CN102747197B - Technological parameter real-time monitoring method for laser shock peening process - Google Patents

Technological parameter real-time monitoring method for laser shock peening process Download PDF

Info

Publication number
CN102747197B
CN102747197B CN201210225116.6A CN201210225116A CN102747197B CN 102747197 B CN102747197 B CN 102747197B CN 201210225116 A CN201210225116 A CN 201210225116A CN 102747197 B CN102747197 B CN 102747197B
Authority
CN
China
Prior art keywords
laser
energy
sheet glass
light path
glass plate
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
CN201210225116.6A
Other languages
Chinese (zh)
Other versions
CN102747197A (en
Inventor
魏延鹏
宋宏伟
黄晨光
吴先前
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.)
Institute of Mechanics of CAS
Original Assignee
Institute of Mechanics of CAS
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 Institute of Mechanics of CAS filed Critical Institute of Mechanics of CAS
Priority to CN201210225116.6A priority Critical patent/CN102747197B/en
Publication of CN102747197A publication Critical patent/CN102747197A/en
Application granted granted Critical
Publication of CN102747197B publication Critical patent/CN102747197B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention discloses a technological parameter real-time monitoring method for a laser shock peening process. The method comprises the following steps: 1) arranging a first glass plate on a laser output light path of a laser device, wherein an included angle between the first glass plate and the laser output light path is 75-85 DEG, and carrying out laser shock peening by the laser transmitted through the first glass plate and output by the laser device; 2) arranging a second glass plate on a light path formed by reflecting the laser output by the laser device by the first glass plate, wherein an included angle between the light path and the second glass plate is 75-85 DEG; arranging an energy meter on a light path transmitted by the second glass plate; and arranging a photoelectric probe on a light path reflected by the second glass plate; and 3) transmitting the laser energy information acquired by the energy meter and laser pulse width information acquired by the photoelectric probe to a processing system. According to the present invention, corresponding laser energy and pulse width effected on a target body are obtained through on-line detection of reflected laser energy and laser pulse width, thereby realizing real-time monitoring on technological parameters of the laser shock peening process.

