CN203061806U - Casting mould of aluminium alloy bearing ring - Google Patents

Casting mould of aluminium alloy bearing ring Download PDF

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Publication number
CN203061806U
CN203061806U CN 201220702507 CN201220702507U CN203061806U CN 203061806 U CN203061806 U CN 203061806U CN 201220702507 CN201220702507 CN 201220702507 CN 201220702507 U CN201220702507 U CN 201220702507U CN 203061806 U CN203061806 U CN 203061806U
Authority
CN
China
Prior art keywords
casting
bearing ring
mould
ways
bearer ring
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
CN 201220702507
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Chinese (zh)
Inventor
刘健
王昌明
程国栋
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.)
Guizhou Aerospace Fenghua Precision Equipment Co Ltd
Original Assignee
Guizhou Aerospace Fenghua Precision Equipment 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 Aerospace Fenghua Precision Equipment Co Ltd filed Critical Guizhou Aerospace Fenghua Precision Equipment Co Ltd
Priority to CN 201220702507 priority Critical patent/CN203061806U/en
Application granted granted Critical
Publication of CN203061806U publication Critical patent/CN203061806U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a casting mould of an aluminium alloy bearing ring, and the casting mould comprises a bearing ring mould, transverse casting ways and straight casting ways, wherein the transverse casting ways are fixedly connected at the lower end of the bearing ring mould and arranged in a radial manner; the straight casting ways are arranged in the centre of the transverse casting ways; the bearing ring mould is a hollow cylindrical structure with a small upper part and a large lower part; and furthermore, the height of the bearing ring mould is 3.5 times of that of a finished bearing ring. By using the casting mould disclosed by the utility model, cast pieces of three bearing rings can be completed through one-time casting; after being sized, the whole cast piece is cut into single bearing ring cast pieces through machining, therefore, the casting efficiency is effectively increased; and the waste problems of raw materials and energy caused by re-melting remained furnace burden after traditional casting are solved.

Description

A kind of casting die of aluminum alloy bearing ring
Technical field
The utility model relates to a kind of casting die of aluminum alloy bearing ring, belongs to casting technology field.
Background technology
Aluminum alloy bearing ring external diameter is big, and height dimension is little, and casting system is arranged inconvenience, even if casting place finished product can not effectively guarantee product quality; For guaranteeing end product quality and the precision of aluminum alloy bearing ring, the general method that adopts the pressure reduction casting, but adopt pressure reduction method pouring cast part, each stove furnace charge can only be poured into a mould a foundry goods, after pouring a foundry goods, the residue furnace charge must return melting again in the heating furnace, and raw material and the energy are all caused serious waste.
The utility model content
The purpose of this utility model is: a kind of casting die of aluminum alloy bearing ring is provided, and to solve in traditional bearer ring casting system the stove furnace charge foundry goods of can only casting, casting efficient is low, raw material and the serious problem of energy waste.
The purpose of this utility model is achieved by following technical solution:
A kind of casting die of aluminum alloy bearing ring, comprise the bearer ring mould, be fixed in being of bearer ring mould lower end radial cross gate of arranging and be arranged in the sprue at cross gate center, wherein: described bearer ring mould is up-small and down-big hollow cylinder, and highly be 3.5 times of finished product bearer ring height, three bearer rings of can once casting, effectively promote casting efficient, saved raw material and the energy.
Described bearer ring mould inwall is provided with a hollow cylinder chill that highly is lower than the bearer ring mould, defectives such as that chill can partly produce the bearer ring part is loose, shrinkage cavity are passed to the direction away from chill, have effectively promoted qualification rate and the dimensional accuracy of finished product bearer ring.
Described bearer ring mould upper end is connected with reinforcement, and it can prevent the casting deformation that foundry goods causes because of cooling velocity difference.
Described reinforcement is " ten " font, and this method for arranging structure is firm, the cost performance height.
Compared with prior art, the casting die of the aluminum alloy bearing ring that the utility model provides, use this mould once to cast and to finish three bearer ring foundry goods, by machined whole foundry goods is cut into single bearer ring foundry goods again after the typing, it has effectively promoted casting efficient, guarantee the dimensional accuracy of processed finished products, solved residue furnace charge after traditional casting and needed raw material that melting again causes and the waste of the energy.
Description of drawings
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of the utility model axis carrier ring mould;
Fig. 3 is the A-A cutaway view of Fig. 2;
Among the figure: 1-chill, 2-reinforcement, 3-cross gate, 4-sprue, 5-bearer ring mould.
The specific embodiment
Below in conjunction with accompanying drawing the technical solution of the utility model is further described, but that scope required for protection is not limited to is described:
As Fig. 1, shown in 2 and 3, the casting die of the aluminum alloy bearing ring that the utility model provides, it comprises bearer ring mould 5, be fixed in being of bearer ring mould 5 lower ends radial cross gate of arranging 3 and be arranged in the sprue 4 at cross gate 3 centers, wherein: described bearer ring mould 5 is up-small and down-big hollow cylinder, and highly be 3.5 times of finished product bearer ring height, lower end diameter is bigger, be process allowance, three bearer rings of can once casting, become the bearer ring of three calibrated altitudes after the typing again through machine cuts, effectively promote casting efficient, saved raw material and the energy.
Described bearer ring mould 5 inwalls are provided with a hollow cylinder chill 1 that highly is lower than bearer ring mould 5, defectives such as that chill 1 can partly produce the bearer ring part is loose, shrinkage cavity are passed to the direction away from chill 1, loose and shrinkage cavity is then stayed on the process allowance, remove after the turning, effectively promoted qualification rate and the dimensional accuracy of finished product bearer ring.
Because cooling velocities such as foundry goods differing heights position, appearance and inside there are differences, foundry goods can cause foundry goods generation distortion in various degree in the bigger casting stress of the inner generation of foundry goods after the cooling fully inevitably.For guaranteeing that the described bearer ring mould of casting dimension accuracy 5 upper ends are connected with reinforcement 2, it can prevent the casting deformation that foundry goods causes because of cooling velocity difference, has effectively guaranteed the dimensional accuracy of foundry goods.
Described reinforcement is " ten " font, and this method for arranging structure is firm, and the cost performance height can guarantee that dimensional accuracy is cheap again, and in the heat treatment artificial aging, after stress elimination or the homogenizing, cutting is removed through machining processes, can further save the energy and cost.

