CN102312055B - Anti-deformation method of flat casting - Google Patents

Anti-deformation method of flat casting Download PDF

Info

Publication number
CN102312055B
CN102312055B CN 201110295417 CN201110295417A CN102312055B CN 102312055 B CN102312055 B CN 102312055B CN 201110295417 CN201110295417 CN 201110295417 CN 201110295417 A CN201110295417 A CN 201110295417A CN 102312055 B CN102312055 B CN 102312055B
Authority
CN
China
Prior art keywords
casting
foundry goods
false boss
height
boss
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.)
Active
Application number
CN 201110295417
Other languages
Chinese (zh)
Other versions
CN102312055A (en
Inventor
张丙岩
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.)
AECC Shenyang Liming Aero Engine Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group 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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN 201110295417 priority Critical patent/CN102312055B/en
Publication of CN102312055A publication Critical patent/CN102312055A/en
Application granted granted Critical
Publication of CN102312055B publication Critical patent/CN102312055B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)

Abstract

The invention relates to an anti-deformation method of a flat casting. By arranging one or several technological shores, bending-resistant ribs, and technological salient points during casting, and through deformation automatic correction after shaping of a casting, the method can produce the qualified casting. The anti-deformation measure of the method and the casting shaping in one body occur simultaneously, with no need for manual cold correction or hot correction. Meanwhile, a fluorescence or coloring inspection after correction can be omitted, thus greatly reducing the cost and enhancing the casting qualification rate.

Description

A kind of Anti-deformation method of flat casting
Technical field
The invention belongs to the sand mold casting technical field, particularly a kind of Anti-deformation method of flat casting.
Background technology
Large two dimensional structure foundry goods metamorphism very easily occurs in casting, heat treatment process, and deformation extent is serious, the routine techniques means are to adopt the auxiliary mould anchor clamps to prevent casting deformation, expense is many, the problems such as delivery cycle are produced in prolongation but the manufacturing anchor clamps exist, thermal treatment is come out of the stove and is proofreaied and correct unfavorable operation factors and operate miss, the crackle hidden danger etc. that also have hot environment in addition, cold sizing or thermal recalibration all must guarantee certain skills involved in the labour simultaneously secondary fluorescence or colour check(test) operation, and qualification rate is lower.
Summary of the invention
In casting or heat treatment process, under the factor affecting such as the heat affected zone of the larger weak point of wall thickness variation, final set and foundry goods convergent force, on-fixed core, easily produce the defective of distortion for the plate class casting of existing large two dimensional structure, the invention provides a kind of Anti-deformation method of flat casting, by technique pillar stiffener, counter-bending rib, technique salient point are set in the cast casting process, be out of shape correction behind the casting forming again and obtain qualified foundry goods, the concrete technology step is as follows:
1) hollow position arranges a place or many places technique pillar stiffener in the middle of foundry goods, and height is concordant with the large plane of foundry goods, and technique supports
Column diameter coupling casting dimension guarantees enough flexural strengths, all technique pillar stiffeners usually after heat treating castings, send before processing remove, special yielding thin-section casting remains into machining finish before removal;
2) at foundry goods yielding position internal surface and/or outside surface counter-bending rib is set, counter-bending rib thickness is got foundry goods basic framework size, and guarantees to be convenient to remove;
3) the large uniform plane in bottom of preparing the thermal treatment horizontal positioned at foundry goods arranges false boss, and the false boss width is near casting section thickness, and the salient point of height and foundry goods is consistent, makes foundry goods depression position and all the other large planar technology boss height polishings;
4) press former horizontal reference scribing inspection after the casting, mark sea line in one week of false boss, remove the false boss surplus and obtain an ideal plane, local little surplus distortion is adjusted this position false boss height by processing and is revised, and the corrected altitude of false boss equals this position deflection.
The invention has the beneficial effects as follows: the method is that preventing deformation measure and foundry goods are simultaneously integrally formed, does not need manual cold sizing or thermal recalibration, and fluorescence or colour check(test) after also not needing to proofread and correct have greatly reduced cost and improved casting qualified rate.
Description of drawings
Fig. 1 is the casting structure schematic diagram of the embodiment of the invention;
Fig. 2 is the vertical view of Fig. 1;
Fig. 3 is the upward view of Fig. 1;
Among the figure: the yielding position of 1 foundry goods, 2 counter-bending ribs, 3 technique pillar stiffeners, 4 false bosses.
Embodiment
The present invention is further described below in conjunction with drawings and Examples.
Anti-deformation method of flat casting provided by the invention, for the yielding position 1 of foundry goods of structure as shown in Figure 1, the preventing deformation concrete technology step of implementing is as follows:
1) hollow position arranges two place's technique pillar stiffeners 3 in the middle of foundry goods, height is concordant with the large plane of foundry goods, technique pillar stiffener 3 diameters are selected according to the foundry goods size, guarantee enough flexural strengths, the formation center subsides when preventing foundry goods roughing or thermal treatment, all technique pillar stiffeners 3 are observed itself and platform gap after thermal treatment, remove after the machining that does not deform finishes;
2) at the yielding position of foundry goods outside surface counter-bending rib 2 is set, counter-bending rib 2 thickness are got foundry goods basic framework size,
And guarantee to be convenient to remove;
3) prepare the large plane layout false boss 4 in bottom of thermal treatment horizontal positioned at foundry goods, false boss 4 width are near casting section thickness, and the salient point of height and foundry goods is consistent, makes highly polishings of the large planar technology boss 4 of foundry goods depression position and all the other;
4) press former horizontal reference scribing inspection after the casting, mark sea line in 4 one weeks of false boss, remove the false boss surplus and obtain an ideal plane, local little surplus distortion is adjusted high 4 degree of this position false boss by processing and is revised, the position that is bent upwards keeps large as far as possible plane, and boss height 4 is constant on one side, reduce the other side false boss 4 height, the height of middle process boss 4 is reduced at reclinate position, and the corrected altitude of false boss 4 equals this position deflection.
After revise adjusting foundry goods placed and prepare thermal treatment on the cast iron platform, privileged sites, discontinuous position auxiliary weight, the weight set-point selects the below that the position of technique point of suppon is arranged.By the enforcement of above-mentioned anti-deformation method, the metamorphism of foundry goods can be restored in heat treatment process automatically.

