is smooth and has no concave-convex mark, the round bar structure is qualified, otherwise, the round bar structure is unqualified; s70: annealing treatment is carried out on the qualified round bar structure, the service life of the modified insert pin is prolonged from 400 die times to 2000 die times, and the depth of the modified insert pin with the phi 2mm forming aperture is increased from 3-4mm to 6-8mm, so that the efficiency and the quality of aluminum alloy die-casting production are improved.
Drawings
FIG. 1 is a flow chart of the insert pin manufacturing method of the present invention.
Fig. 2 is a perspective view of an insert manufactured by the insert manufacturing method shown in fig. 1.
Detailed Description
Referring to fig. 1 and 2, an object of the present invention is to provide a method for manufacturing an insert pin capable of increasing the service life of the insert pin.
In order to achieve the above object, the insert pin manufacturing method of the present invention includes the steps of:
s10: the steel material is processed into a round bar structure with a preset size by wire cutting, preferably, the steel material is 8407 special steel to improve the mechanical fatigue resistance and the thermal stress fatigue resistance of the insert pin 1, improve the hardness of the insert pin 1 to slow down the occurrence of thermal cracking and prolong the service life of the insert pin 1, but not limited thereto.
S20: roughly machining the round bar structure, specifically, roughly machining the round bar structure by one or a combination of rough turning, rough planing, rough milling, drilling and rasping to ensure that the rough machining of the round bar structure meets a preset requirement, but not limited to the preset requirement;
s30: performing heat treatment on the round rod structure to ensure that the surface hardness of the round rod structure is HRC40-55 and the internal hardness of the round rod structure is HRC40-55 so as to ensure the surface hardness and the internal hardness of the round rod structure and further slow down the occurrence of heat cracks of the insert needle 1, preferably, the difference between the surface hardness of the round rod structure and the internal hardness of the round rod structure is HRC 5 so as to further ensure that the difference between the surface hardness and the internal hardness of the round rod structure is smaller, further slow down the occurrence of heat cracks of the insert needle 1 and prolong the service life of the insert needle 1, but not limited thereto;
s40: grinding the round bar structure by using a white corundum grinding wheel with the mesh number smaller than 200#, reserving a grinding allowance with a single side smaller than 0.05mm for subsequent precise machining, preferably, the mesh number of the white corundum grinding wheel is larger than 80# and smaller than 200#, and the reserved single side grinding allowance is 0.01mm, so as to further ensure subsequent precise machining, but not limited by the above;
s50: grinding the round bar structure by using the white corundum grinding wheel with the mesh number not less than 200# so as to further process the surface of the round bar structure and avoid generating concave-convex marks, preferably, the mesh number of the white corundum grinding wheel is more than or equal to 200# and less than or equal to 500# so as to ensure the grinding precision, so that the insert needle 1 is suitable for more precise aluminum alloy die casting, the occurrence of thermal cracking is further slowed down, and the service life of the insert needle 1 is prolonged;
s60: observing the round bar structure by using a magnifying lens which is not less than 40 times, wherein if the surface of the round bar structure is smooth and has no concave-convex mark, the round bar structure is qualified, otherwise, the round bar structure is unqualified, so that the machining error of the round bar structure is ensured to be in a reasonable range, and the service life of the insert pin 1 is ensured, specifically, the magnification of the magnifying lens is 50 times, so that the machining error of the round bar structure is further ensured to be in a reasonable range;
s70: annealing treatment is carried out on the qualified round bar structure so as to reduce the residual stress of the round bar structure, stabilize the size and reduce the deformation and crack tendency, thereby further prolonging the service life of the insert pin 1: more specifically, the following is provided
In S30, the surface hardness of the round bar structure is HRC47-48 to further secure the surface hardness of the round bar structure, thereby extending the life of the insert 1.
At S30, the internal hardness of the round bar structure is HRC47-48 to further secure the internal hardness of the round bar structure, thereby extending the life of the insert 1.
In S40, the mesh number of the white corundum grinding wheel is 120#, and in S50, the mesh number of the white corundum grinding wheel is 240 #. The surface precision of the cylindrical structure is ensured, so that the insert pin 1 is suitable for more precise aluminum alloy die casting, the occurrence of thermal cracking is further slowed down, and the service life of the insert pin 1 is prolonged;
compared with the prior art, the insert pin manufacturing method comprises the following steps: s10: cutting a steel wire into a round bar structure with a preset size; s20: roughly processing the round bar structure; s30: carrying out heat treatment on the round rod structure to ensure that the surface hardness of the round rod structure is HRC40-55 and the internal hardness of the round rod structure is HRC 40-55; s40: grinding the round bar structure by using a white corundum grinding wheel with the mesh number less than 200#, and reserving grinding allowance with a single side less than 0.05 mm; s50: grinding the round bar structure by using a white steel jade grinding wheel with the mesh number not less than 200 #; s60: observing the round bar structure by using a magnifying lens which is not less than 40 times, wherein if the surface of the round bar structure is smooth and has no concave-convex mark, the round bar structure is qualified, otherwise, the round bar structure is unqualified; s70: the qualified round bar structure is annealed, so that the service life of the insert pin 1 is prolonged, and the production efficiency is improved.
The above disclosure is only a preferred embodiment of the present invention, which is convenient for those skilled in the art to understand and implement, and certainly not to limit the scope of the present invention, therefore, the present invention is not limited by the claims and their equivalents.

