Source: http://www.google.com/patents/US6805970?dq=6,360,693
Timestamp: 2016-08-31 07:22:41
Document Index: 554340905

Matched Legal Cases: ['art 13', 'art 13', 'art 13', 'art 13', 'art 13', 'art 13', 'art 47', 'art 47', 'art 57', 'art 57', 'art 73', 'art 73', 'art 73']

Patent US6805970 - Laser peening of components of thin cross-section - Google PatentsSearch Images Maps Play YouTube News Gmail Drive More »Sign inPatentsThe properties of a metal piece are altered by laser peening the piece on the first side using an acoustic coupling material operatively connected to the second side and subsequently laser peening the piece on the second side using an acoustic coupling material operatively connected to the first sid...http://www.google.com/patents/US6805970?utm_source=gb-gplus-sharePatent US6805970 - Laser peening of components of thin cross-sectionAdvanced Patent SearchPublication numberUS6805970 B2Publication typeGrantApplication numberUS 10/674,521Publication dateOct 19, 2004Filing dateSep 29, 2003Priority dateJan 25, 2001Fee statusPaidAlso published asUS6657160, US20020096503, US20040086738, WO2002059385A2, WO2002059385A3Publication number10674521, 674521, US 6805970 B2, US 6805970B2, US-B2-6805970, US6805970 B2, US6805970B2InventorsLloyd A. Hackel, John M. Halpin, Fritz B. Harris, Jr.Original AssigneeThe Regents Of The University Of CaliforniaExport CitationBiBTeX, EndNote, RefManPatent Citations (54), Referenced by (13), Classifications (20), Legal Events (6) External Links: USPTO, USPTO Assignment, EspacenetLaser peening of components of thin cross-section
US 6805970 B2Abstract
The properties of a metal piece are altered by laser peening the piece on the first side using an acoustic coupling material operatively connected to the second side and subsequently laser peening the piece on the second side using an acoustic coupling material operatively connected to the first side.
The invention claimed is: 1. A metal piece, having first side and a second side, produced by the method of:
laser peening all or a portion of the metal piece from the first side by directing at least one laser beam onto the metal piece from the first side creating a multiplicity of pressure pulses in the metal piece, operatively connecting an acoustic coupling material to the second side of the metal piece coupling said multiplicity of pressure pulses out of the metal piece from the second side, and maintaining said fluid acoustic coupling material operatively connected to the second side of the metal piece throughout said step of operatively connecting a fluid acoustic coupling material to the second side of the metal piece coupling said multiplicity of pressure pulses out of the metal piece from the second side, wherein said fluid acoustic coupling material functions to couple said multiplicity of pressure pulses out of the metal piece into said fluid acoustic coupling material throughout said step of operatively connecting a fluid acoustic coupling material to the second side of the metal piece coupling said multiplicity of pressure pulses out of the metal piece from the second side. 2. The metal piece produced by the method of claim 1, wherein said laser peening the metal piece from first the side creates a shock wave in the metal piece and wherein said acoustic coupling material couples a portion or all of the shock wave out of the metal piece from the second side.
3. The metal piece produced by the method of claim 1, wherein said laser peening said the metal piece from said the first side processes rectangular spots on the first side.
4. The metal piece produced by the method of claim 1, wherein said laser peening said the piece from said the first side utilizes a laser that provides a substantially rectangular spot.
5. The metal piece produced by the method of claim 1, including operatively connecting an acoustic coupling material to the first side of the metal piece and laser peening all or a portion of the metal piece from the second side.
6. The metal piece produced by the method of claim 5, wherein said laser peening the metal piece from the second side creates a shock wave in the metal piece and wherein said acoustic coupling material couples a portion or all of the shock wave out of the metal piece from the first side.
7. The metal piece produced by the method of claim 5, wherein said laser peening the metal piece from the second side processes rectangular spots on the second side.
8. The metal piece produced by the method of claim 5, wherein said laser peening the piece from the second side utilizes a laser that provides a substantially rectangular spot.
9. The metal piece produced by the method of claim 1, wherein said acoustic coupling material is a freon compound or water.
10. The metal piece produced by the method of claim 1, wherein said acoustic coupling material is a freon compound.
11. The metal piece produced by the method of claim 1, wherein said acoustic coupling material is water.
12. The metal piece produced by the method of claim 1, wherein said acoustic coupling material is fluorinet.
13. The metal piece produced by the method of claim 1, wherein said laser peening all or a portion of the metal piece from the first side includes operatively connecting an ablation layer of material to the first side of metal piece and transmitting laser light into said ablation layer of material.
14. The metal piece produced by the method of claim 13, wherein said laser light is transmitted into but not out of said ablation layer of material.
15. The metal piece produced by the method of claim 14, including operatively connecting a tamping layer to said ablation layer of material.
16. The metal piece of claim 1, produced by the method including the additional steps of operatively connecting an acoustic coupling material to the first side of said metal piece and laser peening the metal piece from the second side, wherein said laser peening is produced by laser pulses alternately directed onto the first side and the second side, wherein sequential laser pulses are stepped over the first side and over the second side while alternating between the first side and the second side.