Description

A kind of laser impact intensified process parameter real time monitoring method
Technical field
The present invention relates to a kind of laser impact intensified process parameter real time monitoring method.
Background technology
Reiforcing laser impact technology is a kind of novel material surface treatment process, the plasma shockwave that it utilizes intense laser beam to produce, at material surface, produce certain thickness unrelieved stress layer, and change surfacing weave construction, thereby improve antifatigue, the wear-resistant and resistance to corrosion of metallic substance.
Compare with the reinforcing process such as shot-peening in the past, laser impact intensified have outstanding advantages such as noncontact,, unrelieved stress layer depth strong without heat affected zone, controllability and strengthening effect be remarkable.On the absorption layer that a branch of high-energy-density laser radiation is adhered at target body material surface, absorption layer absorbing laser energy generates rapidly high pressure plasma, the high pressure of plasma generation suffer restraints layer effect can not decay very soon, be subject to High Pressure, material surface can produce shockwave and to internal communication, due to the yield strength of pressure over material, the part material of shock wave can produce viscous deformation, at material surface, form the unrelieved stress with certain distribution, these residual stress distribution can effectively stop the generation of surface crack.Thereby material is subject to High Pressure can produce certain phase transformation and forms hardened layer simultaneously, improves surperficial resistance to corrosion.
In reiforcing laser impact technology, pulsed laser energy parameter and pulsewidth parameter have directly determined to act on the pressure characteristic of material surface, thereby have determined the effect of final shock peening.Shock peening parameter in the past determine and the assessment of strengthening effect be all while utilizing laser apparatus to dispatch from the factory to parameter, rather than the result of Real-Time Monitoring.
For laser apparatus, the energy that every pulse laser beam carries and pulse width and factory-said value are all difference to some extent, in order to assess accurately the relation between laser impact intensified parameter and strengthening effect, must carry out Real-Time Monitoring to beam energy and pulsewidth waveform.
In addition, laser apparatus single-shot energy and adjusting by regulating the multistage pump energy of laser apparatus and delay time to regulate, generally do not there is linear regulation relation.This just makes the research of studying strengthening effect under particular energy be difficult to realize, necessary by laser single-shot energy in certain laser impact intensified process of device Real-Time Monitoring and two parameters of pulse width, thus set up the quantitative relationship between multistage pump energy, delay time and Laser output processing parameter.
Summary of the invention
The problem existing for prior art, the object of the present invention is to provide a kind of laser impact intensified process parameter real time monitoring method and system, can realize the Real-Time Monitoring of single-shot beam energy and pulse width in laser impact intensified process, for the relation between assessment reinforcing process parameter and Effect of Laser Shock Processing provides favourable detection means and method.
A kind of laser impact intensified process parameter real time monitoring method of the present invention comprises the steps:
1) angle with this laser apparatus output light path being set in the Laser output light path of laser apparatus is first sheet glass of 75 ~ 85 °, and the laser of described laser apparatus output sees through described the first sheet glass target body is carried out to shock peening;
2) angle with this light path being set in the light path through described the first sheet glass reflection at the laser of described laser apparatus output is second sheet glass of 75 ~ 85 °, through in the light path of this second sheet glass transmission, energy meter is being set, laser energy for acquisition of transmission, in the light path of this second sheet glass reflection, photoelectric probe is set, for gathering the laser pulse width of reflection;
3) the laser energy information of described energy meter collection and the laser pulse width information of described photoelectric probe collection send treatment system to, through converting, obtain acting on laser energy and pulse width on target body.
Preferably, described the first sheet glass and the second sheet glass are the dull and stereotyped silica glass of thickness 1 ~ 3mm.
The present invention, by online laser energy and the laser pulse width detecting through reflection, through converting, obtains respective action laser energy and pulse width on target body, thereby has realized the Real-Time Monitoring of laser impact intensified process parameter.
Accompanying drawing explanation
Fig. 1 is embodiment of the present invention schematic diagram.
Embodiment
As shown in Figure 1, laser impact intensified process parameter method of real-time of the present invention comprises the steps:
1) angle with this laser apparatus 1 output light path being set in the Laser output light path of laser apparatus 1 is first sheet glass 2 of 80 °, and the laser of laser apparatus 1 output sees through 2 pairs of target bodys of the first sheet glass 7 and carries out shock peening;
2) angle with this light path being set in the light path through the first sheet glass 2 reflections at the laser of laser apparatus 1 output is second sheet glass 3 of 80 °, through in the light path of these the second sheet glass 3 transmissions, high frequency sound energy meter 5 is being set, laser energy for acquisition of transmission, in the light path of these the second sheet glass 3 reflections, nanosecond photoelectric probe 4 is set, for gathering the laser pulse width of reflection;
3) the laser pulse width information that the laser energy information that high frequency sound energy meter 5 gathers and nanosecond photoelectric probe 4 gather sends treatment system 6 to, obtains acting on laser energy and pulse width on target body 7, thereby realize on-line real time monitoring through converting.
In embodiments of the present invention, the first sheet glass 2 and the second sheet glass 3 are dull and stereotyped silica glass.
The laser that high-energy short-pulse laser 1 is launched is first through the first sheet glass 2, the thickness of the first sheet glass 2 is 2mm, the normal direction of the first sheet glass 2 and laser are 10 ° of angles, when the normal of the first sheet glass 2 and laser angle are less than 15 °, the one side emittance of sheet glass is 4%, if the energy of laser input is E, emittance is a, and the energy by transmission after 2 two faces of the first sheet glass is E t=E (1-a) 2, the energy of reflection is E f=E-E (1-a) 2=aE (2-a), these energy are again through the second sheet glass 3, and final transmission potential is E n=Ea (1-a) 2(2-a), the ENERGY E of final reflection m=a 2e (2-a) 2.
E E n = 1 a ( 1 - a ) 2 ( 2 - a ) ] ≈ 13.84
E t E n = ( 1 - a ) 2 a ( 1 - a ) 2 ( 2 - a ) ≈ 12.76
E nby high frequency sound energy meter 5, collected, data directly upload to treatment system 6, by being multiplied by gain factor, just can obtain the energy of Laser output and act on the energy on laser impact intensified target body 7.
E mby nanosecond photoelectric probe 4, received, can catch laser pulse width, because pulse width can not change due to the decay of energy and the distance of propagation, so the pulsewidth collecting is exactly the pulsewidth of Laser output and acts on the pulsewidth on target body 7, the pulse width data recording uploads to treatment system 6 equally.
Like this, just can in laser-impact process, act on laser energy and pulse width on target body 7 by Real-Time Monitoring, thereby on the rule that affects of strengthening effect, provide the most effective test instrument for obtaining laser parameter.

Claims (1)

