CN109440033B - Process method for eliminating residual stress of arc-shaped forge piece - Google Patents

Process method for eliminating residual stress of arc-shaped forge piece Download PDF

Info

Publication number
CN109440033B
CN109440033B CN201811628398.8A CN201811628398A CN109440033B CN 109440033 B CN109440033 B CN 109440033B CN 201811628398 A CN201811628398 A CN 201811628398A CN 109440033 B CN109440033 B CN 109440033B
Authority
CN
China
Prior art keywords
arc
die
shaped
residual stress
forge piece
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
CN201811628398.8A
Other languages
Chinese (zh)
Other versions
CN109440033A (en
Inventor
刘强
吴道祥
陈焕良
李丹丹
曾庆华
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.)
Southwest Aluminum Group Co Ltd
Original Assignee
Southwest Aluminum 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 Southwest Aluminum Group Co Ltd filed Critical Southwest Aluminum Group Co Ltd
Priority to CN201811628398.8A priority Critical patent/CN109440033B/en
Publication of CN109440033A publication Critical patent/CN109440033A/en
Application granted granted Critical
Publication of CN109440033B publication Critical patent/CN109440033B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon

Landscapes

  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Forging (AREA)

Abstract

The invention discloses a process method for eliminating residual stress of an arc-shaped forge piece, which comprises the following steps: 1) carrying out primary cold compression on the die forging; 2) and carrying out secondary cold compression on the die forging. By the process method, the residual stress of the arc-shaped forge piece can be effectively eliminated, the operation difficulty is low, and the cost is low.

