CN104846156B - A kind of square focus spot laser multilayer interlocks and impacts uniform intensifying method - Google Patents

A kind of square focus spot laser multilayer interlocks and impacts uniform intensifying method Download PDF

Info

Publication number
CN104846156B
CN104846156B CN201510182755.2A CN201510182755A CN104846156B CN 104846156 B CN104846156 B CN 104846156B CN 201510182755 A CN201510182755 A CN 201510182755A CN 104846156 B CN104846156 B CN 104846156B
Authority
CN
China
Prior art keywords
laser
layer
impact
axis
uniform
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
CN201510182755.2A
Other languages
Chinese (zh)
Other versions
CN104846156A (en
Inventor
罗开玉
朱轶杰
景祥
鲁金忠
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.)
Jiangsu University
Original Assignee
Jiangsu 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 Jiangsu University filed Critical Jiangsu University
Priority to CN201510182755.2A priority Critical patent/CN104846156B/en
Publication of CN104846156A publication Critical patent/CN104846156A/en
Application granted granted Critical
Publication of CN104846156B publication Critical patent/CN104846156B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The present invention relates to field of laser processing, a kind of square focus spot laser multilayer is refered in particular to interlock the uniform intensifying method of impact, i.e. each layer using the equally distributed square focus spot of energy carry out it is adjacent do not overlap it is laser impact intensified, facula position is laterally and longitudinally method staggeredly uniform by a certain percentage is uniformly strengthened realizing the surface of metalwork between adjacent two layers.The method substantially eliminates the boundary effect of square focus spot, makes workpiece surface crystal grain refinement, improves the stability and reliability of large-area laser shock peening, obtains uniform reinforcing effect and high in machining efficiency.The invention can be used for the uniform intensive treatment in the surfaces such as industrial bar, casting and blade.

