CN108838904A - A method of reducing structural metallic materials joint made by flame welding residual stress - Google Patents

A method of reducing structural metallic materials joint made by flame welding residual stress Download PDF

Info

Publication number
CN108838904A
CN108838904A CN201810747439.9A CN201810747439A CN108838904A CN 108838904 A CN108838904 A CN 108838904A CN 201810747439 A CN201810747439 A CN 201810747439A CN 108838904 A CN108838904 A CN 108838904A
Authority
CN
China
Prior art keywords
gas
residual stress
weld seam
metallic materials
particle
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
CN201810747439.9A
Other languages
Chinese (zh)
Inventor
李文亚
邹阳帆
李娜
杨夏炜
徐雅欣
马铁军
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.)
Northwestern Polytechnical University
Original Assignee
Northwestern Polytechnical University
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 Northwestern Polytechnical University filed Critical Northwestern Polytechnical University
Priority to CN201810747439.9A priority Critical patent/CN108838904A/en
Publication of CN108838904A publication Critical patent/CN108838904A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24CABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C1/00Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods
    • B24C1/10Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods for compacting surfaces, e.g. shot-peening
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24BMACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B9/00Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor
    • B24B9/02Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor characterised by a special design with respect to properties of materials specific to articles to be ground
    • B24B9/04Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor characterised by a special design with respect to properties of materials specific to articles to be ground of metal, e.g. skate blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24CABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C5/00Devices or accessories for generating abrasive blasts
    • B24C5/02Blast guns, e.g. for generating high velocity abrasive fluid jets for cutting materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24CABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C7/00Equipment for feeding abrasive material; Controlling the flowability, constitution, or other physical characteristics of abrasive blasts
    • B24C7/0046Equipment for feeding abrasive material; Controlling the flowability, constitution, or other physical characteristics of abrasive blasts the abrasive material being fed in a gaseous carrier

Abstract

The present invention proposes a kind of method for reducing structural metallic materials joint made by flame welding residual stress, hit simultaneously using heat gas and high-velocity particles stream weld metal zone and its near, by generating compression in joint surface, improves stress distribution, improve joint fatigue intensity and service life.Particle size is hit mostly between 10-100 μm, and the acceleration of particle can realize that gas pressure is generally 1.5-3.5MPa, and particle speed can reach 400-1000m/s by high pressure compressed gas (helium, nitrogen or compressed air).Furthermore it can according to need and gas is preheated, preheating temperature is generally 200-600 DEG C.Method high speed particle is hit and the combination of hot gas shock effect, can be effectively reduced or eliminate component residual tension, improves joint mechanical property, member for prolonging service life.The present invention is other than being used to regulate and control the residual stress of structural metallic materials joint made by flame welding, it may also be used for the various welding point residual stress distributions for improving other materials, to improve the security reliability of connector.

