Laser lift off systems and methods

Laser lift off systems and methods may be used to provide monolithic laser lift off with minimal cracking by reducing the size of one or more beam spots in one or more dimensions to reduce plume pressure while maintaining sufficient energy to provide separation. By irradiating irradiation zones with various shapes and in various patterns, the laser lift off systems and methods use laser energy more efficiently, reduce cracking when separating layers, and improve productivity. Some laser lift off systems and methods described herein separate layers of material by irradiating non-contiguous irradiation zones with laser lift off zones (LOZs) that extend beyond the irradiation zones. Other laser lift off systems and methods described herein separate layers of material by shaping the irradiation zones and by controlling the overlap of the irradiation zones in a way that avoids uneven exposure of the workpiece. Consistent with at least one embodiment, a laser lift off system and method may be used to provide monolithic lift off of one or more epitaxial layers on a substrate of a semiconductor wafer.

TECHNICAL FIELD

The present invention relates to separation of layers of material and more particularly, to a laser lift off systems and methods for monolithic separation of layers of material, such as a substrate and a film grown on the substrate.

BACKGROUND INFORMATION

Laser lift off may be used to separate layers of material. One application in which laser lift off has been used advantageously is the separation of GaN layers from sapphire substrates when manufacturing light emitting diodes (LEDs). In spite of the advantages from UV-laser lift-off, GaN LED manufacturing has been limited due to poor productivity caused by low process yield. The low yield is due in part to high residual stresses in a GaN-sapphire wafer, resulting from a Metal-Organic Chemical Vapor Deposit (MOCVD) process. The MOCVD process requires an activation temperature of over 600° C. As shown inFIG. 1A, GaN and InGaN layers32are deposited on a sapphire wafer38by the MOCVD process. Since there is substantial difference in coefficients of thermal expansion (CTE) between the GaN (5.59×10-6/° K) and the sapphire (7.50×10-6/° K) (see Table 1), high levels of residual stresses exist when the GaN/sapphire wafer cools down to ambient temperature from the high temperature of the MOCVD process, as shown inFIG. 1B. The residual stresses include compressive residual stresses40on the GaN and tensional residual stresses42on the sapphire.

TABLE 1Various material properties of GaN and sapphire.BandLatticeLatticeGapThermalConst. aConst. cDensityEnergyExpansionMaterialStructure(Å)(Å)(g/cm3)(eV)×10−6/° KSapphireHexagonal4.75812.9913.979.97.50GaNHexagonal3.1895.8156.13.35.59

When an incident laser pulse with sufficient energy hits a GaN/sapphire interface, the irradiation results in instantaneous debonding of the interface. Since the incident laser pulse has limited size (usually far less than 1 cm2), it creates only a small portion of the debonded or lifted-off interface. Since surroundings of the debonded area still have a high level of residual stress, it creates a concentration of stress at the bonded/debonded border, resulting in fractures at the border. This fracturing, associated with the residual stress, has been one of the obstacles of the UV-laser lift-off process.

Both processes employ raster scanning, as shown inFIG. 3, which involves either translation of the laser beam44or the target of the GaN/sapphire wafer46. A problem associated with the raster scanning method is that it requires overlapping exposures to cover the desired area, resulting in multiple exposures48for certain locations. In both of the above methods, the laser lift-off of GaN/sapphire is a single pulse process. The unnecessary multiple exposures in localized areas increase the potential for fracturing by inducing excessive stresses on the film.

As shown inFIG. 4, raster scanning also involves a scanning of the laser beam44from one end to the other, gradually separating the GaN/sapphire interface from one side to the other. This side-to-side relaxation of residual stresses causes large differences in the stress level at the interface50between the separated and un-separated regions, i.e., the interface between the scanned and the un-scanned area. The disparity in residual stress levels at the interface50increases the probability of propagation of Mode I and Mode II cracks. Although the illustrations inFIGS. 3 and 4are based on a process using a solid state laser, raster scanning of an excimer laser will produce similar results.

Currently, a common size of sapphire wafers is two-inch diameter, but other sizes (e.g., three-inch and four-inch wafers) are also available for the hetero-epitaxial growth of GaN. For a GaN/sapphire wafer, the level of residual stresses varies in the wafer, and compressive and tensile residual stresses may exist together. The existence of the residual stresses may be observed by wafer warping or bowing. When a laser lift-off process relaxes a large area of a continuous GaN/sapphire interface, as described above, a severe strain gradient may be developed at the border between the debonded and the bonded interface. This strain gradient may cause extensive fracturing of the GaN layer.