Claims (10)

1. A method for manufacturing an insert pin, comprising the steps of:
s10: cutting a steel wire into a round bar structure with a preset size;
s20: roughly processing the round bar structure;
s30: carrying out heat treatment on the round rod structure to ensure that the surface hardness of the round rod structure is HRC40-55 and the internal hardness of the round rod structure is HRC 40-55;
s40: grinding the round bar structure by using a white corundum grinding wheel with the mesh number less than 200#, and reserving grinding allowance with a single side less than 0.05 mm;
s50: grinding the round bar structure by using a white steel jade grinding wheel with the mesh number not less than 200 #;
s60: observing the round bar structure by using a magnifying lens which is not less than 40 times, wherein if the surface of the round bar structure is smooth and has no concave-convex mark, the round bar structure is qualified, otherwise, the round bar structure is unqualified;
s70: and annealing the qualified round bar structure.
2. The insert pin manufacturing method according to claim 1, wherein in S10, the steel material is 8407 special steel.
3. The insert manufacturing method according to claim 1, wherein in S20, the roughing is one or a combination of rough turning, rough planing, rough milling, drilling, and rasping.
4. The insert pin manufacturing method according to claim 1, wherein at S20, the surface hardness of the round bar structure differs from the internal hardness of the round bar structure by HRC 5.
5. The insert pin manufacturing method according to claim 1, wherein in S20, the surface hardness of the round bar structure is HRC 47-48.
6. The insert pin manufacturing method of claim 1, wherein in S20, the internal hardness of the round bar structure is HRC 47-48.
7. The insert manufacturing method according to claim 1, wherein in S40, the white corundum abrasive grain number is greater than 80# and less than 200 #; in S50, the white corundum grinding wheel has a mesh number of 200# or more and 500# or less.
8. The insert manufacturing method according to claim 1, wherein in S40, the mesh number of the white corundum grinding wheel is 120 #; in S50, the white corundum grinding wheel has a mesh number of 240 #.
9. The insert pin manufacturing method of claim 1, wherein a single-side grinding margin of 0.01mm is reserved in S40.
10. The insert pin manufacturing method according to claim 1, wherein in S60, the magnification of the magnifying glass is 50 times.
CN202210501930.XA 2022-05-09 2022-05-09 Method for manufacturing insert pin Pending CN114799760A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202210501930.XA CN114799760A (en) 2022-05-09 2022-05-09 Method for manufacturing insert pin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202210501930.XA CN114799760A (en) 2022-05-09 2022-05-09 Method for manufacturing insert pin