Description

A method of reducing structural metallic materials joint made by flame welding residual stress
Technical field
The invention belongs to structural metallic materials interconnection technique fields, and in particular to a kind of reduction structural metallic materials fusion welding The method of head residual stress.
Background technique
Numerous industrial circles such as aerospace, petrochemical industry, automobile ship, pressure vessel, can be related to metal structure material Expect interconnection technique.In welding, local heating expansion in weld metal zone cannot freely be extended by the constraint from weld seam compared with distal part, So that weld metal zone is pressurized and generates plastic deformation;In subsequent cooling procedure, weld metal zone shrink, and by from weld metal zone compared with distal part Constraint cannot freely shorten, thus postwelding generate residual tension.The presence of residual tension can not only reduce holding for component Loading capability, can also precision to component and dimensional stability cause to significantly affect, meanwhile, residual tension is also to cause stress rotten Lose the principal element of cracking.Therefore, it is necessary to take necessary measure to reduce or eliminate residual stress.
Reducing or eliminating postwelding residual stress mainly uses following methods at present:
(1) hammering method:Using the position of steel hammer hammering workpiece residual stress concentrations, answer workpiece surface by the pressure hammered Power and local plastic deformation occurs, to reduce residual stress peak value, improve and balanced workpiece residual stress distribution.But the party The control of hitting dynamics is more difficult when method operates, and dynamics is excessive to be easy to cause processing hardening and weld cracking.
(2) heat treating process:It is heated by butt-welding fitting entirety or part to reduce stress, reducing effect depends primarily on Heating temperature, soaking time, weldment ingredient and tissue, cooling velocity etc..This method time-consuming is more, and is not suitable for larger part.
(3) vibratory drilling method:It is excited by vibration source and generates resonance, make to generate micro-plastic deformation inside metal structure to reduce Stress.This method device therefor is simple, and processing cost is low, and the time is short.But not being recommended to use is preventing fracture and stress corrosion On the structural member of failure.
(4) shot-peening method:Workpiece surface is bombarded using pellet and is implanted into residual compressive stress, improves workpiece fatigue strength.The party Method is low in cost, easy to operate, but workpiece surface roughness can be made to increase, and corrosion resistance is deteriorated, and working environment is severe, unit Yield is relatively low.
(5) disclosing application No. is 200910024032.4 patent a kind of reduces residual stress of ferromagnetic metal material Method achievees the effect that reduce residual stress by pulse current and pulse magnetic field treatment ferromagnetic metal material, but the party Method is only applicable to ferrimagnet, for nonferromugnetic material, cannot achieve the purpose for reducing residual stress.
(6) application No. is 93101690.8 patents to disclose a kind of dynamic control thin-plate element welding residual stress and change The technology of shape.In the welding process of thin-plate element, after being atomized cooling medium using high pressure gas, follow welding heat source to still Weld seam in the condition of high temperature carries out P-Coercive chilling.Exhaust tube by surrounding cooling medium nozzle is situated between cooling in time The steam of matter and remaining cooling medium are drained, and can control the internal stress and deformation of welding section.But this method to weld seam into When row forces chilling, it is easy to generate hardened structure in weld metal zone, or even crack, deteriorates joint performance.
(7) application No. is 201210248669.3 patent disclose it is a kind of using multi-pass welding interlayer welding waste heat it is auxiliary The method for helping vibration to reduce thick plates residual stress.By shake before scanning, under subresonance frequency adjust exciting force obtain to The intrinsic frequency of welder's part.After being soldered one layer, oscillating aging is carried out according to determining intrinsic frequency in the case where welding waste heat state It handles to reduce the residual stress of slab weldment.But this method is not especially bright for the reduction of thin plate postwelding residual stress It is aobvious, and it is directed to different materials, intrinsic frequency will be first determined before weldering, reduce production efficiency.
(8) it discloses a kind of holding intensity of aluminum alloy application No. is 201510295203.2 patent and reduces quenching remnants and answer The ageing hot processing method of power.Will solid solution, after quenched aluminium alloy directly carries out level-one artificial aging, then to carry out second level artificial Timeliness;Level-one timeliness is that aluminium alloy is carried out at least artificial aging in short-term three times, is come out of the stove air-cooled;Improve each artificial aging in short-term Heating rate generates the stress field opposite with quenching state and answers to offset remnants to obtain the temperature field opposite with quenching process Power.This method is particularly suitable for larger thickness, forging of regular shape and plate.But aluminium alloy is repeatedly made by heat during being somebody's turn to do With easily causing microstructure coarsening.
(9) application No. is 201610180639.1 patents to disclose a kind of externally-applied magnetic field device control argon tungsten-arc welding (TIG) system of connector residual stress.The electricity that longitudinal magnetic field acts on TIG weld is specifically generated by externally-applied magnetic field generating device Arc, the charged particle in electric arc rotate under the action of externally-applied magnetic field to electric arc edge, and electric arc becomes bell shape from cone, electricity Arc energy and current density become bimodal shape distribution, so as to cause the reduction of welding temperature field gradient, the distribution of welding residual stress Improve.But this method is only applicable to TIG weld connector, and the stress distribution of other Solid-State Welding connectors can not be regulated and controled.