When a target material is irradiated with an intense laser pulse, a shallow layer of the target material may be instantaneously vaporized into the high temperature and high pressure surface plasma. This phenomenon is called ablation. The plasma created by the ablation subsequently expands to surroundings. The expansion of the surface plasma may induce shock waves, which transfer impulses to the target material. The ablation may be confined in between two materials when the laser is directed through a transparent material placed over the target. During this confined ablation, the plasma trapped at the interface may create a larger magnitude of shock waves, enhancing impact pressures. The explosive shock waves from the confined ablation at the GaN/sapphire interface can cause not only separation of the GaN layer from the sapphire substrate but may also fracture the GaN layer near the laser beam spot (see, e.g., P. Peyre et. al., Journal of Laser Applications, vol. 8 pp. 135-141, 1996).

Another technique for laser lift off involves the use of near-field imaging techniques to image a beam spot at the interface between the layers being separated.FIG. 5illustrates one example of a projection of a homogeneous beam by near-field imaging and shows a representative beam profile along the beam path. The raw beam from an excimer laser120has Gaussian distribution in short side and flat topped distribution in the long side. The beam homogenizer122(e.g., of multi-array configuration) makes the gradient raw beam profile into a square flat-topped profile. The homogenized beam is cropped by the mask124(e.g., the rectangular variable aperture) to utilize the best portion of the beam, which is projected to the LED target wafer116by near-field imaging, for example, using beam imaging lens126. The edge resolution of the homogeneous beam spot130at the LED wafer116therefore becomes sharp.

FIGS. 6-8Cillustrate one way in which the imaged beam (e.g., the beam spot130) can cause separation of layers of material of the LED wafer116. Referring toFIG. 6, the laser may be directed through at least one layer of substrate material102(e.g., sapphire) to at least one target material104(e.g., GaN) to separate the materials102,104. The separation of the materials102,104may be achieved by using a laser energy density sufficient to induce a shock wave at the interface106of the target material104and the substrate material102, thereby instantaneously debonding the target material104from the substrate material102. The shock wave may be created by the explosive expansion of plasma108at the interface as a result of the increased density of the ionized vapor sharply elevating the plasma temperature. The laser energy density may be in a range sufficient to induce a force Faon the target material104that causes separation without fracturing. The applied force Famay be represented as follows:
Pp(GPa)=C[Ir(GW/cm2)]1/2
Fa(N)=Pp(GPa)Ar(cm2)
where Ppis the peak pressure induced by explosive shock waves, C is an efficiency and geometrical factor, Iris the irradiance of the incident laser beam, Fais the applied force and Aris the area under irradiation.

When the plasma108is expanding, as shown inFIG. 7, the irradiation zone is acting as a bending arm pivoting at the edge of the irradiation zone. For example, the force (Fr) required for rupturing or fracturing may be viewed as a two-point bend test and may be represented as follows:

Fr∝wd2L⁢σr
where d is the thickness of the target material104, w is the width of the applied force or width of the laser pulse, L is the length of applied arm or half length of the laser pulse, and σris the modulus of rupture or fracture stress of GaN. To increase the force (Fr), the width w of the laser pulse may be increased and the half length L of the laser pulse may be decreased, thereby forming a line shaped beam. The line shaped beam may be scanned across the target material104to minimize the bending moment upon irradiation.

At a laser energy density under the ablation threshold of GaN (˜0.3 J/cm2at 248 nm), for example, the instantaneous separation of the GaN/sapphire interface106may not be successfully achieved, as shown inFIG. 8A. Although decomposition of the GaN can occur under the ablation threshold, this alone cannot achieve instantaneous separation of the interface106, because there is no driving force, i.e. shock waves from the expanding plasma, without the ablation. Conversely, applying overly-intense laser energy density may create excessive explosive stress wave propagation, which results in cracks and fractures on the target material104(e.g., the GaN film), as shown inFIG. 8C. When the irradiating laser energy density is optimized, as shown inFIG. 8B, the force created by the shock wave is sufficient to separate the layers102,104at the interface106but not enough to induce fracture in the target material104. According to this example with GaN and sapphire, the laser energy density may be between about 0.60 J/cm2to 1.5 J/cm2to achieve the separation shown inFIG. 8B.