1. a laser impact intensified process parameter real time monitoring method, is characterized in that, comprises the steps:
1) angle with this laser apparatus output light path being set in the Laser output light path of laser apparatus is first sheet glass of 75~85 °, and the laser of described laser apparatus output sees through described the first sheet glass target body is carried out to shock peening; Wherein, the thickness of the first sheet glass is 2mm, when the normal of the first sheet glass and laser angle are less than 15 °, the one side emittance of the first sheet glass is 4%, if the energy of laser input is E, emittance is a, and the energy by transmission after 2 two faces of the first sheet glass is E t=E (1-a) 2;
2) angle with this light path being set in the light path through described the first sheet glass reflection at the laser of described laser apparatus output is second sheet glass of 75~85 °, through in the light path of this second sheet glass transmission, energy meter is being set, laser energy for acquisition of transmission, in the light path of this second sheet glass reflection, photoelectric probe is set, for gathering the laser pulse width of reflection; Wherein, the energy through the first sheet glass back reflection is E f=E-E (1-a) 2=aE (2-a), these energy are again through the second sheet glass, and final transmission potential is E n=Ea (1-a) 2(2-a), the ENERGY E of final reflection m=a 2e (2-a) 2;
3) the laser energy information of described energy meter collection and the laser pulse width information of described photoelectric probe collection send treatment system to, through converting, obtain acting on laser energy and pulse width on target body.
CN201210225116.6A 2012-06-29 2012-06-29 Technological parameter real-time monitoring method for laser shock peening process Expired - Fee Related CN102747197B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210225116.6A CN102747197B (en) 2012-06-29 2012-06-29 Technological parameter real-time monitoring method for laser shock peening process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210225116.6A CN102747197B (en) 2012-06-29 2012-06-29 Technological parameter real-time monitoring method for laser shock peening process

Publications (2)

Publication Number Publication Date
CN102747197A CN102747197A (en) 2012-10-24
CN102747197B true CN102747197B (en) 2014-04-02

Family

ID=47027684

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210225116.6A Expired - Fee Related CN102747197B (en) 2012-06-29 2012-06-29 Technological parameter real-time monitoring method for laser shock peening process

Country Status (1)

Country Link
CN (1) CN102747197B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111220358A (en) * 2018-11-26 2020-06-02 大族激光科技产业集团股份有限公司 High-power laser light source continuous stability testing system and method
CN110346038A (en) * 2019-05-30 2019-10-18 大族激光科技产业集团股份有限公司 A kind of laser beam separator and method

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3739862A1 (en) * 1987-11-25 1989-06-08 Bosch Gmbh Robert WORKPIECE MACHINING DEVICE
CN201680906U (en) * 2009-11-27 2010-12-22 北京工业大学 High-power laser on-line digital test instrument
CN101825491B (en) * 2010-05-18 2012-07-04 江苏大学 Method for detecting Q-switching energy and amplified spontaneous emission simultaneously for laser
CN202066590U (en) * 2011-02-22 2011-12-07 闫妍 Laser power detecting apparatus
CN102500923B (en) * 2011-09-21 2015-03-11 长春理工大学 Preparation device for preparing functional micro-nano materials on silicon surfaces based on femtosecond laser and method

Also Published As

Publication number Publication date
CN102747197A (en) 2012-10-24

Similar Documents

Publication Publication Date Title
CN111044613B (en) Metal plate micro-defect detection method based on nonlinear Lamb wave
Ostachowicz et al. Damage localisation in plate-like structures based on PZT sensors
Konstantinidis et al. The temperature stability of guided wave structural health monitoring systems
CN104215203B (en) A kind of deformation of transformer winding online test method and system based on ultrasonic wave
Burrows et al. Laser generation of Lamb waves for defect detection: experimental methods and finite element modeling
CN101722361B (en) Device and method for controlling residual stress on surface of metal microstructure
CN102156166B (en) Ultrasonic climbing wave detection method for laterally assembled fir tree blade root of steam turbine
Dong et al. Directional dependence of aluminum grain size measurement by laser-ultrasonic technique
CN103255268B (en) Method for optimizing thickness in process of simultaneously impacting alloy by using lasers from two sides
CN103837601B (en) A kind of broadband guided wave phase array focusing scan method and system
CN102747197B (en) Technological parameter real-time monitoring method for laser shock peening process
CN108548869A (en) A kind of nuclear power station polyethylene pipe phased array ultrasonic detecting method
Kusano et al. Mid-infrared pulsed laser ultrasonic testing for carbon fiber reinforced plastics
Gao et al. Defect detection using the phased-array laser ultrasonic crack diffraction enhancement method
CN106680372A (en) Correction method for evaluating crystalline grain size of metal material by stress influence ultrasonic waves
CN101395467B (en) Structure/material measuring device for metallic material
Zarei et al. Laser ultrasonics for nondestructive testing of composite materials and structures: a review
Kwon et al. High-frequency lowest torsional wave mode ultrasonic inspection using a necked pipe waveguide unit
CN106595926A (en) Correcting method for influences of grain size on ultrasonic evaluation for welding residual stress
CN109355490A (en) The processing method that a kind of laser shock in oblique angle strengthens complex parts
CN105584061A (en) Method and device for microwave nondestructive testing, quick repairing and real-time monitoring of composite material
CN104698086A (en) Nondestructive flaw detection method for one-dimensional stress waves based on time inversion and multipath effects
Fu et al. Artificial neural network-based damage detection of composite material using laser ultrasonic technology
CN105698988B (en) Hole diameter influences the modification method of critical refraction longitudinal wave evaluation metal material stress
Qi et al. Detection of parallel double crack in pressure vessel based on optical fibre ultrasonic sensing

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

Granted publication date: 20140402

Termination date: 20170629

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