Description

A kind of square focus spot laser multilayer interlocks and impacts uniform intensifying method
Technical field
The inventive method is related to field of laser processing, refers in particular to a kind of square focus spot laser multilayer and interlocks the uniform reinforcing side of impact Method, is particularly suitable for the uniform intensive treatment of the material surfaces such as industrial bar, casting and blade.
Background technology
It is laser impact intensified(It is called laser peening)It is a kind of new material surface strengthening technology, using strong laser induced Knock wave mechanics effect material is processed, the features such as with high pressure, high energy, ultrafast and Under High Strain rate;What it was formed Residual compressive stress layer can effectively eliminate the stress concentration of material internal and suppress the germinating and extension of crackle, can significantly improve The fatigue life of metal parts and anticorrosive and antiwear property, substantial amounts of research have shown that reiforcing laser impact technology is extension The crack initiation time reduces the effective means that crack propagation velocity improves material lifetime.
Common laser impact reinforcing method has some limitations, such as:During common laser shock peening treatment blade, Easily peel off absorbed layer warpage, cause blade surface ablation, residual compressive stress field that is damaged and impacting generation and surface micro- Pattern is uneven;Section blades extend inconsistent to length direction reinforcing effect;The laser impact intensified technique of blade surface without Method reaches standard.
The content of the invention
In order to solve the above technical problems, interlock impacting uniform reinforcing side the invention provides a kind of square focus spot laser multilayer Method, i.e., each layer carries out adjacent laser impact intensified, the adjacent two layers not overlapped using the equally distributed square focus spot of energy Between facula position laterally and longitudinally method staggeredly uniform by a certain percentage is uniformly strengthened realizing the surface of metalwork; The method substantially eliminates the boundary effect of square focus spot, makes workpiece surface crystal grain refinement, improves large-area laser shock peening Stability and reliability, obtain uniform reinforcing effect and high in machining efficiency, realize the uniform reinforcing at blade parts edge, have Body step is:
(1)The power output and hot spot parameter of laser are set by laser control device, makes its light spot shape be side Shape, the length of side is a.
(2)Workpiece is arranged on five axle workbench, and absorbed layer is covered in workpiece work surface, absorbing layer surface It is the square net of a to draw the length of side, and determines impact number of plies N altogether.
(3)Adjusting five axle workbench by digital control system makes the single grid corner of laser beam position and latticed absorbed layer Overlap, at shock zone starting turning as the laser impact intensified treatment initial point position of ground floor, and make grid restraint layer X-axis and Y-axis it is consistent with the X-axis and Y-axis of workbench.
(4)Using flowing water as restraint layer, laser is opened, five are controlled by digital control system using the method processed line by line The movement of axle workbench and rotating realize carrying out workpiece work surface ground floor it is laser impact intensified, it is adjacent in impact process Square focus spot is adjacent not to be overlapped.
(5)Absorbed layer is changed, and grid is repainted layer surface is absorbed.
(6)Adjusting five axle workbench by digital control system makes the single grid corner of laser beam position and latticed absorbed layer Overlapping positions from the shock zone starting turning X-direction in last layer to b is offset outside shock zone, Y-direction is to shock zone Outer skew b, as the laser impact intensified treatment initial point position of the second layer, and makes the X-axis and Y-axis of grid restraint layer and work The X-axis of platform is consistent with Y-axis.
(7)Using flowing water as restraint layer, laser is opened, five are controlled by digital control system using the method processed line by line The movement of axle workbench and rotating realize carrying out workpiece work surface the second layer it is laser impact intensified, it is adjacent in impact process Square focus spot is adjacent not to be overlapped.
(8)Repeat step(5)(6)(7), until N layers of completion is laser impact intensified.
Laser impact intensified pulse laser beam of the present invention is square hot spot, and length of side a is 2-8mm, frequency Rate is 1-5Hz, and pulsewidth is 8-30ns, pulse energy 3-15J;Laser reinforcing impacts X-axis and Y-axis side-play amount b=a/N;Using flowing water Used as restraint layer, thickness is 1mm;Absorption layer material is aluminium foil, and thickness is 100 μm.
Impact number of plies N determines according to experiment material property and laser-impact threshold value, is 3-5 layers.
Beneficial effects of the present invention:The boundary effect of square focus spot is eliminated, workpiece surface crystal grain refinement improves large area and swashs The stability and reliability of light shock peening, obtain uniform reinforcing effect and high in machining efficiency.
Brief description of the drawings
Fig. 1 impacts the schematic diagram of uniform intensifying method for square focus spot laser multilayer interlocks.
Fig. 2 is the workpiece surface metallographic structure after uniform intensifying method treatment.
Fig. 3 is undressed workpiece surface metallographic structure.
Fig. 4 is two groups of sample detection site surface residual stress value curves.
Fig. 5 is two groups of sample detection site superficial hardness number curves.
Fig. 6 impacts the flow process chart of uniform intensifying method for square focus spot laser multilayer interlocks.
Specific embodiment
The present invention is described in detail below in conjunction with the accompanying drawings.
The matrix of samples material that the present embodiment is used is 316L stainless steels, its physical dimension be 140mm ×
70mm×25mm。
The technological parameter of laser is:Pulsewidth 8ns, frequency 1Hz, pulse energy 6J, light spot shape are square, spot size A is 5mm, and adjacent prismatic hot spot is adjacent not to be overlapped.
Concretely comprise the following steps:
(1)The power output and hot spot parameter of laser are set by laser control device, makes its light spot shape be side Shape, the length of side is 5mm.
(2)Workpiece is arranged on five axle workbench, and absorbed layer is covered in workpiece work surface, absorbing layer surface It is the square net of a to draw the length of side, and determines impact number of plies N altogether;According to experiment material property and laser-impact threshold value come really Surely number of plies N is impacted, N=5 is taken.
(3)Adjusting five axle workbench by digital control system makes the single grid corner of laser beam position and latticed absorbed layer Overlap, at shock zone starting turning as the laser impact intensified treatment initial point position of ground floor, and make grid restraint layer X-axis and Y-axis it is consistent with the X-axis and Y-axis of workbench.
(4)Using flowing water as restraint layer, laser is opened, five are controlled by digital control system using the method processed line by line The movement of axle workbench and rotating realize carrying out workpiece work surface ground floor it is laser impact intensified, it is adjacent in impact process Square focus spot is adjacent not to be overlapped.
(5)Absorbed layer is changed, and grid is repainted layer surface is absorbed.
(6)Adjusting five axle workbench by digital control system makes the single grid corner of laser beam position and latticed absorbed layer Overlapping positions from the shock zone starting turning X-direction in last layer to 1mm is offset outside shock zone, Y-direction is to impact zone Overseas skew 1mm, as the laser impact intensified treatment initial point position of the second layer, and make the X-axis and Y-axis of grid restraint layer with The X-axis of workbench is consistent with Y-axis.
(7)Using flowing water as restraint layer, laser is opened, five are controlled by digital control system using the method processed line by line The movement of axle workbench and rotating realize carrying out workpiece work surface the second layer it is laser impact intensified, it is adjacent in impact process Square focus spot is adjacent not to be overlapped;
(8)Repeat step(5)(6)(7), until 5 layers of completion is laser impact intensified.
Choose two parallel lines along Y direction in the square region on workpiece treatment surface, two parallel lines at a distance of 15mm, With square region side at a distance of 5mm, decile takes six points on every straight line, and spacing is 5mm, totally 12 points, to the residual of sample point Residue stress and hardness are tested and analyzed.
Arranged as shown in Fig. 2 by the workpiece surface crystal grain refinement of intensive treatment, between crystal grain closely in order, obtain compared with Good uniform reinforcing effect.And in Fig. 3, the workpiece surface crystal grain arrangement without intensive treatment is disorderly and unsystematic and intercrystalline Gap is larger.
As shown in Figure 4,5, in 280MPa or so, hardness value stabilization exists the surface residual stress value stabilization that detection is obtained 350Hv or so, it can be deduced that conclusion:Interlocking by square focus spot laser multilayer, it is notable to impact the uniform workpiece surface performance strengthened Improve, the refinement of workpiece material surface layer grain improves the stability and reliability of large-area laser shock peening, obtains uniform reinforcing Effect and high in machining efficiency.