17. The metal piece of claim 16, wherein said sequential laser pulses are stepped over the first side and over the second side while alternating between the first side and the second side on equivalent spots on the first side and the second side.
18. The metal piece of claim 17, wherein said equivalent spots on said the side and the second side are adjacent to each other.
This application is a division of application Ser. No. 09/771,179 filed Jan. 25, 2001 entitLed “Laser Peening of Components of Thin Cross-Sections” now U.S. Pat. No. 6,657,160 issued Dec. 2, 2003.
The present invention relates to industrial applications of lasers and more particularly to laser peening of metals.
Improving the strength of metals by cold working undoubtedly was discovered early in civilization, as ancient man hammered out his weapons and tools. Since the 1950s shot peening has been used as a means to improve the fatigue properties of metals. Another method of shock processing involves the use of high explosive materials in contact with the metal surface. The use of high intensity laser outputs for the generation of mechanical shock waves to treat the surfaces of metals has been well known since the 1970s. The laser shock process can be used to generate compressive stresses in the metal surfaces adding strength and resistance to corrosive failure. Lasers with pulse outputs of 10 to 100 J and pulse durations of 10 to 100 ns are useful for generating inertially confined plasmas on the surfaces of metals. These plasmas create pressures in the range of 10,000 to 100,000 atmospheres and the resulting shock pressure can exceed the elastic limit of the metal and thus compressively stress a surface layer as deep or deeper than 1 mm in the metals.
The article, “Blasts of Light to Strengthen Metals,” Science & Technology Review, October 1998, provides the following description: “At first glance, it would seem that bombarding a metal part with an intense stream of tiny metal or ceramic balls might not be the best approach for making that part more resistant to cracking and corrosion. And yet, shot peening is a tried-and-true technique for strengthening metals. Now a team of Lawrence Livermore researchers, in tandem with colleagues at New Jersey-based Metal Improvement Co. Inc., have replaced the tiny balls with short-lived, repetitive blasts of light from a reliable, high-powered laser.”
U.S. Pat. No. 4,401,477 for laser shock processing, by Clauer et al, patented Aug. 30, 1983, provides the following description “. . . constitutes an improvement of the U.S. Pat. No. 3,850,698 which is the basic method of laser shock processing a solid target with a radiation pulse of high power generation, the disclosure of which is herein incorporated by reference. The patented invention is particularly useful when the target material is sufficiently thick so that the stress wave does not penetrate to the back surface of the target material. Their more recent invention involved “the mounting of a trapping material (hereinafter referred to as a momentum trap) that is placed along the back surface of the metal substrate to be laser shock processed. It is important that the trap and the substrate have substantially the same acoustical impedance. Other material properties that are important are a matching of material densities, and sound speed. Preferably, the trap and the substrate are the same material, so that no matching is needed. The trap is placed against the back surface of the substrate, and mineral oil can be used there between to enhance the coupling of the materials. A spring-loaded, disk-shaped trapping material is placed against the substrate. An overlay material that is substantially transparent to laser radiation (e.g.—fused quartz, acrylic, water) is placed in direct contact with the front surface of the specimen. Initially the specimen is coated with a thin layer of paint, preferably black, to enhance absorption of the laser radiation and to protect the surface from melting by the radiation. A high power, pulsed laser emits a high intensity pulse of short duration radiation that passes through the overlay material, is absorbed by the paint, produces a high pressure condition at the front surface of the metal substrate, thereby driving a high amplitude stress wave into and through the metal substrate and into the momentum trap. The surface of the paint is vaporized when it is struck by the laser radiation causing an extremely high pressure near the surface when the vaporized gas is trapped between the specimen surface and the transparent overlay. At the back surface of the target specimen the stress wave passes into the momentum trap and is reflected back from the back surfaces. However, the momentum imparted to the trap by the reflected wave causes the spring loaded trap to break away and disconnect from the specimen after the stress wave is reflected from the back surface of the momentum trap and strike the common surface of the specimen and the trap. The momentum trap thereby carries away the tensile wave which would produce distortion in the specimen. Another means of absorbing the stress wave after it has passed through the metal substrate involves the use of a large mass of material, having a long dimension in the same direction as the stress wave, and having substantially the same acoustical impedance as the metal substrate. Being in direct contact with the metal substrate, and mounted so that the stress wave passes through the long dimension of the material mass, the stress wave is considerably weakened when it is reflected back to the common surface of the mass and the substrate. Copending patent application Ser. No. 334,612, now European Patent No. 085278A1 for split beam method of altering material properties, by Clauer et al, issued Aug. 10, 1983, discloses the use of a split beam to simultaneously laser shock the opposing two sides of the target material. However, the split beam method has several inherent disadvantages. 1. To shock process two sides simultaneously requires that the laser generate twice the power as for only doing one side. High powered lasers are extremely expensive and such cost may be prohibitive. 2. The split beam method requires the use of precisely calibrated and positioned lenses and mirrors. This precision may be difficult to achieve in a high production manufacturing environment. 3. In many applications only one side of the metal substrate is subject to fatigue, so there is no need to use the split beam method. In other applications, it is not possible to have line of sight access to both sides of the fatigue critical region for split beam processing.” This description of the process for simultaneous dual sided peening thin sections fails to adequately recognize or address the problem of internal spalling.”