Publications (1)

Publication Number Publication Date
CN114799760A true CN114799760A (en) 2022-07-29

Family

ID=82513555

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202210501930.XA Pending CN114799760A (en) 2022-05-09 2022-05-09 Method for manufacturing insert pin

Country Status (1)

Country Link
CN (1) CN114799760A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4760668A (en) * 1986-07-02 1988-08-02 Alfred Schlaefli Surface grinding machine and method
CN105922013A (en) * 2016-04-22 2016-09-07 太仓市东晖机械厂 Cutting-grinding integrated machine
CN206254041U (en) * 2016-11-29 2017-06-16 深圳天珑无线科技有限公司 Pin processing unit (plant)
CN107350903A (en) * 2017-09-12 2017-11-17 苏州沃思诺自动化科技有限公司 A kind of grinding machine processing technology for improving mold surface finish
CN109483330A (en) * 2018-10-26 2019-03-19 无锡市普高精密机械科技有限公司 A kind of preparation method and its detection device of red needle
CN110814668A (en) * 2019-12-04 2020-02-21 广州市型腔模具制造有限公司 Mold insert pin machining process

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4760668A (en) * 1986-07-02 1988-08-02 Alfred Schlaefli Surface grinding machine and method
CN105922013A (en) * 2016-04-22 2016-09-07 太仓市东晖机械厂 Cutting-grinding integrated machine
CN206254041U (en) * 2016-11-29 2017-06-16 深圳天珑无线科技有限公司 Pin processing unit (plant)
CN107350903A (en) * 2017-09-12 2017-11-17 苏州沃思诺自动化科技有限公司 A kind of grinding machine processing technology for improving mold surface finish
CN109483330A (en) * 2018-10-26 2019-03-19 无锡市普高精密机械科技有限公司 A kind of preparation method and its detection device of red needle
CN110814668A (en) * 2019-12-04 2020-02-21 广州市型腔模具制造有限公司 Mold insert pin machining process

Similar Documents

Publication Publication Date Title
KR100845873B1 (en) Method for producing forging die
US20080236341A1 (en) Powdered metal multi-lobular tooling and method of fabrication
CN102825438B (en) Processing method of four-station concave die
CN105499924A (en) Machining method for molding lower die body of die of pulling ring of ring-pull can
CN104057269B (en) A kind of processing technique of the drift of hard alloy top hammer shaping mould
CN102554113B (en) Precise forming method of high-temperature alloy mounting seat
JPWO2013054436A1 (en) Method for manufacturing a valve for an internal combustion engine
CN105458135A (en) Alloy piece forging technology
CN107598128A (en) The manufacturing process of high-effect wheel hub mold
CN108746375B (en) Method for preparing hot stamping die insert based on electric arc additive and laser cladding
CN114799760A (en) Method for manufacturing insert pin
CN109274231B (en) Machining process for producing motor shell by using titanium metal
CN111496254B (en) Die cooling insert and manufacturing method thereof
CN104175081A (en) Method for machining female mold for countersunk head angle rivet
JP5575991B2 (en) Method for manufacturing a valve for an internal combustion engine
CN110997190B (en) Method for producing a sintered component and sintered component
CN112281156B (en) Laser casting repair method for conformal mold
JP5610124B2 (en) Forming tool processing method
CN107953080A (en) Magnetron molybdenum conically shaped processing method
JP2002035884A (en) Gear die for warm or hot forging and manufacturing method thereof
CN110814668A (en) Mold insert pin machining process
CN114269495B (en) Sintered gear and method for manufacturing sintered gear
CN209664436U (en) A kind of broaching tool
CN114161089B (en) Processing method of thin-wall aluminum connecting piece
CN108757560B (en) Aluminum alloy fan blade and manufacturing method thereof

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