WO2003059568A1 - Procede d'usinage laser d'une piece par agrandissement de point laser - Google Patents

Procede d'usinage laser d'une piece par agrandissement de point laser Download PDF

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Publication number
WO2003059568A1
WO2003059568A1 PCT/US2003/000686 US0300686W WO03059568A1 WO 2003059568 A1 WO2003059568 A1 WO 2003059568A1 US 0300686 W US0300686 W US 0300686W WO 03059568 A1 WO03059568 A1 WO 03059568A1
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WO
WIPO (PCT)
Prior art keywords
laser
positioning system
primary
fast
accelerations
Prior art date
Application number
PCT/US2003/000686
Other languages
English (en)
Inventor
Donald R. Cutler
Original Assignee
Electro Scientific Industries, Inc.
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 Electro Scientific Industries, Inc. filed Critical Electro Scientific Industries, Inc.
Priority to KR1020047010540A priority Critical patent/KR100982677B1/ko
Priority to DE10392185T priority patent/DE10392185T5/de
Priority to CA002469520A priority patent/CA2469520A1/fr
Priority to GB0412827A priority patent/GB2397545B/en
Priority to AU2003214818A priority patent/AU2003214818A1/en
Priority to JP2003559716A priority patent/JP4340745B2/ja
Publication of WO2003059568A1 publication Critical patent/WO2003059568A1/fr

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/064Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/08Devices involving relative movement between laser beam and workpiece
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/08Devices involving relative movement between laser beam and workpiece
    • B23K26/083Devices involving movement of the workpiece in at least one axial direction
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/38Removing material by boring or cutting
    • B23K26/382Removing material by boring or cutting by boring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/38Removing material by boring or cutting
    • B23K26/382Removing material by boring or cutting by boring
    • B23K26/389Removing material by boring or cutting by boring of fluid openings, e.g. nozzles, jets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/40Removing material taking account of the properties of the material involved
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K3/00Apparatus or processes for manufacturing printed circuits
    • H05K3/0011Working of insulating substrates or insulating layers
    • H05K3/0017Etching of the substrate by chemical or physical means
    • H05K3/0026Etching of the substrate by chemical or physical means by laser ablation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/36Electric or electronic devices
    • B23K2101/42Printed circuits
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/08Non-ferrous metals or alloys
    • B23K2103/12Copper or alloys thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/30Organic material
    • B23K2103/42Plastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/50Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/50Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26
    • B23K2103/52Ceramics