U.S. Pat. No. 5,531,570 for distortion control for laser shock peened gas turbine engine compressor blade edges, by Mannava et al, patented Jul. 2, 1996, provides the following description, “A method for counteracting distortion of the airfoil caused by laser shock peening a gas turbine engine compressor metallic airfoil along its leading and/or trailing edge to form laser shock peened surfaces extending radially along at least a portion of the edges with a region having deep compressive residual stresses imparted by laser shock peening (LSP) extending into the airfoil from the laser shock peened surfaces.” Although this patent discusses distortion of the part shape, it also fails to address an effective approach to peening of thin components without internally spalling.
The present invention provides a system for altering the properties of a metal piece having first and second surfaces by a process of laser peening. In an embodiment of the invention, the properties of a metal piece having first side and a second side are altered by laser peening the piece on the first side using an acoustic coupling material operatively connected to the second side. In another embodiment of the invention, laser peening is employed from one side at a time with a material on the back side that couples a portion or all of the shock wave out of the metal. Other features and advantages of the present invention will become apparent from the following detailed description. It should be understood, however, that the detailed description and the examples, while indicating specific embodiments of the invention, are given by way of illustration only, since various changes and modifications within the spirit and scope of the invention will become apparent to those skilled in the art from this detailed description and by practice of the invention.
The accompanying drawings, which are incorporated into and constitute a part of the specification, illustrate embodiments of the invention and, together with the general description of the invention, and the detailed description of the embodiments, serve to explain the principles of the invention.
FIG. 1 shows a system for laser peening a part.
FIGS. 2A and 2B illustrate the behavior of the shock waves for dual sided and single sided peening.
FIG. 3 shows a counterbalancing effect.
FIG. 4 shows rectangular pulses systematically applied next to each other with just overlapping edges.
FIG. 5 shows a system for laser peening a part.
Referring now to the drawings, specific embodiments of the invention are illustrated. The detailed description of the specific embodiments, together with the general description of the invention, serve to explain the principles of the invention.
Improving the strength of metals by cold working undoubtedly was discovered early in civilization, as ancient man hammered out his weapons and tools. Since the 1950s shot peening has been used as a means to improve the fatigue properties of metals. At first glance, it would seem that bombarding a metal part with an intense stream of tiny metal or ceramic balls might not be the best approach for making that part more resistant to cracking and corrosion. And yet, shot peening is a tried-and-true technique for strengthening metals. The use of high intensity laser outputs for the generation of mechanical shock waves to treat the surfaces of metals has been well known since the 1970s. The laser shock process can be used to generate compressive stresses in the metal surfaces adding fatigue strength and resistance to corrosive failure.
The currently accepted practice for laser peening thin section materials, such as jet engine fan and compressor blades, is to apply a simultaneous laser pulse to each side of the piece being peened. This approach results from the belief that the simultaneous counter propagating shock waves will counteract the distortion associated with peening only one side at a time. However one can recognize that the simultaneous waves actually create a deleterious doubly intense tensile wave within the part. This intense tensile wave can undo the peening effect and actually rupture (spall) the interior material. The present invention employs laser peening from one side at a time and places a material on the back side that couples the shock wave out of the metal preventing its reflection and deleterious effect.
Referring now to FIG. 1, a system for laser peening a part is shown and designated generally by the reference numeral 10. The near field output of a beam from a laser such as a Nd:glass laser is image relayed to the part to be peened. The front surface of the part is coated with an ablative layer and a pressure confinement (tamping) layer of fluid is flowed over the ablative layer. This layer, transparent to the laser light, confines the plasma pressure that develops and greatly increases the intensity of the shock wave that transmits into the metal. In the recommended configuration, the laser beam output comprises a rectangular beam that allows precise and uniform overlap of pulses and hence highly uniform compressive stress from front to back side within the part. This minimizes distortion of the peened part.
It has become accepted practice in the laser peening of metal components with thin cross sections to simultaneously peen both sides with the intent of preventing component distortion. This technique is described in a European patent European Patent Application 82810554.4 filed Dec. 20, 1982 entitled “Split Beam Method of Altering Material Properties” by Clauer et al and U.S. Pat. No. 5,531,570 entitled “Distortion Control for Laser Shock Peened Gas Turbine Engine Compressor Blade Edges” by S. R. Mannava et al of General Electric Company.