The near-field imaging techniques described above have been used successfully in a process known as patterned laser lift off to overcome many of the problems associated with residual stress and other problems discussed above. The patterned laser lift off technique forms streets in one or more layers to be separated, forms a beam spot to cover one or more of the sections defined by the streets, and separates layers in the sections. One example of a patterned lift off method is described in greater detail in U.S. Pat. No. 7,202,141, which is fully incorporated herein by reference. Although successful, the patterned lift off technique requires the additional steps of forming the streets, which results in a more time-consuming process. Attempts at using the techniques described above to provide monolithic laser lift off, however, have been less successful because of the problems associated with residual stress.

DETAILED DESCRIPTION

Laser lift off systems and methods, consistent with the embodiments described herein, may be used to provide monolithic laser lift off with minimal cracking by reducing the size of one or more beam spots in one or more dimensions to reduce plume pressure while maintaining sufficient energy to provide separation. By irradiating irradiation zones with various shapes and in various patterns, the laser lift off systems and methods use laser energy more efficiently, reduce cracking when separating layers, and improve productivity. Some laser lift off systems and methods described herein separate layers of material by irradiating non-contiguous irradiation zones with laser lift off zones (LOZs) that extend beyond the irradiation zones. Other laser lift off systems and methods described herein separate layers of material by shaping the irradiation zones and/or by controlling the overlap of the irradiation zones in a way that avoids uneven exposure of the workpiece. Consistent with at least one embodiment, a laser lift off system and method may be used to provide monolithic lift off of one or more epitaxial layers on a substrate of a semiconductor wafer.

According to some exemplary embodiments, the laser lift off systems and methods described herein are used to lift off or separate a GaN epi layer from a sapphire substrate of a semiconductor wafer; although other types of substrates and layers of material may be used which are known to those skilled in the art. Also, a sacrificial layer can be provided between the GaN (or other layer of material) and the sapphire (or other type of substrate). Any of the lift off systems and methods described herein can be applied to any highly absorbing material on a transparent carrier including, without limitation, a polymer material such as polyamide on transparent glass.

Referring toFIGS. 9A and 9B, a laser beam1000is used to separate one or more layers1002,1004of material of a workpiece1001. The laser beam1000passes through at least one layer1002to irradiate an interface1006with at least one other layer1004to be separated or lifted off. As used herein, “irradiate” refers to exposing an area with a single pulse of laser radiation. A beam spot formed by the laser beam1000at the interface1006irradiates an exposed laser irradiation zone1010and causes separation of the layers1002,1004in a lift off zone (LOZ)1012, which may extend beyond the irradiation zone1010. The refractive index of the layer1002(e.g., the sapphire) through which the laser beam1000passes may also cause the laser light to bend inside (not shown) to create smaller irradiated beam spot on the layer1004as compared to the beam1000or beam spot as seen on a surface of the layer1002. This smaller beam spot size on the layer1004may be taken into consideration when determining the spot size, spot spacing, and process parameters using the lift off methods described below to avoid cracking while allowing monolithic lift off.

The energy of a laser pulse causes ablation of the material in one of the layers1002,1004primarily in the irradiation zone1010where the pulse energy is absorbed. This ablation results in an instantaneous debonding and separation of the layers1002,1004. Because thermal energy may be conducted beyond the irradiation zone1010, ablation and/or decomposition may occur beyond the irradiation zone1010and may result in separation of the layers1002,1004beyond the irradiation zone1010(i.e., creating the LOZ1012). The ablation of material at the interface1006also generates a plasma plume that expands and creates a pressure (referred to as plume pressure) between the layers1002,1004, which may also extend the lift off zone1012.

As mentioned above, when the plume pressure is too high, the resulting force may cause cracking in one or more of the layers1002,1004being separated. Consistent with the lift off systems and methods described herein, laser irradiation parameters such as laser wavelength, pulse width, energy density, beam spot size, beam spot shape, and beam spot array patterns may be configured to provide adequate separation of the layers1002,1004while minimizing plume pressure to minimize cracking. Consistent with at least some embodiments, the laser irradiation parameters may be configured to provide monolithic lift off of a GaN layer on a substrate of a semiconductor wafer with minimal or no cracking.