Definitions

  • the present invention relates to laser micromachining and, in particular, to a method and apparatus employing an fast steering mirror to move a laser spot having a focused spot size in a desired pattern on a substrate to remove a target area that is larger than the focused spot size on the substrate.
  • MCMs and high-density interconnect circuit boards, that have become the most preferred components of the electronics packaging industry.
  • Devices for packaging single chips such as ball grid arrays, pin grid arrays, circuit boards, and hybrid microcircuits typically include separate component layers of metal and an organic dielectric and/or reinforcement materials, as well as other new materials.
  • Much recent work has been directed toward developing laser-based micromachining techniques to form vias in, or otherwise process, these types of electronic materials . Vias are discussed herein only by way of example to micromachining and may take the form of complete through-holes or incomplete holes called blind vias.
  • UV lasers currently used in micromachining operations produce relatively small spot sizes compared to the kerf widths and hole diameters desired for many applications.
  • Laser machining throughput for creation of such feature geometries that are large compared to the laser spot size, hereinafter referred to as "contoured machining,” may be increased by employing a larger and lower power density laser beam. As described in U.S. Pat. No. 5,841,099, by operating the laser out of focus, Owen et al.
  • U.S. Pat. No. 4,461,947 of Ward discloses a method of contoured drilling in which a lens is rotated within a plane perpendicular to an incident laser beam to affect a target area that is greater in size than that of the focused laser spot.
  • the lens rotation is independent of the position of the supporting mounting arm.
  • Ward also discloses a prior art method of contoured drilling that relies on movement of the mounting arm within a plane to effect lens rotation.
  • the beam may be rotated by a rotating mirror.
  • U.S. Pat. No. 5,571,430 of Kawasaki et al. discloses a laser welding system that employs a concave condensing mirror that is pivotal about a first axis and supported by a rotary support member on a bearing such that the mirror is rotatable about a second axis perpendicular to the first axis.
  • the mirror is oscillated about the first axis to increase the "width" of target removed and rotated about the second axis to create an annular pattern.
  • An object of the present invention is, therefore, to provide a method or apparatus for quickly spatially spreading out the focused laser spots, and therefore the energy density, of high repetition rate laser pulses.
  • Another object of the invention is rapidly create geometric features having dimensions greater than those of the focused laser spot.
  • a further object of the invention is to improve the throughput and/or quality of work pieces in such laser machining operations.
  • U.S. Pat. Nos. 5,751,585 and 5,847,960 of Cutler et al. and U.S. Pat. No. 6,430,465 B2 of Cutler include descriptions of split-axis positioning systems, in which the upper stage is not supported by, and moves independently from, the lower stage and in which the work piece is carried on one axis or stage while the tool is carried on the other axis or stage.
  • These positioning systems have one or more upper stages, which each support a fast positioner, and can process one or multiple work pieces simultaneously at high throughput rates because the independently supported stages each carry less inertial mass and can accelerate, decelerate, or change direction more quickly than can those of a stacked stage system.
  • the resonance frequencies for a given load are increased.
  • the slow and fast positioners are adapted to move, without necessarily stopping, in response to a stream of positioning command data while coordinating their individually moving positions to produce temporarily stationary tool positions over target locations defined by the database.
  • These split-axis, multirate positioning systems reduce the fast positioner movement range limitations of prior systems while providing significantly increased tool processing throughput and can work from panelized or unpanelized databases.
  • split-axis positioning systems are becoming even more advantageous as the overall size and weight of the work pieces increase, utilizing longer and hence more massive stages, they may not provide sufficient bandwidth to effectively spread out the energy by large geometric spacing between the laser pulses at high pulse repetition frequencies (PRFs).
  • PRFs pulse repetition frequencies
  • the present invention employs, therefore, an fast steering mirror, such as a piezoelectrically controlled mirror, in the beam path to continuously move the laser beam in a high speed prescribed pattern about a nominal target position to spatially separate the focused laser spots generated at a high laser repetition rate and thereby create geometric features having dimensions greater than those of the focused laser spot.
  • an fast steering mirror such as a piezoelectrically controlled mirror
  • the invention permits a series of laser pulses at a given repetition rate to appear as a series of larger diameter pulses at a lower pulse rate without the beam quality problems associated with working out of focus.
  • FIG. 1 is a partly isometric and partly schematic view of a simplified laser system incorporating fast steering mirror in accordance with present invention.