Summary of the invention
Technical problems to be solved:
In order to avoid the shortcomings of the prior art, the present invention proposes that a kind of reduction structural metallic materials joint made by flame welding is remaining The method of stress, in particular to using the high-velocity particles stream with certain temperature hit weld metal zone and its near, by connector Surface generates compression, improves stress distribution, improves joint fatigue intensity and service life, while not will increase the surface of workpiece Roughness.This method operating procedure is simple and convenient, have many advantages, such as low cost, short route, efficiently it is convenient, be easy to large-scale industry Change application.
The technical scheme is that:A method of reducing structural metallic materials joint made by flame welding residual stress, feature It is:Concrete operation step is as follows,
Step 1:Face of weld is pre-processed:First with sand paper polishing metal material weld seam and pending area, to Remove impurity;Then the weld seam of metal material and the greasy dirt of pending area are removed with acetone or alcohol;
Step 2:Metallic is packed into powder feeder, the metal particle size is between 10-100 μm;
Step 3:High-pressure air source is connected, the acceleration gas pressure being passed through is 1.5-3.5MPa, and gas will be accelerated to pass through high pressure Gas source a part is passed through the powder feeder, for pushing the metallic, so that its speed is reached 400-1000m/s, is formed high Fast particle flux;Another part is passed through gas heater, and gas temperature is heated to 200-600 DEG C;
Step 4:Metal material is subjected to clamping by mechanical arm or mechanical device, it then will be described using processing rifle Acceleration gas after high-velocity particles stream and heating sprays simultaneously, hits the weld seam and pending area of metal material;
Step 5:Decide whether to repeat the above steps by stress mornitoring result.
A further technical scheme of the invention is that:The acceleration gas is helium, nitrogen or compressed air.
A further technical scheme of the invention is that:The metallic is Cu, Ni, W or stainless steel.
Beneficial effect
According to an embodiment of the invention, this method is hit using high-velocity particles stream and the combination of hot gas shock effect, weld seam And it after pending area is hit by high-velocity particles under the action of impacting with hot gas, is plastically deformed, stress obtains certain journey Degree release, can be effectively reduced or eliminate component residual tension;The load bearing ability of component gets a promotion, and improves weld seam power Performance is learned, fatigue strength increases substantially, and stress corrosion cracking is eased, member for prolonging service life.
Metallic selects size between 10-100 μm, in the weld seam on high-velocity particles stream striking work surface and to be processed It will not influence its roughness when region, while being easy to deposit when metallic formation high-velocity particles stream striking work surface, can mention High weld seam and pending area corrosion resistance;Method and process of the invention is simple compared with the existing technology, using processing rifle by institute State high-velocity particles stream and heating after acceleration gas and meanwhile spray, hit the weld seam and pending area of metal material, a step can Being completed at the same time reduces residual stress and raising corrosion resistance.The acceleration gas pressure being passed through is that 1.5-3.5MPa makes metallic When formation speed is 400-1000m/s high-velocity particles stream, workpiece weld seam and pending area is enabled to be plastically deformed, together When in weld seam and pending area generate compression, and then be effectively reduced or eliminate component residual tension.When gas temperature plus When heat arrives 200-600 DEG C, high-velocity particles stream may be implemented in the good deposition of workpiece surface to be processed, while the temperature is to workpiece Surface to be treated can generate certain annealing effect, which is also beneficial to the release of workpiece surface residual tension to be processed.
Detailed description of the invention
Fig. 1 is the principle of the present invention figure;
Fig. 2 is the working principle diagram of the embodiment of the present invention;
Description of symbols:1. powder feeder, 2. high-pressure air sources;3. gas heater;4. substrate;5. high-velocity particles stream;6. Handle rifle, 7. pending areas, 8. weld seams.
Specific embodiment
The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to be used to explain the present invention, and cannot understand For limitation of the present invention.
One, embodiment (one):
The processing method of the present embodiment includes the following steps:
(1) 2219 aluminium alloy plates (300mm × 150mm × 8mm) VPTIG weld seam is beaten with the sand paper of 70#-400# Mill, is degreased with acetone or alcohol, and pending area is that entire weld seam and weld seam two sides extend at 20mm to base material respectively;
(2) parameter selection:Metallic is Cu particle, and gas pressure 2.6MPa, preheating temperature is 400 DEG C, accelerates gas Body selects nitrogen;
(3) Cu particle is packed into powder feeder, connects high-pressure air source, nitrogen pressure reaches 2.6MPa, nitrogen is passed through high pressure Gas source a part is passed through the powder feeder, for pushing Cu particle, so that its speed is reached 400-1000m/s, forms high-velocity particles Stream;Another part is passed through gas heater, after gas temperature is heated to 400 DEG C;
(4) sample is carried out by clamping by mechanical arm or mechanical device, then uses processing rifle by the high-velocity particles Acceleration gas after stream and heating sprays simultaneously, hits the weld seam and pending area of metal material;
(5) circulation aforesaid operations are primary.
The result shows that:The peak stress of substrate is 152MPa when as-welded, hits the effect with hot gas impact in high-velocity particles Under, the stress distribution of substrate is improved, maximum stress 25MPa, and more presentation compressive stress states around weld seam.
Two, embodiment (two):