Claims (2)

1. a kind of square focus spot laser multilayer interlocks the uniform intensifying method of impact, it is characterised in that comprise the following steps that:
(1) power output and hot spot parameter of laser are set by laser control device, makes its light spot shape be square, side A length of a;
(2) workpiece is arranged on five axle workbench, and absorbed layer is covered in workpiece work surface, in absorbed layer surface rendering The length of side is the square net of a, and impact number of plies N is determined according to experiment material property and laser-impact threshold value;
(3) adjusting five axle workbench by digital control system makes the single grid corner weight of laser beam position and latticed absorbed layer Close, at shock zone starting turning as the laser impact intensified treatment initial point position of ground floor, and make the X of grid restraint layer Axle and Y-axis are consistent with the X-axis and Y-axis of workbench;
(4) using flowing water as restraint layer, laser is opened, five axle works is controlled by digital control system using the method processed line by line Make the movement of platform and rotating and realize carrying out workpiece work surface ground floor laser impact intensified, adjacent prismatic in impact process Hot spot is adjacent not to be overlapped;
(5) absorbed layer is changed, and grid is repainted layer surface is absorbed;
(6) adjusting five axle workbench by digital control system makes the weight of laser beam position and the single grid corner of latticed absorbed layer Position is closed from the shock zone starting turning X-direction in last layer to offseting b outside shock zone, Y-direction to outside shock zone partially B is moved, as the laser impact intensified treatment initial point position of the second layer, and makes the X-axis and Y-axis of grid restraint layer and workbench X-axis is consistent with Y-axis;
(7) using flowing water as restraint layer, laser is opened, five axle works is controlled by digital control system using the method processed line by line Make the movement of platform and rotating and realize carrying out workpiece work surface the second layer laser impact intensified, adjacent prismatic in impact process Hot spot is adjacent not to be overlapped;
(8) repeat step (5) (6) (7), until N layers of completion is laser impact intensified;
The length of side a of the square focus spot is 2-8mm;The laser impact intensified technological parameter is:Laser frequency is 1-5Hz, Pulsewidth is 8-30ns, and pulse energy is 3-15J;It is the shock ply number of plies, N that laser reinforcing impacts X-axis and Y-axis side-play amount b=a/N, N Value is 3-5.
2. a kind of square focus spot laser multilayer as claimed in claim 1 interlocks the uniform intensifying method of impact, it is characterised in that:Adopt With flowing water as restraint layer, thickness is 1mm;Absorption layer material is aluminium foil, and thickness is 100 μm.
CN201510182755.2A 2015-04-17 2015-04-17 A kind of square focus spot laser multilayer interlocks and impacts uniform intensifying method Expired - Fee Related CN104846156B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510182755.2A CN104846156B (en) 2015-04-17 2015-04-17 A kind of square focus spot laser multilayer interlocks and impacts uniform intensifying method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510182755.2A CN104846156B (en) 2015-04-17 2015-04-17 A kind of square focus spot laser multilayer interlocks and impacts uniform intensifying method

Publications (2)

Publication Number Publication Date
CN104846156A CN104846156A (en) 2015-08-19
CN104846156B true CN104846156B (en) 2017-06-27

Family

ID=53846136

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510182755.2A Expired - Fee Related CN104846156B (en) 2015-04-17 2015-04-17 A kind of square focus spot laser multilayer interlocks and impacts uniform intensifying method

Country Status (1)

Country Link
CN (1) CN104846156B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2796661C1 (en) * 2022-09-19 2023-05-29 Федеральное государственное бюджетное учреждение науки Пермский федеральный исследовательский центр Уральского отделения Российской академии наук (ПФИЦ УрО РАН) Method for processing a flat billet made of titanium alloy with a stress concentrator