Description

Process method for eliminating residual stress of arc-shaped forge piece
Technical Field
The invention relates to the technical field of aeronautical machinery, in particular to a process method for eliminating residual stress of an arc-shaped forge piece.
Background
The large-scale T-shaped section arc-shaped forge piece is used as a bearing structural part of an airplane, is easy to deform after quenching and has large residual stress, and generates severe machining deformation during machining, so that cold deformation is needed to achieve the purposes of correcting and eliminating the residual stress.
At present, the tensile method elimination residual stress of the general adoption profiling of foreign countries, but need large-scale tensile equipment, the input is great, under the condition that lacks large-scale tensile equipment, when adopting one set of mould to carry out cold compression to this type of forging, especially when compressing the fillet, the fillet is extremely sensitive to compression deformation, and requirement to compression precision is high, and is difficult to control, and takes place the card mo easily, if keep away the fillet position, then the stress of forging cross department can not obtain effective release, and is extremely unsatisfactory to residual stress's elimination effect.
Therefore, how to provide a process method for eliminating residual stress of an arc-shaped forge piece not only can effectively eliminate the residual stress, but also has small operation difficulty and low cost, and is a technical problem which needs to be solved by technical personnel in the field.
Disclosure of Invention
In view of this, the invention aims to provide a process method for eliminating residual stress of an arc-shaped forge piece, which can effectively eliminate the residual stress, and has small operation difficulty and low cost.
In order to achieve the above purpose, the invention provides the following technical scheme:
a process method for eliminating residual stress of an arc-shaped forge piece comprises the following steps:
1) carrying out primary cold compression on the die forging;
2) and carrying out secondary cold compression on the die forging.
Preferably, in the step 1), the die forging is subjected to cold compression by using a planar upper die and a planar lower die.
Preferably, in the step 1), the planar upper die and the planar lower die each include a plane for contacting the die forging.
Preferably, in the step 2), the die forging is subjected to cold compression by adopting an arc-shaped cold-pressing upper die and an arc-shaped cold-pressing lower die.
Preferably, in the step 2), the arc-shaped upper cold press die and the arc-shaped lower cold press die both comprise arc-shaped surfaces used for contacting with the die forging.
Preferably, the die forging is a die forging with a T-shaped section, or a die forging with an I-shaped section.
According to the technical scheme, the process method for eliminating the residual stress of the arc-shaped forge piece disclosed by the embodiment of the invention comprises the following steps: 1) carrying out primary cold compression on the die forging; 2) and carrying out secondary cold compression on the die forging. By the process method, the residual stress of the arc-shaped forge piece can be effectively eliminated, the operation difficulty is low, and the cost is low.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the description of the embodiments or the prior art are briefly introduced below, it is obvious that the drawings in the following description are only embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the provided drawings without creative efforts.
FIG. 1 is a schematic flow chart of a process for eliminating residual stress of an arc-shaped forge piece disclosed by the embodiment of the invention;
FIG. 2 is a schematic view of a primary cold compression configuration disclosed in an embodiment of the present invention;
FIG. 3 is a schematic structural view of a secondary cold compression disclosed in an embodiment of the present invention;
fig. 4 is a schematic structural diagram of the position of the secondary cold compression disclosed by the embodiment of the invention.
Wherein, each part name is as follows:
1-die forging, 2-flat upper die, 3-flat lower die, 4-arc cold-pressing upper die and 5-arc cold-pressing lower die.
Detailed Description
In view of the above, the core of the invention is to provide a residual stress eliminating process method for an arc-shaped forging, which can effectively eliminate residual stress, and has small operation difficulty and low cost.
In order that those skilled in the art will better understand the disclosure, the following detailed description will be given with reference to the accompanying drawings and the detailed description.
The process method for eliminating the residual stress of the arc-shaped forge piece disclosed by the embodiment of the invention comprises the following steps: 1) carrying out primary cold compression on the die forging 1; 2) and carrying out secondary cold compression on the die forging 1. By the process method, the residual stress of the arc-shaped forge piece can be effectively eliminated, the operation difficulty is low, and the cost is low.
In step 1), the die forging 1 is subjected to primary cold compression by using a flat upper die 2 and a flat lower die 3. The upper flat die 2 and the lower flat die 3 are both made of metal materials, and the surfaces for contacting the die forging 1 are both the plane of the upper flat die 2 and the plane of the lower flat die 3.
It should further be noted that, after carrying out primary cold compression to the die forging 1, carry out secondary cold compression to the die forging 1 again, when carrying out secondary cold compression, need adopt arc to coldly press last mould 4 and arc to coldly press lower mould 4 and carry out cold compression, wherein, arc is coldly pressed last mould 4 and arc and is coldly pressed lower mould 4 and all adopts the metal material to make, arc is coldly pressed last mould 4 and arc and is coldly pressed lower mould 5 and all is included the arcwall face that is used for contacting with die forging 1, the arcwall face and the arc die forging 1 profile modeling setting of arc cold pressing last mould 4 and arc cold pressing lower mould 5, after the arcwall face through arc cold pressing last mould 4 and the arcwall face of arc cold pressing lower mould 5 and the upper and lower two sides of die forging 1 contact respectively, carry out secondary cold compression to die.
Certainly, the die forging 1 can be used for manufacturing a finished product meeting the quality requirement at a proper temperature, and in the process method for eliminating the residual stress of the arc forging provided by the embodiment of the invention, the temperature for realizing primary cold compression and the temperature for realizing secondary cold compression are both cold compression at normal temperature.
It should be noted that the specific shape of the die forging 1 is not limited, and in the process method for eliminating the residual stress of the arc-shaped forging disclosed in the embodiment of the present invention, the die forging 1 is preferably a T-shaped cross-section die forging or an i-shaped cross-section die forging, and particularly, the technical effect achieved by the large-sized T-shaped cross-section die forging using the process method disclosed in the embodiment of the present invention is better.
The embodiments in the present description are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims (2)

1. A process method for eliminating residual stress of an arc-shaped forge piece is characterized by comprising the following steps:
1) carrying out primary cold compression on the die forging (1);
2) carrying out secondary cold compression on the die forging (1);
in the step 1), cold compression is carried out on the die forging (1) by adopting a plane upper die (2) and a plane lower die (3); in the step 1), the plane upper die (2) and the plane lower die (3) both comprise planes used for being in contact with the die forging (1);
in the step 2), an arc-shaped cold pressing upper die (4) and an arc-shaped cold pressing lower die (5) are adopted to carry out cold compression on the die forging piece (1); in the step 2), the arc cold pressing upper die (4) and the arc cold pressing lower die (5) both comprise arc-shaped surfaces used for being in contact with the die forging (1).
2. The process for eliminating the residual stress of the arc-shaped forge piece according to the claim 1, characterized in that the die forge piece (1) is a T-shaped section die forge piece or an I-shaped section die forge piece.
CN201811628398.8A 2018-12-28 2018-12-28 Process method for eliminating residual stress of arc-shaped forge piece Active CN109440033B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811628398.8A CN109440033B (en) 2018-12-28 2018-12-28 Process method for eliminating residual stress of arc-shaped forge piece