  • FIG. 2 is a partly pictorial and partly schematic view of an fast steering mirror mechanism employed in the laser system of FIG. 1.
  • FIG. 3 is a partly sectional and partly schematic view of an fast steering mirror mechanism employed in the laser system of FIG. 1.
  • FIG. 4 is a frontal view of the fast steering mirror demonstrating how mirror flexion can affect the position of the laser spot.
  • FIG. 5 is computer model of an exemplary straight line kerf-forming profile enhanced by movement of an fast steering mirror in accordance with the present invention.
  • FIG. 6 is computer model of an exemplary via drilling profile enhanced by movement of an fast steering mirror in accordance with the present invention.
  • an exemplary embodiment of a laser system 10 of the present invention includes Q-switched, diode-pumped (DP), solid-state (SS) laser 12 that preferably includes a solid-state lasant.
  • DP diode-pumped
  • SS solid-state laser 12
  • pumping sources other than diodes such as a krypton arc lamp
  • the pumping diodes, arc lamp, or other conventional pumping means receive power from a power supply (not shown separately) which may form part of laser 12 or may be positioned separately.
  • the exemplary laser 12 provides harmonically generated laser output 14 of one or more laser pulses having primarily a TEMoo spatial mode profile.
  • Preferred laser wavelengths from about 150 nanometers (nm) to about 2000 nm include, but are not limited to, 1.3, 1.064, or 1.047, 1.03-1.05, 0.75-0.85 microns ( ⁇ m) or their second, third, fourth, or fifth harmonics from Nd:YAG, Nd.YLF, Nd:YVO 4 , Nd:YAP, Yb:YAG, or Ti:Sapphire lasers 64.
  • Such harmonic wavelengths may include, but are not limited to, wavelengths such as about 532 nm (frequency doubled Nd:YAG), 355 nm (frequency tripled Nd.YAG), 266 nm (frequency quadrupled Nd:YAG), or 213 nm (frequency quintupled Nd.YAG).
  • Lasers 12 and harmonic generation techniques are well known to skilled practitioners. Details of one exemplary laser 12 are described in detail in U.S. Pat. No. 5,593,606 of Owen et al.
  • An example of a preferred laser 12 includes a Model 210 UV-3500 laser sold by Lightwave Electronics of Mountain View, California.
  • laser output 14 may be manipulated by a variety of well-known optics including beam expander lens components 16 that are positioned along beam path 18 before being directed by a series of beam-directing components 20 (such as stage axis positioning mirrors), fast steering mirror FSM (30), and fast positioner 32 (such as a pair of galvanometer-driven X- and Y- axis mirrors) of beam positioning system 40.
  • beam-directing components 20 such as stage axis positioning mirrors
  • FSM fast steering mirror FSM
  • fast positioner 32 such as a pair of galvanometer-driven X- and Y- axis mirrors
  • laser output 14 is passed through a objective lens 42, such as a focusing or telecentric scan lens, before being applied as laser system output beam 46 with laser spot 48 at work piece 50.
  • objective lens 42 such as a focusing or telecentric scan lens
  • a preferred beam positioning system 40 is described in detail in U.S. Pat. No. 5,751,585 of Cutler et al. and may include ABBE error correction means described in U.S. Pat. No. 6,430,465 B2 of Cutler.
  • Beam positioning system 40 preferably employs a translation stage positioner that preferably controls at least two platforms or stages 52 and 54 and supports positioning components 20 to target and focus laser system output beam 46 to a desired laser target position 60.
  • the translation stage positioner is a split-axis system where a Y stage 52, typically moved by linear motors, supports and moves work piece 50 along rails 56, an X stage 54 supports and moves fast positioner 32 and objective lens 42 along rails 58, the Z dimension between the X and Y stages is adjustable, and beam-directing components 20 align the beam path 18 through any turns between laser 12 and FSM 30.
  • a typical translation stage positioner is capable of a velocity of 500 mm/sec and an acceleration of 1.5 G.
  • the combination of the fast positioner 32 and one or more translation stages 52 and/or 54 may be referred to as a primary or integrated positioning system.
  • Beam positioning system 40 permits quick movement between target positions 60 on the same or different circuit boards or chip packages to effect unique or duplicative processing operations based on provided test or design data.
  • An exemplary fast positioner is capable of a velocity of 400 or 500 mm/sec and an acceleration of 300 or 500 G, and hence these are also the typical capabilities of an exemplary integrated positioning system.
  • An example of a preferred laser system 10 that contains many of the above-described positioning system components is a Model 5320 laser system or others in its series manufactured by Electro Scientific Industries, Inc. (ESI) in Portland, Oregon. Skilled persons will appreciate, however, that a system with a single X-Y stage for work piece positioning and a fixed beam position and/or stationary galvanometer for beam positioning may alternatively be employed.
  • a laser system controller 62 preferably synchronizes the firing of laser 12 to the motion of stages 52 and 54 and fast positioner 32 in a mamier well known to skilled practitioners.