The processing method of this embodiment example includes the following steps:
(1) 2219 aluminium alloy plates (300mm × 150mm × 8mm) VPTIG weld seam is beaten with the sand paper of 70#-400# Mill, is degreased with acetone or alcohol, and pending area is that the entire weld seam of tow sides and weld seam two sides are prolonged to base material respectively It stretches at 20mm;
(2) parameter selection:Metallic is Cu particle, and gas pressure 2.0MPa, preheating temperature is 200 DEG C, accelerates gas Body selects nitrogen;
(3) Cu particle is packed into powder feeder, connects high-pressure air source, nitrogen pressure reaches 2.0MPa, nitrogen is passed through high pressure Gas source a part is passed through the powder feeder, for pushing Cu particle, so that its speed is reached 400-1000m/s, forms high-velocity particles Stream;Another part is passed through gas heater, and gas temperature is heated to 200 DEG C;
(4) sample is carried out by clamping by mechanical arm or mechanical device, then uses processing rifle by the high-velocity particles Acceleration gas after stream and heating sprays simultaneously, hits the weld seam and pending area of metal material;
(5) circulation aforesaid operations are primary.
The result shows that:The peak stress of substrate is 160MPa when as-welded, hits the effect with hot gas impact in high-velocity particles Under, the stress distribution of substrate is improved, and front maximum stress is 18MPa, and reverse side maximum stress is 6MPa, and more around weld seam Compressive stress state is presented.
Three, embodiment (three):
The processing method of this embodiment example includes the following steps:
(1) it is polished with the sand paper of 70#-400# 2024 aluminium alloy plates (300mm × 150mm × 4mm) TIG weld seam, It is degreased with acetone or alcohol, pending area is that entire weld seam and weld seam two sides extend at 20mm to base material respectively;
(2) parameter selection:Metallic is aluminium oxide particles, and gas pressure 2.6MPa, preheating temperature is 300 DEG C, is added Fast gas selects nitrogen;
(3) aluminium oxide particles are packed into powder feeder, connect high-pressure air source, nitrogen pressure reaches 2.6MPa, nitrogen is passed through High-pressure air source a part is passed through the powder feeder, for pushing aluminium oxide particles, so that its speed is reached 400-1000m/s, is formed High-velocity particles stream;Another part is passed through gas heater, and gas temperature is heated to 300 DEG C;
(4) sample is carried out by clamping by mechanical arm or mechanical device, then uses processing rifle by the high-velocity particles Acceleration gas after stream and heating sprays simultaneously, hits the weld seam and pending area of metal material;
(5) aforesaid operations are recycled twice.
The result shows that:As-welded peak stress is 103MPa, under the action of high-velocity particles hit and impact with hot gas, sample Stress distribution is improved, maximum stress 8MPa, and more presentation compressive stress states around weld seam.
Four, embodiment (four):
The processing method of this embodiment example includes the following steps:
(1) with the sand paper of 70#-400# to Q235 plate (300mm × 150mm × 4mm) gas metal-arc welding (MIG) Weld seam is polished, and is degreased with acetone or alcohol, and pending area is that entire weld seam and weld seam two sides are prolonged to base material respectively It stretches at 20mm;
(2) parameter selection:Metallic is stainless steel particle, and gas pressure 3.0MPa, preheating temperature is 200 DEG C, is added Fast gas selects nitrogen;
(3) stainless steel particle is packed into powder feeder, connects high-pressure air source, nitrogen pressure reaches 3.0MPa, nitrogen is passed through High-pressure air source a part is passed through the powder feeder, for pushing aluminium oxide particles, so that its speed is reached 400-1000m/s, is formed High-velocity particles stream;Another part is passed through gas heater, and gas temperature is heated to 200 DEG C;
(4) sample is carried out by clamping by mechanical arm or mechanical device, then uses processing rifle by the high-velocity particles Acceleration gas after stream and heating sprays simultaneously, hits the weld seam and pending area of metal material;
(5) circulation aforesaid operations are primary.
The result shows that:As-welded peak stress is 186MPa, under the action of high-velocity particles hit and impact with hot gas, sample Stress distribution is improved, maximum stress 23MPa, and more presentation compressive stress states around weld seam.
Five, embodiment (five):
The processing method of the present embodiment includes the following steps:
(1) 2219 aluminium alloy plates (300mm × 150mm × 8mm) VPTIG weld seam is beaten with the sand paper of 70#-400# Mill, is degreased with acetone or alcohol, and pending area is that entire weld seam and weld seam two sides extend at 20mm to base material respectively;
(2) parameter selection:Metallic is Cu particle, and gas pressure 2.6MPa, preheating temperature is 600 DEG C, accelerates gas Body selects nitrogen;
(3) Cu particle is packed into powder feeder, connects high-pressure air source, nitrogen pressure reaches 2.6MPa, nitrogen is passed through high pressure Gas source a part is passed through the powder feeder, for pushing Cu particle, so that its speed is reached 400-1000m/s, forms high-velocity particles Stream;Another part is passed through gas heater, and gas temperature is heated to 600 DEG C;
(4) sample is carried out by clamping by mechanical arm or mechanical device, then uses processing rifle by the high-velocity particles Acceleration gas after stream and heating sprays simultaneously, hits the weld seam and pending area of metal material;
(5) circulation aforesaid operations are primary.
The result shows that:The peak stress of substrate is 140MPa when as-welded, hits the effect with hot gas impact in high-velocity particles Under, the stress distribution of substrate is improved, maximum stress 38MPa, and stress distribution is more uniform, gentle.
Although the embodiments of the present invention has been shown and described above, it is to be understood that above-described embodiment is example Property, it is not considered as limiting the invention, those skilled in the art are not departing from the principle of the present invention and objective In the case where can make changes, modifications, alterations, and variations to the above described embodiments within the scope of the invention.