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811628398.8A CN109440033B (en) 2018-12-28 2018-12-28 Process method for eliminating residual stress of arc-shaped forge piece

Publications (2)

Publication Number Publication Date
CN109440033A CN109440033A (en) 2019-03-08
CN109440033B true CN109440033B (en) 2020-06-09

Family

ID=65542230

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811628398.8A Active CN109440033B (en) 2018-12-28 2018-12-28 Process method for eliminating residual stress of arc-shaped forge piece

Country Status (1)

Country Link
CN (1) CN109440033B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112705658A (en) * 2020-12-28 2021-04-27 西南铝业(集团)有限责任公司 Arc-shaped forge piece machining system and machining method
CN113215505B (en) * 2021-03-22 2022-05-03 湖南大学 Method for eliminating residual stress of annular special-shaped forge piece
CN115446610B (en) * 2022-07-21 2023-07-21 成都飞机工业(集团)有限责任公司 Method for eliminating residual stress by cold pressing

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6289543A (en) * 1985-10-15 1987-04-24 Kobe Steel Ltd Cold compressing method for relieving residual stress
JP2003211248A (en) * 2002-01-21 2003-07-29 Kobe Steel Ltd Die for cold compression, and method for removing residual stress of stamp forging
CN102513780A (en) * 2011-12-22 2012-06-27 西南铝业(集团)有限责任公司 Forging process of large forged ring
CN106734790A (en) * 2016-12-03 2017-05-31 贵州航天新力铸锻有限责任公司 The forging molding process of v-shaped cavity forging

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6289543A (en) * 1985-10-15 1987-04-24 Kobe Steel Ltd Cold compressing method for relieving residual stress
JP2003211248A (en) * 2002-01-21 2003-07-29 Kobe Steel Ltd Die for cold compression, and method for removing residual stress of stamp forging
CN102513780A (en) * 2011-12-22 2012-06-27 西南铝业(集团)有限责任公司 Forging process of large forged ring
CN106734790A (en) * 2016-12-03 2017-05-31 贵州航天新力铸锻有限责任公司 The forging molding process of v-shaped cavity forging

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
7050铝合金H型截面长轴锻件成形工艺优化及淬火残余应力消除研究;吴道祥;《中国博士学位论文全文数据库 工程科技Ⅰ辑》;20170315;97页图6.5和第98页 *

Also Published As

Publication number Publication date
CN109440033A (en) 2019-03-08

Similar Documents

Publication Publication Date Title
CN109440033B (en) Process method for eliminating residual stress of arc-shaped forge piece
EP3663012A1 (en) Press molded article manufacturing method
CN104117624A (en) Cold heading manufacturing method for connection bolt of ignition switch and die
CN104213059B (en) Titanium alloy bilayer curved surface wing plate part method for controlling heat treatment deformation
CN103212634B (en) The method for designing of rubber shaping male bend limit multistep mould and forming surface thereof
JPWO2008111118A1 (en) Method for manufacturing ring-shaped member
CN102921755A (en) Right angle extrusion processing method and right angle extrusion processing mould
TW201545825A (en) Formed material manufacturing method and formed material
CN105414233A (en) Backward extrusion die with back pressure and processing technology adopting same
JP2017164755A (en) Manufacturing method for press-molded article and press-molded article
JPH11294481A (en) Gear for integral type transmission and molding thereof
US20150047406A1 (en) Method of reducing wrinkles in pressed sheet metal components
US20170072455A1 (en) Burr-freebolt forging mould
JP2014166645A (en) Method for manufacturing metallic structure material
CN115740313A (en) Machining process of conical forge piece
JP2010201495A (en) Method for manufacturing connecting rod, and coining die apparatus used therefor
KR102086366B1 (en) Forging Method With Adjustable Width And Length For Thick Slab
US3000251A (en) Die and method of making same
JP2003211248A (en) Die for cold compression, and method for removing residual stress of stamp forging
KR20200030039A (en) Forging Method With Adjustable Width And Length For Thick Slab
KR101603597B1 (en) Form rolling die of gear
KR101841233B1 (en) Press die for forming a bolt portion or a nut portion on products
KR102348556B1 (en) Roll Forging Apparatus
CN108043933A (en) Automatic hole flanging demoulding mechanism and machine tool
CN210497906U (en) Porous stamping die of pipe fitting preface

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
GR01 Patent grant
GR01 Patent grant