It was believed that by bringing a split laser pulse to each side of the metal, nearly equal opposing forces and hence traveling shock waves could be generated to prevent “back-side” spallation or distortion of the metal. In the analysis that led to the present specific embodiments, it was learned that the propagation duration of the shock wave through the metal is substantially long, on the order of 200 ns, such that the typically 20 ns long duration laser pulse and its corresponding back pressure have long since ended before the shock wave reaches the output surface. Thus the intended effect of balancing the forces will not be realized. In fact, an adverse effect actually occurs in that as a shock wave reaches the metal to air (or plastic) interface at the far side of the part, it strongly reflects due to the impedance difference at the boundary and additionally the reflected shock wave is inverted becoming a tensile wave. The tensile waves resulting from each of the two reflected waves interfere near the center of the metal part causing a doubly intense cavitation force that can spall or split apart the metal in the center.
In the analysis that led to the present specific embodiments, it was discovered that improvement could be made by laser peening only one side of the thin section material at a time. A uniformly controlled, rectangular shaped laser pulse is incident from one (front) side only and creates a shock wave. On the back side a liquid such as water or fluorinert is flowed over the surface directly behind the area to be peened with a thickness of about 1 mm. Alternately a sound absorbing material can be pressed against the surface. Using the density of water as 1000 kg/m3 and the sound velocity as 1461 m/s, as the shock wave propagates to the back side a reflected wave is generated of intensity relative R=−0.84 for water.
As indicated by the negative sign, this wave propagates back as a tensile wave but because the thin material is being peened on only a single side, it now has no counter propagating wave with which to interfere. Thus the magnitude of the tensile force is reduced by a factor of 2.4 over that of dual sided peening, a factor that can be critical in preventing cavitation or spalling in the material.
Referring again to FIG. 1, The system 10 for laser peening a part is shown. The near field output of a beam from a laser 11 is image relayed by the optical imaging system 12 to the part 13 to be peened. The front surface 14 of the part 13 is coated with an ablative layer 16 and a pressure confinement (tamping) layer 17 of fluid is flowed over the ablative layer 16. The pressure confinement (tamping) layer 17 of fluid is provided by the tamping fluid source 22. This layer 17, transparent to the laser light 18, confines the plasma pressure that develops and greatly increases the intensity of the shock wave that transmits into the metal part 13. The part 13 is peened with an acoustic coupling material, shock absorbing layer 19. The acoustic coupling material, shock absorbing layer 19 can be a material such as water or fluorinert applied over the back side 15 of the part 13. The acoustic coupling material/shock absorbing layer 19 material is provided by the shock absorber fluid source 20. The laser beam output comprises a rectangular beam that allows precise and uniform overlap of pulses and hence highly uniform compressive stress from front to back side within the part. This minimizes distortion of the peened part. The part 13 is positioned within the system 10 by the part manipulator 21.
The behavior of the shock waves for dual sided and single sided peening is illustrated graphically in FIGS. 2A and 2B. The behavior of the shock waves for dual sided peening, designated generally by the reference numeral 30, is illustrated in FIG. 2A. The behavior of the shock waves for single sided peening, designated generally by the reference numeral 40, is illustrated in FIG. 2B.
As shown in FIG. 2A, laser beams 31 and 32 are simultaneously directed onto sides 35 and 36 respectively. The compressive pressure pulse T1, for example [1], from one side 35 has traversed to the opposite side 36 by the time the first pressure pulse T1[2] reaches its far side 36. Both pulses reflect from their respective back sides and form reverse traveling tensile waves. These waves constructively interfere near the middle of the material and form the doubly intense tensile force that can spall (tear apart) the metal in the center. There is also no apparent benefit to having a pressure pulse simultaneous on both sides.
As shown in FIG. 2b, a laser beam 41 is directed onto one side 45 of a part 47. The strain wave 43 propagates in from side 45. The compressive pressure pulse T1 from side 45 propagates from side 45. The analysis that led to the present specific embodiments focused on eliminating the dual counter propagating waves shown in FIG. 2A. In the present specific embodiments shown in FIG. 2B, the part 47 is peened on one side at a time with the acoustic coupling material 42, such as water or fluorinert, applied over the back side 46. The closer the acoustic impedance, given by the product of material density and speed of sound in the material, of the backing is to that of the material being peened, the greater fraction of the shock wave is coupled out. After peening a single layer of one side of a component, the component is rotated 180 degrees and the opposite side is peened again with a coupling material applied to the back side to couple out the acoustic shock wave. With careful placement of the peening to each side thereby producing equal counterbalancing compressive residual stress fields, distortion induced from peening the first side is fully removed.
The counterbalancing effect is illustrated in FIG. 3. A part 57 is shown at three different times in the process in FIG. 3. The part 57 shown in the middle view 52 is peened on the first side 54. As show in the views 51 and 52, peening an area 58 on one side of a thin section material will result in distortion curvature because of the residual compressive stress. As shown in view 53, peening on the first side 55 of a thin section material resulted in distortion curvature because of the residual compressive stress, but after peening in an equivalent stress 59 to the back side 56, the part will return to near straight condition.