  • Laser system controller 62 is shown generically to control fast positioner 32, stages 52 and 54, laser 12, and FSM controller 64. Skilled persons will appreciate that laser system controller 62 may include integrated or independent control subsystems to control and/or provide power to any or all of these laser components and that such subsystems may be remotely located with respect to laser system controller 62.
  • Laser system controller 62 also preferably controls the movement, including direction, tilt angles or rotation, and speed or frequency, of FSM 30, either directly or indirectly through a mirror controller 64, as well as controls any synchronization with laser 12 or components of positioning system 40.
  • the parameters of laser system output beam 46 are selected to facilitate substantially clean, sequential drilling, i.e. , via formation, in a wide variety of metallic, dielectric, and other material targets that may exhibit different optical absorption, ablation threshold, or other characteristics in response to UV or visible light.
  • Exemplary parameters of laser system output include average energy densities greater than about 120 micro Joules ( ⁇ J) measured over the beam spot area, preferably greater than 200 ⁇ J; spot size diameters or spatial major axes of less than about 50 ⁇ m, and preferably from about 1- 50 ⁇ m, and typically from about 20-30 ⁇ m; a repetition rate of greater than about 1 kiloHertz (kHz), preferably greater than about 5 kHz, and most preferably even higher than 20 kHz; and a wavelength preferably between about 150-2000 nm, more preferably between about 190-1325 nm, and most preferably between about 266 nm and 532 nm.
  • ⁇ J micro Joules
  • laser system output beam 46 The preferred parameters of laser system output beam 46 are selected in an attempt to circumvent certain thermal damage effects by utilizing temporal pulse widths that are shorter than about 100 nanoseconds (ns), and preferably from about 0.1 picoseconds (ps) to 100 ns, and more preferably from about 1-90 ns or shorter. Skilled persons will appreciate that these parameters will vary and can be optimized for the material to be processed, and that different parameters may be used to process different target layers. [0028] Laser system output beam 46 preferably produces a spot area 48 of a diameter of less than about 25-50 ⁇ m at beam position 60 on work piece 50.
  • spot area 48 and diameter generally refer to 1/e 2 dimensions, especially with respect to the description of laser system 10, these terms are occasionally used to refer to the spot area or diameter of the hole created by a single pulse.
  • spot area 48 of output beam 46 is generally circular, but may be shaped to be substantially square.
  • output beam 46 can be imaged or clipped of its wings or tails, particularly for first step processing, if desired for specific operations.
  • Fig. 2 shows a preferred embodiment of an FSM 30 that is positioned to receive laser output 14, deflect it through fast positioner 32, through objective lens 42 to a target position 60 on work piece 50 for the purpose of ECB via drilling, circuit element trimming, or other micro-machining applications.
  • FSM 30 is preferably implemented as part of a limited deflection beam positioning stage employing electrostrictive actuators having a higher frequency response than the fast positioner 32.
  • FSM 30 is deflected by ferroelectric ceramic actuator material, such as lead magnesium niobate (PMN), actuators 22 that translate voltage into displacement.
  • PMN material is similar to the more common piezoelectric actuator material but has less than 1 percent hysteresis, high electromechanical conversion efficiency, exhibits wide operating and manufacturing temperature ranges, does not require permanent polarization, and provides useful mechanical activity with small electrical drive voltages.
  • Exemplary PMN actuators 22 have a limited displacement of about 20 microns for a 40 mm long cylinder of PMN material, but have a very high stiffness of about 210 Newtons per micron for a 5 mm diameter cylinder.
  • FSM 30 is coupled through a flexure to three PMN actuators 22 having first ends arranged as an equilateral triangle having its center aligned with a center 24 of FSM 120.
  • the second ends of PMN actuators 22 are mechanically coupled to a mount 26 that attaches to X-axis translation stage 54.
  • the three PMN actuators 22 are preferably implemented in a 3 -degree of freedom configuration that is used in a 2-degree of freedom mode to tilt and tip FSM 30.
  • the three PMN actuators 22 are preferably formed as a hollow cylinder of PMN material that is electrically circumferentially divided into three active regions. Activating a region causes it to expand or contract, thereby tipping or tilting FSM 30.
  • the actuator triangle has 5 mm sides such that FSM 30 can be deflected at about a +4 milliRadian ("mRad”) angle, which translates into a + 640 micron deflection of laser output 14 when projected onto work piece 50 with an 80 mm objective lens 42.
  • An exemplary FSM 30 may provide a typical range of travel limit that limits the pattern dimension to up to about 25 or 50 times the laser spot size; however, a the maximum frequency response of the FSM 30 may be a more constraining limit that limits the pattern dimension to up to about 15 times the laser spot size, and typically up to 5 to 10 times the laser spot size.
  • FSM 30 operates at higher frequencies and accelerations than exemplary galvanometer-driven X- and Y- axis mirrors of fast positioner 32.