Claims (3)

1. a kind of method for reducing structural metallic materials joint made by flame welding residual stress, it is characterised in that:Concrete operation step is as follows,
Step 1:Face of weld is pre-processed:First with sand paper polishing metal material weld seam and pending area, to remove Impurity;Then the weld seam of metal material and the greasy dirt of pending area are removed with acetone or alcohol;
Step 2:Metallic is packed into powder feeder, the metal particle size is between 10-100 μm;
Step 3:High-pressure air source is connected, the acceleration gas pressure being passed through is 1.5-3.5MPa, and gas will be accelerated to pass through high-pressure air source A part is passed through the powder feeder, for pushing the metallic, so that its speed is reached 400-1000m/s, forms high speed grain Subflow;Another part is passed through gas heater, and gas temperature is heated to 200-600 DEG C;
Step 4:Metal material is subjected to clamping by mechanical arm or mechanical device, then uses processing rifle by the high speed Acceleration gas after particle flux and heating sprays simultaneously, hits the weld seam and pending area of metal material;
Step 5:Decide whether to repeat the above steps by stress mornitoring result.
2. reducing the method for structural metallic materials joint made by flame welding residual stress according to claim 1, it is characterised in that:It is described Acceleration gas is helium, nitrogen or compressed air.
3. reducing the method for structural metallic materials joint made by flame welding residual stress according to claim 1, it is characterised in that:It is described Metallic is Cu, Ni, W or stainless steel.
CN201810747439.9A 2018-07-09 2018-07-09 A method of reducing structural metallic materials joint made by flame welding residual stress Pending CN108838904A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810747439.9A CN108838904A (en) 2018-07-09 2018-07-09 A method of reducing structural metallic materials joint made by flame welding residual stress