This embodiment employs only laser peening from one side at a time and places a materiel on the back side that couples the shock wave out of the metal preventing its reflection and deleterious effect. It also uses a rectangular beam that allows precise and uniform overlap of pulses and hence highly uniform compressive stress from front to back side within the part. In treating an entire piece, using this uniform beam, one approach is to peen the desired area with a single layer placing the rectangular spots precisely adjacent to each other. After this first step the piece will distort in a convex shape with respect to the direction of laser peening. Next, the piece is flipped around and the reverse side peened with a matched layer generating an identical counterbalancing compressive residual stress field. As this laser peening is completed, the distortion is essentially removed. To impart multiple laser peening layers, the process can be repeated, by starting laser peening on the second side and positioning the individual laser peening spots so that the center of an individual spot coincides with the four-corner area of the previous laser peening pattern. After the second side is peened, the part is reversed and the second area is peened in a like manner.
In order to laser peen both sides of the thin section component with minimal distortion, several different approaches can be taken with respect to placing the individual pulses that comprise to overall treatment pattern. As discussed in the above referenced patents, previous workers have had difficulty with distortion believed to be primarily associated with the circular nature of their laser spot and its non-uniform intensity profile. This causes the generation of non-identical compressive residual stress fields on either side of the part, thus imparting distortion to the part's geometry.
U.S. patent application Ser. No. 09/133,590, filed Aug. 13, 1998, now U.S. Pat. No. 6,198,069 entitled “Laser Beam Temporal and Spatial Tailoring for Laser Shock Processing,” (the disclosure of which is incorporated herein by reference) describes an effective means for delivering highly uniform rectangular spots that provide excellent local uniformity. The U.S. patent application Ser. No. 09/133,590 invention is a method for formatting the laser spatial shape and for effectively and efficiently delivering the energy to a work surface in the laser shock process. An appropriately formatted pulse helps to eliminate breakdown and generate uniform shocks. The invention uses a high power laser technology capable of meeting the laser requirements for a high throughput process, that is, a laser which can treat many square centimeters of surface area per second.
Another means for delivering highly uniform rectangular spots is described in U.S. Pat. No. 5,689,363, entitled Long-Pulse-Width Narrow Bandwidth Solid State Laser. U.S. Pat. No. 5,689,363 is incorporated herein by reference. According to an embodiment disclosed therein, a laser head with rectangular slab amplifier comprises a laser system that emits a rectangular shaped beam with near diffraction-limited divergence and near transform-limited bandwidth. The system consists of one or more flashlamp-pumped Nd:glass zig-zag amplifiers, a very low threshold SBS phase conjugator system, and a self seeded single frequency Nd:YLF master oscillator. Completely passive polarization switching provides eight amplifier gain passes. Multiple frequency output can be generated by using SBS cells having different pressures of a gaseous SBS medium or different SBS materials. This laser system produces a long pulse, low divergence, narrow-bandwidth, multi-frequency output. Because of its high average power and high beam quality, this system has application in any process which would requires a long pulse format, including the material processing application of the present invention.
Referring now to FIG. 4, a component 62 being peened is shown and designated generally by the reference numeral 60. The component is handled by a part gripper and motion controller 65. A laser beam 61 is directed onto the component 62 being peened. The laser beam 61 produces a spot 63 on the component being peened. The peened area 64 is produced. As shown in FIG. 4, the rectangular pulses are systematically applied next to each other with just overlapping edges. This greatly minimizes distortion of the peened part because a highly uniform and highly repeatable stress is applied to each side of the part.
This laser peening or laser shock processing process is especially valuable for jet turbine engines. FAA Service Difficulty Reports show that there are an average of 15 uncontained rotor failures per year in the US involving turbine powered aircraft. Turbine engine uncontainment events were identified as the top priority by the Aerospace Industries Association Continued Airworthiness Assessment Methodoligies Report.
Laser peening or laser shock processing of the leading edge of turbine blades has been clearly shown to halt the growth of cracks and enormously reduce blade failure. The leading edges of these titanium alloy blades are 1 to a few millimeters in thickness and must be carefully treated in the laser peening or laser shock processing process to avoid damage and distortion. In the process developed and patented by personnel of LSP, Inc., of Dublin, Ohio, (European Patent Application 82810554.4 filed Dec. 20, 1982 entitled “Split Beam Method of Altering Material Properties” filed by Clauer et al) and a similar process patented by General Electric Aircraft Engines of Cincinnati, Ohio (U.S. Pat. No. 5,531,570 “Distortion Control for Laser Shock Peened Gas Turbine Engine Compressor Blade Edges” by S. R. Mannava et al of General Electric Company) the simultaneous peening or laser shock processing of both sides of the blade is described as the means to reduce distortion. As described in the GE patent, “the blade may have laser shock peened surfaces on both suction and pressure sides of the blade wherein both sides were simultaneously laser shock peened. The process is performed with circular shaped laser beams which is a consequence of the previous laser design and makes uniform overlap of the peened areas difficult. The inventors/authors describe “circular laser shocked areas such that the suction side pattern is different from the compression side pattern and each of the patterns includes overlapping rows of circular laser shocked areas.” The simultaneous peening or laser shock processing of both sides of the blade and the use of varying overlap of the circular patterns are described in the GE patent.