  • An exemplary FSM 30 of the nonintegrated positioning system provides velocities of greater than 1,000 mm/sec and may be capable of velocities of 4,000 mm/sec or higher, which are 5 to 10 times the velocity of the typical integrated positioning system.
  • An exemplary FSM 30 of the nonintegrated positioning system provides accelerations of greater than 1,000 G and may be capable of accelerations of 30,000 G or greater, which are 50 to 100 times the acceleration of the typical integrated positioning system.
  • exemplary PMN actuators 22 have about a 2.0 microFarad characteristic capacitance, 1.0 ohm DC impedance, 17 ohms impedance at 5 kHz, and draws over three amperes of current at 75 volts of drive.
  • the exemplary PMN actuator 22 driving FSM 30 has a large-signal bandwidth greater than about 5 kHz, a small-signal bandwidth greater than about 8 kHz, and a deflection angle of at least about 4 mRad for deflecting laser output 14 with about ⁇ 0.5 micron positioning resolution.
  • Skilled persons will appreciate that any other precision high-bandwidth actuators could be employed for mirror actuators 22.
  • FIG. 3 is a partly sectional and partly schematic view of an alternative FSM 30 along with some exemplary control circuitry 70 of an exemplary mirror controller 64 for mirror actuators 72a and 72b (generically mirror actuators 72), which are preferably piezoelectric-type (PZT) devices, that are employed to make small changes in the angle of FSM 30 resulting in small changes in the angle of laser system output beam 46 that causes small changes in the position 60 of the laser spot 48 at the surface of work piece 50.
  • FIG. 4 is a frontal view of FSM 30 demonstrating how mirror flexion can affect the position 60 of the laser spot 48.
  • one corner of a generally rectangular FSM 30 is anchored to a reference structure with a flexure that can flex but not compress or stretch.
  • Two other corners of FSM 30 are driven by the piezoelectric mirror actuators 72a and 72b in response to sine waves to introduce small angles into the beam path 18 that cause small changes in the beam position of laser spot 48 superimposed on target positions 60 established by other components of beam positioning system 40.
  • the sine (a) signal 74 drives the piezoelectric mirror actuators 72a and 72b in opposite directions to create an angle change in one direction
  • the sine (a +90 degrees) signal 76 drives the piezoelectric mirror actuators 72a and 72b in the same direction by sine to create an angle change at 90 degrees to the first angle change.
  • the laser output 14 is reflected off FSM 30 at a point approximately in the center. This results in a circle motion at the work surface after the small angles introduced by the mirror movement are converted to position changes by the scan lens 42.
  • a preferred objective lens focal length is about 50- 100 mm, and a preferred distance from the FSM 30 to scan lens 42 is as small as practical within design constraints and preferably less than about 300 mm, and more preferably less than 100 mm, when the Z stage (not shown) is at its normal focus height.
  • FSM 30 is mounted up stream of fast positioner 32 on the X stage 54 and replaces the final turn mirror of some conventional beam positioning systems.
  • FSM 30 is adapted for easy upgrade of existing lasers and positioning systems 40, such as employed in models 5200 or 5320 manufactured by Electro Scientific Industries, Inc. of Portland Oregon, and can be easily exchanged for the final turn mirror on the X stages 54 of conventional laser systems. Skilled persons will appreciate that FSM 30 could be positioned in the beam path 18 but mounted somewhere other than on the X stage 54.
  • FSMs 30 that employ a flexure mechanism and voice coil actuators, piezoelectric actuators that rely upon deformation of piezoelectric, electrostrictive, or PMN actuators materials, and piezoelectric or electrostrictive actuators to deform the surface of a mirror.
  • Exemplary voice coil actuated FSMs 30 are described in U.S. Pat. No. 5,946,152 of Baker and can be adapted to work at high frequencies. Suitable voice coil actuated FSMs 30 are available from Ball Aerospace Corporation of Broomfield, Colorado and Newport Corporation of Irvine, California.
  • a suitable piezoelectric actuator is a model S-330 Ultra-Fast Piezo Tip/Tilt Platform manufactured by Physik Instrumente (“PI”) GmbH & Co. of Düsseldorf, Germany.
  • the laser controller 64 commands the stages 52 and 54 and fast positioner 32 of the integrated positioning system to follow a predetermined tool path, such as a trimming profile or a blind via drilling profile, while the mirror controller 64 independently causes FSM 30 to move the laser spot position of laser system output beam 46 in a desired pattern, such as small circles or oscillations.
  • This superimposed, free running beam movement or vibration distributes the energy of laser system output beam 46 over a larger area and effectively makes a wider cut along the tool path.
  • the effective kerf width is generally equal to the size of the pattern dimension plus the spot diameter.
  • the beam movement also spreads the laser energy over a larger area to effectively increase the area that can be treated with a given average energy density within a period of time.
  • mirror controller 64 may, however, cooperate with laser controller 62 to effect particular desired patterns of movement of laser system output beam 46 during particular laser applications or particular tool paths of the integrated positioning system.