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810747439.9A CN108838904A (en) 2018-07-09 2018-07-09 A method of reducing structural metallic materials joint made by flame welding residual stress

Publications (1)

Publication Number Publication Date
CN108838904A true CN108838904A (en) 2018-11-20

Family

ID=64196985

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810747439.9A Pending CN108838904A (en) 2018-07-09 2018-07-09 A method of reducing structural metallic materials joint made by flame welding residual stress

Country Status (1)

Country Link
CN (1) CN108838904A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110421045A (en) * 2019-07-19 2019-11-08 大冶市同创不锈钢金属材料有限公司 A kind of sheet stamping device and process for stamping
CN112757168A (en) * 2020-12-21 2021-05-07 浙江来福谐波传动股份有限公司 High-speed kinetic energy microparticle composite shot blasting surface strengthening process
CN112935256A (en) * 2021-01-26 2021-06-11 四川大学 Method for modifying non-ferromagnetic powder sintered metal parts based on pulsed magnetic field
CN113239477A (en) * 2021-04-01 2021-08-10 四川大学 Application of cyclic hardening model based on welding line dislocation entanglement in fatigue life prediction of welding joint

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1532295A (en) * 2003-03-19 2004-09-29 中国科学院金属研究所 Gas and solid two phase flaw impact metal material surface nano device and its use
CN2709083Y (en) * 2004-07-19 2005-07-13 河北农业大学 Parameter regulatable bammer blow device along with welding
CN1757484A (en) * 2005-10-13 2006-04-12 南京工业大学 Glass cloudburst treatment art for improving anti-stress corrosion performance of welding joint of stainless steel
EP1602442B1 (en) * 2004-06-01 2012-11-28 United Technologies Corporation Methods for repairing gas turbine engine components
JP2014208363A (en) * 2013-04-16 2014-11-06 友鉄工業株式会社 Method for manufacturing pressing die
CN104625403A (en) * 2015-01-27 2015-05-20 湖南大学 Method for restraining myriawatt-class laser welding thick plate upper surface defects
CN105543837A (en) * 2015-12-25 2016-05-04 北京有色金属研究总院 Repair method for copper-tungsten composite structure

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1532295A (en) * 2003-03-19 2004-09-29 中国科学院金属研究所 Gas and solid two phase flaw impact metal material surface nano device and its use
EP1602442B1 (en) * 2004-06-01 2012-11-28 United Technologies Corporation Methods for repairing gas turbine engine components
CN2709083Y (en) * 2004-07-19 2005-07-13 河北农业大学 Parameter regulatable bammer blow device along with welding
CN1757484A (en) * 2005-10-13 2006-04-12 南京工业大学 Glass cloudburst treatment art for improving anti-stress corrosion performance of welding joint of stainless steel
JP2014208363A (en) * 2013-04-16 2014-11-06 友鉄工業株式会社 Method for manufacturing pressing die
CN104625403A (en) * 2015-01-27 2015-05-20 湖南大学 Method for restraining myriawatt-class laser welding thick plate upper surface defects
CN105543837A (en) * 2015-12-25 2016-05-04 北京有色金属研究总院 Repair method for copper-tungsten composite structure