Claims (4)

1. the casting die of an aluminum alloy bearing ring, comprise bearer ring mould (5), be fixed in being radial cross gate of arranging (3) and being arranged in the sprue (4) at cross gate (3) center of bearer ring mould (5) lower end, it is characterized in that: described bearer ring mould (5) is up-small and down-big hollow cylinder, and highly is 3.5 times of finished product bearer ring height.
2. the casting die of aluminum alloy bearing ring according to claim 1 is characterized in that: described bearer ring mould (5) inwall is furnished with a hollow cylinder chill (1) that highly is lower than bearer ring mould (5).
3. the casting die of aluminum alloy bearing ring according to claim 1 is characterized in that: be connected with reinforcement (2) on the described bearer ring mould (5).
4. the casting die of aluminum alloy bearing ring according to claim 3, it is characterized in that: described reinforcement (2) is " ten " font.
CN 201220702507 2012-12-18 2012-12-18 Casting mould of aluminium alloy bearing ring Expired - Fee Related CN203061806U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220702507 CN203061806U (en) 2012-12-18 2012-12-18 Casting mould of aluminium alloy bearing ring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220702507 CN203061806U (en) 2012-12-18 2012-12-18 Casting mould of aluminium alloy bearing ring

Publications (1)

Publication Number Publication Date
CN203061806U true CN203061806U (en) 2013-07-17

Family

ID=48760632

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220702507 Expired - Fee Related CN203061806U (en) 2012-12-18 2012-12-18 Casting mould of aluminium alloy bearing ring

Country Status (1)

Country Link
CN (1) CN203061806U (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104550757A (en) * 2014-12-30 2015-04-29 宁夏共享装备有限公司 Cold iron and core rod combining device for casting of sand core of generator cylinder block and manufacturing method
CN105081230A (en) * 2015-09-02 2015-11-25 太仓市顺昌锻造有限公司 Annular casting mold
CN105436419A (en) * 2015-12-03 2016-03-30 内蒙古北方重工业集团有限公司 Space curve type casting anti-deformation box cage structure and machining method
CN107008866A (en) * 2017-06-22 2017-08-04 洛阳鹏起实业有限公司 A kind of manufacturing process of cylindrical work pieces
CN108237204A (en) * 2018-03-07 2018-07-03 衢州学院 A kind of aluminium alloy front end frame running gate system and manufacturing method
CN113560494A (en) * 2021-07-21 2021-10-29 贵州航天风华精密设备有限公司 Deformation-reducing casting method and structure for large aluminum-magnesium alloy thin-wall cabin

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104550757A (en) * 2014-12-30 2015-04-29 宁夏共享装备有限公司 Cold iron and core rod combining device for casting of sand core of generator cylinder block and manufacturing method
CN105081230A (en) * 2015-09-02 2015-11-25 太仓市顺昌锻造有限公司 Annular casting mold
CN105436419A (en) * 2015-12-03 2016-03-30 内蒙古北方重工业集团有限公司 Space curve type casting anti-deformation box cage structure and machining method
CN107008866A (en) * 2017-06-22 2017-08-04 洛阳鹏起实业有限公司 A kind of manufacturing process of cylindrical work pieces
CN108237204A (en) * 2018-03-07 2018-07-03 衢州学院 A kind of aluminium alloy front end frame running gate system and manufacturing method
CN108237204B (en) * 2018-03-07 2023-06-20 衢州学院 An aluminum alloy front frame pouring system and manufacturing method
CN113560494A (en) * 2021-07-21 2021-10-29 贵州航天风华精密设备有限公司 Deformation-reducing casting method and structure for large aluminum-magnesium alloy thin-wall cabin
CN113560494B (en) * 2021-07-21 2023-03-14 贵州航天风华精密设备有限公司 Deformation-reducing casting method and structure for large aluminum-magnesium alloy thin-wall cabin

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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: 20130717

Termination date: 20151218

EXPY Termination of patent right or utility model