  • the FSM- effective spot pattern may be selected to have a pattern dimension to obtain a particular kerf width, such as for a trimming operation, and/or may be selected to impart a particular hole edge quality, such as during a via drilling operation.
  • FIG. 5B is computer model of an exemplary straight-line kerf-forming tool path 80 of FIG. 5A, enhanced by movement of FSM 30.
  • the parameters include: a PRF of about 18 kHz; a spot size of about 25 ⁇ m; a linear velocity (the rate the small rotating circular pattern is moving across the work surface) of about 50 mm/sec; a rotation rate (the rate the circular pattern is rotating) of about 2 kHz; a rotation aptitude (the diameter of the circular pattern (to center of beam)) of about 30 ⁇ m; an inside diameter (the starting diameter of the spiral pattern (to center of circular pattern) ) of about 10 ⁇ m; an outside diameter (the end diameter of spiral pattern (to center of circular pattern)) of about 150 ⁇ m; and a number of cycles (the number of rotations of the spiral pattern) of about 2.
  • mirror-enhanced straight-line profile 82 creates a kerf width 84 that is larger than the spot diameter 86 of output beam 46. This technique permits a kerf wider than the spot diameter 86 to be formed in fewer passes while maintaining the machining quality and other benefits of using a focused output beam 46 (i.e. without defocusing the beam to achieve a wider spot).
  • FIG. 6B is computer model of an exemplary via-forming spiral tool path 90 (FIG. 6A) enhanced by movement of FSM 30.
  • FIGS. 6A and 6B collectively FIG.
  • the parameters include: a PRF of about 15 kHz; a spot size of about 15 ⁇ m; a linear velocity (the rate the small rotating circular pattern is moving across the work surface) of about 30 mm/sec; a rotation rate (the rate the circular pattern is rotating) of about 1.5 kHz; a rotation aptitude (the diameter of the circular pattern (to center of beam)) of about 20 ⁇ m; an inside diameter (the starting diameter of the spiral pattern (to center of circular pattern) ) of about 10 ⁇ m; an outside diameter (the end diameter of spiral pattern (to center of circular pattern)) of about 150 ⁇ m; and a number of cycles (the number of rotations of the spiral pattern) of about 2.
  • the model shows that in order to support laser pulse rates in the 15 to 20 kHz range, a rotation rate of 1 kHz to 2.5 kHz (5 to 15 pulses per rotation) is desired for a practical pulse overlap.
  • the CO2 laser system 10 employs a PRF of 30-40 kHz with 20-30 pulses per via hole.
  • the FSM 30 oscillates the laser system output beam 46 at 1.0-1.5 kHz so it makes one complete revolution as the hole is drilled, and the drill time takes less than 0.6-1 ms.
  • a blind via is formed by sequentially directing laser system output beam 46 having spot area 86 at overlapping contiguous locations along a spiral tool path 90 to a periphery.
  • Beam 46 is preferably moved continuously through each location at a speed sufficient for system 10 to deliver the number of beam pulses necessary to achieve the depth of cut at the location.
  • the target material is "nibbled" away to form a hole of increasing size each time beam 46 is moved to a new cutting location. The final shape of the hole is typically achieved when beam 46 moves along a circular path at the periphery.
  • mirror-enhanced via-drilling profile 92 creates a kerf width 84 that is larger than the spot diameter 86 of output beam 46 such that the diameter 94 of the resulting via is much greater than the diameter would be for a spiral made from a kerf width the same size as the spot size.
  • the invention permits a series of laser pulse spots 48 at a given repetition rate appear as a series of larger-diameter laser pulse spots at a lower pulse rate without the beam quality problems associated with working out of focus.
  • Via diameters or kerf widths typically range from 25-300 ⁇ m, but vias or kerfs having diameters or widths as large as or greater than 1 millimeter (mm) may also be desirable.
  • An alternative tool path to form a blind via would be to start at the center and cut concentric circles of incrementally increasing radii defined by of kerf width 84.
  • the overall diameter of the via would increase as the concentric circles forming via travel in a circular path at greater distances from center of region.
  • this process may begin by defining the desired circumference and processing the edges toward the center.
  • Outward spiral processing tends to be a little more continuous and quicker than concentric circle processing; however, a blind via can also be created by spiraling inward.
  • Skilled persons will appreciate that either work piece 50 or processing output beam 46 may be fixed or moved relative to the position of the other. In a preferred embodiment, both work piece 50 and processing output beam 46 are moved simultaneously.
  • the integrated positioning system may be directed toward a single location for processing a small area via and the nonintegrated FSM 30 is used to create a via diameter that is-larger than the spot diameter 48 of output beam 46 without significant dwell time and without the complexity of moving the integrated positioning system to perform a tool path such as tool path 90.
  • the via quality including edge quality and bottom uniformity, could be greatly improved, particularly whenever the laser system output beam 46 is relatively Gaussian.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Plasma & Fusion (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Laser Beam Processing (AREA)
  • Mechanical Optical Scanning Systems (AREA)