In the process, laser light of typically 100 to 200 J/cm2 passes through a confining layer (typically 1 mm thickness of water) and is incident on an ablation layer (typically a plastic of a few hundred micron thickness) to create a high pressure shock wave. Although the laser pulse lasts for only 20 ns, the shock wave propagates through the blade at acoustic sound speed which is approximately 4000 meters per second for titanium 6-4 alloy. In order to travel the blade thickness of 1 mm to 2 mm requires 250 ns to 500 ns. For a laser beam incident from each side simultaneously, the laser pulse and plasma pressure are well dissipated by the time the shock wave reaches the opposite side, hundreds of nanoseconds later. The plasma pressure of about 70 kbar that formed on each side during the incident pulse has lifted the water covering layer off the surface by approximately 40 microns. Now the backside has just the ablation layer which is a poor acoustic match to the metal and beyond it a void left by the displaced water layer. With this interface situation, the acoustic shock wave will mostly reflect as a tensile wave back into the metal. The intensity of the reflected stress wave will be given by the formula (see “Behavior of Metals Under Implusive Loads” by John s. Rinehard and John Pearson, page 42, Dover Publications, Inc., New York 1954);
R=(ρ1 c 1−ρ1 c 1)/(ρ1 c 1−ρ1 c 1) Where ρ1 is the metal density, ρ2 is the density of the material just across the boundary (one atmosphere of air or the impedance of the remaining ablation layer since the pressure pulse has dissipated), c1 and c2 are the velocities of sound in the respective media. For Titanium with a density of 4500 kg/m3 and a sound velocity of 4000 m/s and air with a density of 1.29 kg/m3 and a sound velocity of 340 m/s the reflected intensity is R=−1 where the minus sign indicates a tensile reflected wave.
For dual sided peening, a strong tensile wave reflects from both sides of the metal/air interface and can overlap in the center forming a tensile wave of twice the incident stress. This strong tensile stress can cause cavitation and spalling within the metal. For air or the low density ablation layer the reflectivity is essentially unity.
A uniformly controlled, rectangular shaped laser pulse is incident from one (front) side only and creates a shock wave. On the back side a liquid such as water or fluorinert is flowed over the surface directly behind the area to be peened with a thickness of about 1 mm. Alternately a sound absorbing material can be pressed against the surface. Using the density of water as 1000 kg/m3 and the sound velocity as 1461 m/s as the shock wave propagates to the back side the reflected wave is now of intensity R=−0.84 for water
This wave propagates back as a tensile wave but now has no counter propagating wave with which to interfere. Thus the magnitude of the tensile force is reduced by a factor of 2.4 a factor that can be critical in preventing cavitation or spalling in the material.
Referring now to FIG. 5, an alternate approach to dual sided laser peening of thin sections is to peen individual spots first on the front side and then on the backside. The structural elements of the system are shown. A Nd:glass Laser 71 produces laser beam 81. The polarization rotator 72 provides the position of � polarization shifter and causes the beam to take propagate along one of two paths, either up/to right or horizontal/up/to left path. A polarization beam splitter 79 controls the polarization of the laser 71 to be either transverse electric or transverse magnetic causing the beam 81 to either pass through the splitter 79 or reflect off of it. The part 73 is handled by the motion controller 74 which moves the part 73 after 2nd, 4th, 6th, . . . pulse. The surface of the part 73 is coated with an ablative layer 78 and a pressure confinement (tamping) layer 77. The polarization rotator 72 provides for two alternate beam paths 75 and 76. One beam path 75 images the beam onto the front side 75. This side fires for pulses 1,3,7 etc. One beam path imaging the beam onto the back side 76. This side fires for pulses 2,4,6, etc. This allows local laser peening of the front side and back side on sequential laser pulses.
To accomplish the dual sided laser peening, the single beam 81 output of the laser 71 passes through a polarization rotator 72 and then onto a polarization beam splitter 79. By controlling the polarization of the laser 71 to be either transverse electric or transverse magnetic, the beam 81 can be made to either pass through the splitter 79 or reflect off of it. This provides for two possible beam paths 75 and 76 one imaging the beam onto the front side 75 and one onto the back side 76. This allows local laser peening of the front side and back side on sequential laser pulses. The desired surface area is then treated by stepping pulses over the desired peening area while alternating between front and back sides of the piece.