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110421045A (en) * 2019-07-19 2019-11-08 大冶市同创不锈钢金属材料有限公司 A kind of sheet stamping device and process for stamping
CN112757168A (en) * 2020-12-21 2021-05-07 浙江来福谐波传动股份有限公司 High-speed kinetic energy microparticle composite shot blasting surface strengthening process
CN112757168B (en) * 2020-12-21 2022-06-28 浙江来福谐波传动股份有限公司 High-speed kinetic energy microparticle composite shot blasting surface strengthening process
CN112935256A (en) * 2021-01-26 2021-06-11 四川大学 Method for modifying non-ferromagnetic powder sintered metal parts based on pulsed magnetic field
CN113239477A (en) * 2021-04-01 2021-08-10 四川大学 Application of cyclic hardening model based on welding line dislocation entanglement in fatigue life prediction of welding joint
CN113239477B (en) * 2021-04-01 2023-05-02 四川大学 Application of cyclic hardening model based on dislocation entanglement of weld joint in fatigue life prediction of welded joint

Similar Documents

Publication Publication Date Title
CN108838904A (en) A method of reducing structural metallic materials joint made by flame welding residual stress
CN103409758B (en) Pump shells and blade microcrack laser reinforcing life-prolonging method
JP6558443B2 (en) Resistance spot welding method
JP2004149843A (en) Method for improving toughness in heat affected zone in welded joint of steel product
US20080032152A1 (en) Use of laser shock processing in oil & gas and petrochemical applications
CN109158831A (en) A kind of modified method in laser assisted ultrasonic burnishing surface
CN109609747A (en) A kind of homogenization technique of coiled tubing
CN110091023A (en) A kind of vacuum welding method of titanium carbide steel bonded carbide and steel alloy
CA2491743A1 (en) Ultrasonic impact machining of body surfaces to correct defects and strengthen work surfaces
JP2006122969A (en) Welded joint of metallic material and metallic clad material, and laser peening of casting material
Abass et al. Study of solidification behaviour and mechanical properties of arc stud welded AISI 316L stainless steel
Benchouia et al. Fatigue life enhancement of TIG-welded 304L stainless steels by shot peening
US20130047394A1 (en) Solid state system and method for refurbishment of forged components
CN105108294A (en) Vacuum electron beam welding method for 30CrMnSiNi2A steel
CN102936647A (en) Method for prolonging fatigue life of welded joint subjected to mechanical surface strengthening
JP2004130313A (en) Method for increasing fatigue strength of lap fillet weld joint
JP2004169065A (en) Method for improving strength of cold-worked part with ultrasonic shock treatment and its metallic product
JP3899008B2 (en) Method for improving fatigue strength of butt welded joints
JP2004130316A (en) Boxing joint of excellent fatigue strength, boxing joint manufacturing method, and welded structure
JP2007098462A (en) Flash butt welding method
CN109943842A (en) The processing method and metal-base composites of material surface high hardness wear-resisting composite layer
WO2004046395A1 (en) Method of setting ultrasonic shock treatment conditions for metal material
CN113579531A (en) Method for ultrasonic pulse MAG composite welding of ultrahigh-strength steel
Ebrahimzadeh et al. Fabrication of synchronized hammer peening with pulsed laser welding and its effect on 6061 aluminum alloy weld
Sun et al. Crack repair of hot work tool steel by laser melt processing

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

Application publication date: 20181120

RJ01 Rejection of invention patent application after publication