Abstract

Selon l'invention, un miroir d'orientation rapide (30) de type miroir actionné par PMN, est positionné dans un chemin de faisceau (18) d'un système de positionnement (40) comprenant des étages, pour le déplacement continu d'un faisceau laser (46) dans un modèle déterminé à vitesse élevée autour d'une position cible nominale (60), afin que soient séparés spatialement des points laser focalisés (48) produits à une fréquence de récurrence laser élevée, ce qui permet de créer des caractéristiques géométriques présentant des dimensions supérieures à celles d'un point laser focalisé (48). Une série de points laser (48), à une fréquence de récurrence donnée, apparaissent sous forme de série de points laser présentant un diamètre supérieur, à une fréquence d'impulsions inférieure, sans les problèmes de qualité de faisceau associés à la mise en oeuvre de la focalisation.
PCT/US2003/000686 2002-01-11 2003-01-10 Procede d'usinage laser d'une piece par agrandissement de point laser WO2003059568A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
KR1020047010540A KR100982677B1 (ko) 2002-01-11 2003-01-10 레이저 스폿 확장을 이용한 소재의 레이저 가공 방법
DE10392185T DE10392185T5 (de) 2002-01-11 2003-01-10 Verfahren zur Laserbearbeitung eines Werkstücks mit Laserpunktvergrösserung
CA002469520A CA2469520A1 (fr) 2002-01-11 2003-01-10 Procede d'usinage laser d'une piece par agrandissement de point laser
GB0412827A GB2397545B (en) 2002-01-11 2003-01-10 Method for laser machining a workpiece with laser spot enlargement
AU2003214818A AU2003214818A1 (en) 2002-01-11 2003-01-10 Method for laser machining a workpiece with laser spot enlargement
JP2003559716A JP4340745B2 (ja) 2002-01-11 2003-01-10 レーザースポットを拡大するワークピースのレーザー加工方法

Applications Claiming Priority (2)

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US34861302P 2002-01-11 2002-01-11
US60/348,613 2002-01-11

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WO2003059568A1 true WO2003059568A1 (fr) 2003-07-24

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KR (1) KR100982677B1 (fr)
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AU (1) AU2003214818A1 (fr)
CA (1) CA2469520A1 (fr)
DE (1) DE10392185T5 (fr)
GB (1) GB2397545B (fr)
TW (1) TW564196B (fr)
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CN102566590A (zh) * 2011-03-14 2012-07-11 北京国科世纪激光技术有限公司 光学元件智能调整系统及方法