Patent CitationsCited PatentFiling datePublication dateApplicantTitleUS3850698Jun 23, 1972Nov 26, 1974Ind Materials LtdAltering material propertiesUS4401447Jul 25, 1980Aug 30, 1983Multiform Desiccants, Inc.Self-retaining adsorbent bag unitUS4401477May 17, 1982Aug 30, 1983Battelle Development CorporationLaser shock processingUS4937421Jul 3, 1989Jun 26, 1990General Electric CompanyLaser peening system and methodUS5394875Oct 21, 1993Mar 7, 1995Lewis; Judith T.Automatic ultrasonic localization of targets implanted in a portion of the anatomyUS5492447Oct 6, 1994Feb 20, 1996General Electric CompanyLaser shock peened rotor components for turbomachineryUS5522706Oct 6, 1994Jun 4, 1996General Electric CompanyLaser shock peened disks with loading and locking slots for turbomachineryUS5525429Mar 6, 1995Jun 11, 1996General Electric CompanyLaser shock peening surface enhancement for gas turbine engine high strength rotor alloy repairUS5531570Mar 6, 1995Jul 2, 1996General Electric CompanyDistortion control for laser shock peened gas turbine engine compressor blade edgesUS5569018Mar 6, 1995Oct 29, 1996General Electric CompanyTechnique to prevent or divert cracksUS5584586Mar 4, 1996Dec 17, 1996General Electric CompanyLaser shock peened bearingsUS5584662Mar 6, 1995Dec 17, 1996General Electric CompanyLaser shock peening for gas turbine engine vane repairUS5591009Jan 17, 1995Jan 7, 1997General Electric CompanyLaser shock peened gas turbine engine fan blade edgesUS5620307Mar 6, 1995Apr 15, 1997General Electric CompanyLaser shock peened gas turbine engine blade tipUS5671628Dec 18, 1995Sep 30, 1997General Electric CompanyLaser shock peened diesUS5674328Apr 26, 1996Oct 7, 1997General Electric CompanyDry tape covered laser shock peeningUS5674329Apr 26, 1996Oct 7, 1997General Electric CompanyAdhesive tape covered laser shock peeningUS5675892Jun 20, 1996Oct 14, 1997General Electric CompanyLaser shock peening for gas turbine engine vane repairUS5730811Dec 21, 1995Mar 24, 1998General Electric CompanyCavity dumped laser shock peening processUS5735044Dec 12, 1995Apr 7, 1998General Electric CompanyLaser shock peening for gas turbine engine weld repairUS5741559Oct 23, 1995Apr 21, 1998Lsp Technologies, Inc.Laser peening process and apparatusUS5742028Jul 24, 1996Apr 21, 1998General Electric CompanyPreloaded laser shock peeningUS5744781Aug 7, 1995Apr 28, 1998General Electric CompanyMethod and apparatus for laser shock peeningUS5756965Nov 13, 1996May 26, 1998General Electric CompanyOn the fly laser shock peeningUS5846054Oct 6, 1994Dec 8, 1998General Electric CompanyLaser shock peened dovetails for disks and bladesUS5846057Mar 25, 1997Dec 8, 1998General Electric CompanyLaser shock peening for gas turbine engine weld repairUS5911890Feb 25, 1997Jun 15, 1999Lsp Technologies, Inc.Oblique angle laser shock processingUS5911891Sep 11, 1997Jun 15, 1999Lsp Technologies, Inc.Laser shock peening with tailored multiple laser beamsUS5932120Dec 18, 1997Aug 3, 1999General Electric CompanyLaser shock peening using low energy laserUS5935464Sep 11, 1997Aug 10, 1999Lsp Technologies, Inc.Laser shock peening apparatus with a diffractive optic elementUS5948293Dec 3, 1998Sep 7, 1999General Electric CompanyLaser shock peening quality assurance by volumetric analysis of laser shock peened dimpleUS5951790Jun 26, 1998Sep 14, 1999General Electric CompanyMethod of monitoring and controlling laser shock peening using an in plane deflection test couponUS5980101Oct 31, 1997Nov 9, 1999General Electric CompanyMethod and apparatus for measuring laser pulse energyUS5987042Oct 31, 1997Nov 16, 1999General Electric CompanyMethod and apparatus for shaping a laser pulseUS5987991Jan 2, 1998Nov 23, 1999General Electric CompanyDetermination of Rayleigh wave critical angleUS5988982Sep 9, 1997Nov 23, 1999Lsp Technologies, Inc.Altering vibration frequencies of workpieces, such as gas turbine engine bladesUS6002102Feb 25, 1997Dec 14, 1999Lsp Technologies, Inc.Hidden surface laser shock processingUS6002706Dec 30, 1997Dec 14, 1999General Electric CompanyMethod and apparatus for controlling the size of a laser beamUS6005219Dec 18, 1997Dec 21, 1999General Electric CompanyRipstop laser shock peeningUS6021154Nov 21, 1997Feb 1, 2000General Electric CompanyLaser shock peening method and reflective laser beam homogenizerUS6045035Nov 4, 1997Apr 4, 2000Microflex CorporationInterlocking mailing packageUS6049058Dec 15, 1998Apr 11, 2000Lsp Technologies, Inc.Laser peening process and apparatus