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105002349B (en) * 2015-07-21 2017-05-03 江苏大学 Method for conducting variable-light-spot multilayer staggered laser shock homogeneous enhancement on blades
CN105925792B (en) * 2016-07-08 2018-10-19 中国科学院长春光学精密机械与物理研究所 Laser impact intensified system
CN106282532B (en) * 2016-08-18 2018-01-16 江苏大学 A kind of laser impact intensified combined method for obtaining metal surface crystal grain mixed distribution
CN106446517B (en) * 2016-08-30 2019-04-30 江苏大学 A kind of modeling of laser impact intensified alloy plastic deformation's depth and method of discrimination
CN107937707B (en) * 2017-11-28 2019-11-08 广东工业大学 A kind of method and system of pulse laser reinforced metal
CN110885920A (en) * 2019-10-29 2020-03-17 天津修船技术研究所(中国船舶重工集团公司第六三一三研究所) Method for strengthening exhaust valve seat of cylinder cover of special cast iron diesel engine
CN111944989B (en) * 2020-09-04 2021-09-14 武汉大学 Method for rapidly selecting area laser reinforcement

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6336991A (en) * 1986-07-30 1988-02-17 Komatsu Ltd Laser beam molding device
CN103526010B (en) * 2013-10-28 2015-01-14 东南大学 Method and device for reinforcement of hole structure by utilization of square laser spot shock wave
CN104164538B (en) * 2014-07-16 2017-02-22 江苏大学 Laser shock reinforcing method for obtaining large area uniform surface morphology
CN104164554A (en) * 2014-07-16 2014-11-26 江苏大学 Method for reinforcement of metal surface by large area laser shock

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2796661C1 (en) * 2022-09-19 2023-05-29 Федеральное государственное бюджетное учреждение науки Пермский федеральный исследовательский центр Уральского отделения Российской академии наук (ПФИЦ УрО РАН) Method for processing a flat billet made of titanium alloy with a stress concentrator

Also Published As

Publication number Publication date
CN104846156A (en) 2015-08-19

Similar Documents

Publication Publication Date Title
CN104846156B (en) A kind of square focus spot laser multilayer interlocks and impacts uniform intensifying method
CN105039652B (en) A kind of uniform intensifying method of square focus spot laser-impact for curved surface
CN105002349B (en) Method for conducting variable-light-spot multilayer staggered laser shock homogeneous enhancement on blades
CN104164538B (en) Laser shock reinforcing method for obtaining large area uniform surface morphology
CN101665859B (en) Laser shot-blasting process for stainless steel welded joint
CN103409758B (en) Pump shells and blade microcrack laser reinforcing life-prolonging method
CN101392382B (en) Method and device for strengthening surface modification by combination of laser cladding and laser peening
WO2016074314A1 (en) Laser thermal combination remanufacturing method for damaged metal part
CN101492759B (en) Stress corrosion dehiscence resistant ultrasonic impact treatment process
PL195102B1 (en) Contour forming of metals by laser peening
CN105177273B (en) A kind of laser shock peening method for improving crucial important component fatigue strength
CN1708593A (en) Method of increasing toughness of heat-affected part of steel product welded joint
CN102199690A (en) Laser plasma shock wave surface nanocrystallization method for polycrystal metal material
Zhang et al. Progress in applications of shockwave induced by short pulsed laser on surface processing
Zhang et al. Effects of laser shock processing on mechanical properties of laser welded ANSI 304 stainless steel joint
CN105651957A (en) Method for assessing laser shot peening effect
CN112375899A (en) Rectangular uniform laser pulse shock strengthening and forming system and application method thereof
Chen et al. Effects of LSP on micro-structures and residual stresses in a 4 mm CLAM steel weld joints
Yang et al. Distortion control of thin sections by single-sided laser peening
CN110938740B (en) Intermetallic compound laser shock peening life prolonging and deformation control method
CN1708592A (en) Metal structure product with excellent environmental cracking resistance and method of enhancing environmental cracking resistance of metal structure product
CN107236859A (en) A kind of modeling for obtaining optimum surface quality laser peening parameter and computational methods
CN103343189B (en) Method for combinatorially reinforcing thick plate through laser shock
Kattoura et al. Modern laser peening for material surface enhancement
Zhang et al. Investigation of residual stress field in the curved surface of round rod subjected to multiple laser shock peening

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170627

Termination date: 20190417

CF01 Termination of patent right due to non-payment of annual fee