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CN100462181C (zh) * 2006-10-30 2009-02-18 西安交通大学 飞秒激光真三维微纳加工中心
US7663269B2 (en) * 2006-12-13 2010-02-16 A-Tech Corporation High bandwidth linear actuator for steering mirror applications
DE102007012815A1 (de) 2007-03-16 2008-09-18 Sauer Gmbh Lasertec Verfahren und Vorrichtung zur Werkstückbearbeitung
TWI523720B (zh) 2009-05-28 2016-03-01 伊雷克托科學工業股份有限公司 應用於雷射處理工件中的特徵的聲光偏轉器及相關雷射處理方法
DE102009044316B4 (de) 2009-10-22 2015-04-30 Ewag Ag Verfahren zur Herstellung einer Fläche und/oder einer Kante an einem Rohling sowie Laserbearbeitungsvorrichtung zur Durchführung des Verfahrens
US8338745B2 (en) * 2009-12-07 2012-12-25 Panasonic Corporation Apparatus and methods for drilling holes with no taper or reverse taper
KR102253017B1 (ko) * 2010-10-22 2021-05-20 일렉트로 싸이언티픽 인더스트리이즈 인코포레이티드 빔 디더링 및 스카이빙을 위한 레이저 처리 시스템 및 방법
CN102069298A (zh) * 2010-12-20 2011-05-25 珠海市铭语自动化设备有限公司 一种板材激光切割系统及其切割加工方法
CN103100797B (zh) * 2013-01-23 2015-09-09 刘茂珍 基于自适应光学的激光微细加工设备和方法
WO2014126020A1 (fr) * 2013-02-13 2014-08-21 住友化学株式会社 Dispositif d'irradiation par laser et procédé de fabrication d'un élément optique stratifié
GB2514084B (en) * 2013-02-21 2016-07-27 M-Solv Ltd Method of forming an electrode structure for capacitive touch sensor
GB2511064A (en) 2013-02-21 2014-08-27 M Solv Ltd Method of forming electrode structure for capacitive touch sensor
US20140263212A1 (en) * 2013-03-15 2014-09-18 Electro Scientific Industries, Inc. Coordination of beam angle and workpiece movement for taper control
IT201600070259A1 (it) * 2016-07-06 2018-01-06 Adige Spa Procedimento di lavorazione laser di un materiale metallico con controllo della posizione dell'asse ottico del laser rispetto ad un flusso di gas di assistenza, nonché macchina e programma per elaboratore per l'attuazione di un tale procedimento.
CN107876981B (zh) * 2017-11-20 2019-08-20 张家港初恒激光科技有限公司 一种改进型的激光焊接加工工作站
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CN112122776A (zh) * 2020-09-23 2020-12-25 苏州科韵激光科技有限公司 基于高速旋转反射镜的非线性形状加工系统及方法
KR102497645B1 (ko) * 2021-06-23 2023-02-08 인하대학교 산학협력단 금형 표면 레이저 가공하는 방법
CN113897608A (zh) * 2021-10-23 2022-01-07 河南省锅炉压力容器安全检测研究院 一种用于阀门密封面的激光表面强化加工设备

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WO2010005701A3 (fr) * 2008-06-16 2010-03-11 Electro Scientific Industries, Inc. Modification des angles d’entrée associés à des actions d’outillage circulaires pour améliorer le débit d’usinage
CN102566590A (zh) * 2011-03-14 2012-07-11 北京国科世纪激光技术有限公司 光学元件智能调整系统及方法

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DE10392185T5 (de) 2004-12-02
CN1612793A (zh) 2005-05-04
JP4340745B2 (ja) 2009-10-07
GB0412827D0 (en) 2004-07-14
TW200301718A (en) 2003-07-16
CA2469520A1 (fr) 2003-07-24
TW564196B (en) 2003-12-01
GB2397545A (en) 2004-07-28
KR100982677B1 (ko) 2010-09-17
JP2005532908A (ja) 2005-11-04
KR20040073542A (ko) 2004-08-19
GB2397545B (en) 2005-05-11
AU2003214818A1 (en) 2003-07-30

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