Claims (1)

1. Anti-deformation method of flat casting is characterized in that: by technique pillar stiffener, counter-bending rib, false boss are set in the cast casting process, are out of shape behind the casting forming to revise again and obtain qualified foundry goods, the concrete technology step is as follows:
1) hollow position arranges a place or many places technique pillar stiffener in the middle of foundry goods, and height is concordant with the large plane of foundry goods, and technique pillar stiffener diameter coupling casting dimension guarantees enough flexural strengths;
2) at foundry goods yielding position internal surface and/or outside surface counter-bending rib is set, counter-bending rib thickness is got foundry goods basic framework size, and guarantees to be convenient to remove;
3) prepare the large plane layout false boss in bottom of thermal treatment horizontal positioned at foundry goods, the false boss width is near casting section thickness, and the salient point of height and foundry goods is consistent, makes foundry goods depression position and all the other large planar technology boss height polishings;
4) press former horizontal reference scribing inspection after the casting, mark sea line in one week of false boss, remove the false boss surplus and obtain an ideal plane, local little surplus distortion is adjusted this position false boss height by processing and is revised, and the corrected altitude of false boss equals this position deflection.
CN 201110295417 2011-09-30 2011-09-30 Anti-deformation method of flat casting Active CN102312055B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201110295417 CN102312055B (en) 2011-09-30 2011-09-30 Anti-deformation method of flat casting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201110295417 CN102312055B (en) 2011-09-30 2011-09-30 Anti-deformation method of flat casting

Publications (2)

Publication Number Publication Date
CN102312055A CN102312055A (en) 2012-01-11
CN102312055B true CN102312055B (en) 2013-02-27

Family

ID=45425622

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201110295417 Active CN102312055B (en) 2011-09-30 2011-09-30 Anti-deformation method of flat casting

Country Status (1)

Country Link
CN (1) CN102312055B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105436391A (en) * 2015-12-30 2016-03-30 无锡透平叶片有限公司 Cooling and deformation prevention tooling used after forging large-sized titanium alloy grid beam forge piece
CN108374075B (en) * 2018-03-12 2019-11-15 包头北方安全防护装备制造有限公司 The method for controlling large-scale armour plate brake forming part quenching distortion
CN111890078A (en) * 2020-07-24 2020-11-06 都江堰川相铝业有限公司 Manufacturing process of machine oil pump shell

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101462149B (en) * 2009-01-15 2011-08-10 洛阳市兴荣工业有限公司 Foundry technique method of lower support board of ball type support
CN101537624A (en) * 2009-04-09 2009-09-23 江苏万盛铸造有限公司 Manufacturing process of robot joints

Also Published As

Publication number Publication date
CN102312055A (en) 2012-01-11

Similar Documents

Publication Publication Date Title
CN100364693C (en) Casting method for exhaust branch pipe of thin-wall ball iron triplet
CN103846392B (en) The casting method of spheroidal graphite cast-iron knuckle
CN107282892A (en) A kind of 3D printing core formative method of aluminium alloy castings
CN102312055B (en) Anti-deformation method of flat casting
CN103302242A (en) Precise casing method of tiles of floating wall of combustion chamber of aeroengine
CN104195448B (en) Casting alloy material and the technique casting ocean platform canine tooth roller box foundry goods with it
CN201231310Y (en) Low-segregation large-size ingot obtaining device through quickening the cooling of the bottom, lateral wall
CN104174819B (en) The climb casting technique of machine third-level planetary frame of a kind of ocean platform
CN103894550B (en) Contiuum type copper alloy propeller hub Casting Equipment and special method thereof
CN102392114A (en) Thermal calibration method for precisely cast structural pieces of cartridge receiver
CN102513512A (en) Integral mold casting method for resin sand of support piece of bulldozer
CN101380663B (en) Precision casting method of lost foam hollow-shell
CN104858365A (en) Integral casting production method of water-cooled furnace mouth
CN109719241B (en) Short-process casting and forging integrated process for steel
CN103949584A (en) Sand mold casting method for medium-pressure 22nd-stage stationary blade of H-stage combined cycle turbine
CN111822677A (en) Light metal casting method based on composite casting mold
CN107876704B (en) A kind of big mould group casting and molding method of low cost
CN205927014U (en) Return bend sand -lined metal mold mould
CN104985133A (en) Inblock cast producing method of large-sized long-strip box body provided with long-strip cavity
CN1311941C (en) Method for quick changing bottom inlet of intermediate ladle
CN110252954A (en) The casting method for preventing high alloy cast steel ingate root from cracking
CN102527941A (en) Pouring process of aluminum alloy air intake manifold
CN105964920A (en) White die casting process for ductile iron casting
CN210412416U (en) Novel high-strength atmospheric pressure riser device
CN107952934A (en) A kind of stent and application method for being used in model casting be segmented wax pattern splicing

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
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company

Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City