with uniform pressure pulse confinementUS6057003Jun 13, 1997May 2, 2000Lsp Technologies, Inc.Peening process with reduction of dielectric breakdown to increase peak pressure pulseUS6075593Aug 3, 1999Jun 13, 2000General Electric CompanyMethod for monitoring and controlling laser shock peening using temporal light spectrum analysisUS6078022Dec 30, 1997Jun 20, 2000Lsp Technologies, Inc.Laser peening hollow core gas turbine engine bladesUS6127649Dec 8, 1999Oct 3, 2000Lsp Technologies, Inc.Process chamber for laser peeningUS6130400Jun 26, 1998Oct 10, 2000General Electric CompanyBallistic momentum apparatus and method for monitoring and controlling laser shock peeningUS6144012Nov 5, 1997Nov 7, 2000Lsp Technologies, Inc.Efficient laser peeningUS6155789Apr 6, 1999Dec 5, 2000General Electric CompanyGas turbine engine airfoil damper and method for productionUS6198069 *Aug 13, 1998Mar 6, 2001The Regents Of The University Of CaliforniaLaser beam temporal and spatial tailoring for laser shock processingUS6320989Jan 22, 1999Nov 20, 2001Harris CorporationStepped acoustic impedance-matching transformer for very narrow channel acoustic traveling wave lens waveguideUS6333488Aug 30, 1999Dec 25, 2001General Electric CompanyMethod for setting up and controlling confinement media flow in laser shock peeningUS6559415 *Jul 12, 2002May 6, 2003General Electric CompanySingle sided laser shock peeningEP0085278A1Dec 20, 1982Aug 10, 1983Battelle Development CorporationSplit beam method of altering material properties* Cited by examinerReferenced byCiting PatentFiling datePublication dateApplicantTitleUS7960671Dec 7, 2006Jun 14, 2011Metal Improvement Company LlcLaser shock processing with momentum trapUS8256116 *Sep 24, 2008Sep 4, 2012SnecmaMethod of using laser shock impacts to produce raised elements on a wall surface capable of being swept by a fluid in order to control the intensity of turbulence in a transition zoneUS8322004Apr 29, 2009Dec 4, 2012Caterpilar Inc.Indirect laser induced residual stress in a fuel system component and fuel system using sameUS8455793Jun 4, 2013Frank's International, Inc.Laser shock peeningUS8607456Aug 9, 2012Dec 17, 2013SnecmaMethod of using laser shock impacts to produce raised elements on a wall surface capable of being swept by a fluid in order to control the intensity of turbulence in a transition zoneUS9227268Mar 31, 2008Jan 5, 2016Lsp Technologies, Inc.Methods, systems, and apparatuses for laser shock peening metal materialsUS20050205529 *Mar 21, 2005Sep 22, 2005The Regents Of The University Of CaliforniaCalibration system for laser peeningUS20070138157 *Dec 7, 2006Jun 21, 2007Metal Improvement Company LlcLaser Shock Processing With Momentum TrapUS20090083979 *Sep 24, 2008Apr 2, 2009SnecmaMethod for forming raised elements disruptive of the boundary layerUS20090230104 *Mar 11, 2009Sep 17, 2009Frank's International, Inc.Laser shock peeningUS20100066809 *Mar 18, 2010Cdm Optics, Inc.Deployable Image SensorUS20100276520 *Apr 29, 2009Nov 4, 2010Caterpillar Inc.Indirect laser induced residual stress in a fuel system component and fuel system using sameWO2007076330A2 *Dec 18, 2006Jul 5, 2007Metal Improvement Company LlcLaser shock processing with momentum trap* Cited by examinerClassifications U.S. Classification428/544, 148/525, 219/121.85, 428/687, 428/610, 148/565International ClassificationB23K26/073, C21D10/00Cooperative ClassificationB23K26/0884, Y10T428/12, B23K26/0732, C21D2221/00, Y10T428/12458, Y10T428/12993, C21D10/005, B23K26/0069European ClassificationB23K26/08L2B, B23K26/073B, C21D10/00L, B23K26/00J1Legal EventsDateCodeEventDescriptionSep 30, 2003ASAssignmentOwner name: REGENTS OF THE UNIVERSITY OF CALIFORNIA, THE, CALIFree format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:HACKEL, LLOYD A.;HALPIN, JOHN M.;REEL/FRAME:014574/0970Effective date: 20010112Apr 17, 2008FPAYFee paymentYear of fee payment: 4Jun 23, 2008ASAssignmentOwner name: LAWRENCE LIVERMORE NATIONAL SECURITY LLC, CALIFORNFree format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:THE REGENTS OF THE UNIVERSITY OF CALIFORNIA;REEL/FRAME:021217/0050Effective date: 20080623Mar 5, 2012FPAYFee paymentYear of fee payment: 8Apr 28, 2016FPAYFee paymentYear of fee payment: 12Apr 28, 2016SULPSurcharge for late paymentYear of fee payment: 11RotateOriginal ImageGoogle Home - Sitemap - USPTO Bulk Downloads - Privacy Policy - Terms of Service - About Google Patents - Send FeedbackData provided by IFI CLAIMS Patent Services