The plume pressure is a function of the volume of material that is ablated per pulse at the interface1006(also referred to as the interaction volume), which relates to the area of the irradiation zone1010and the ablation depth. Higher ablation rates, for example, may remove a larger volume of material and create higher plume pressures. One way to reduce the interaction volume is by reducing the size of the laser beam1000and thus the size of the beam spot. When reducing the spot size reduces the pulse energy applied to the irradiation zone1010, the ablation depth may be reduced in addition to the area. As shown inFIG. 9B, for example, the laser beam1000is smaller than the laser beam10and forms a beam spot (and irradiation zone) having a smaller area and lower pulse energy. As a result of the smaller area of the irradiation zone and the lower pulse energy reducing the ablation depth, the volume of material1011ablated by a pulse of the smaller beam1000is smaller than a volume of material11ablated by a pulse of the larger beam10.

Thus, the beam may be adjusted to reduce the beam spot size to match an allowable stress level for the materials1002,1004being separated. Various sizes of beam spots may be used depending upon, for example, the type of material, the thickness of the layers, and the area to be separated. Examples of smaller beam spots that have been found capable of monolithic lift off of epi layers from sapphire substrates include 100 by 100 micron square beams and 200 by 200 micron square beams. As described in greater detail below, the number of beam spots with reduced size on target may be extended to achieve a higher throughput and various spacings may be used between irradiations (e.g., positive, negative or zero overlapping) to allow separation while minimize cracking. The spacings or overlapping may also be different in different axes or scan direction, for example, depending upon beam divergence in the axes and/or the internal stresses along the axes. A beam passing through a homogenizer, for example, may have an asymmetrical point spread function such that the beam profile is sharper along its Y axis than along its X axis. Such a beam may have positive overlap along the X axis and zero or negative overlap along the Y axis.

Another way to change the interaction volume is by using different wavelengths and/or pulse durations or widths. Depending upon the material characteristics, the ablation depth may be related to optical penetration depth and/or thermal penetration depth. Changing the wavelength may impact optical penetration depth and changing the pulse width may impact both optical penetration depth and thermal penetration depth. Shorter wavelengths having a higher photonic energy, for example, may provide better absorption and shallower optical penetration depth for certain materials such as GaN. Shorter pulse widths reduce diffusion effects because the pulse may be delivered in a shorter time than the time it takes to conduct heat into the material and thus reduce thermal penetration depth. Shorter pulse widths may also increase non linear effects resulting in higher absorption and reduced optical penetration in certain cases. Depending upon the materials, for example, a nanosecond excimer laser at 248 nm or 193 nm or an ultrashort laser (with pulse durations less than 1 ns) may be used to provide a desired ablation depth.

A further way to change the interaction volume is by adjusting the energy density of the beam spot that irradiates the irradiation zone1010. Ablation occurs when the energy density is above an ablation threshold for a particular material and wavelength. As the energy density increases, the absorption depth increases resulting in a larger interaction volume. In general, energy density is energy over area and may be controlled by changing either the energy or the area of the beam. For example, energy density may be controlled by controlling the power to the laser, by using attenuators, or by shaping (e.g., expanding or contracting) the beam using beam shaping optics, as will be described in greater detail below. Thus, the energy density of the beam spot on the workpiece may be varied to optimize the fluence and coupling efficiency for a particular material, to provide a desired ablation depth, and/or to control the amount of heat in the layer being lifted off.

The laser irradiation parameters, such as the wavelength, pulse width, and energy density, depend on the types of materials being separated. For example, a laser wavelength of 248 nm is suitable for separating GaN from sapphire because the photonic energy of 248 nm (5 eV) is between the bandgaps of GaN (3.4 eV) and sapphire (9.9 eV). Thus, the 248 nm radiation is better absorbed in GaN than in sapphire and the selective absorption allows the laser radiation to pass through the sapphire to ablate the GaN resulting in separation. At a wavelength of 248 nm, the ablation threshold of GaN is about 0.3 J/cm2.

Those skilled in the art will recognize that other laser wavelengths may be used to separate other types of materials. For example, a buffer layer may be used between the sapphire substrate and the GaN layer(s) to facilitate epitaxial growth of the GaN. Examples of the buffer layer include a GaN buffer layer and an Aluminum Nitride (AlN) buffer layer. Where an AlN buffer layer is used, a laser at 193 nm may be used because the photonic energy of the 193 nm laser light (6.4 eV) is in between bandgaps of sapphire (9.9 eV) and AlN (6.1 eV).

Referring toFIGS. 10A-10E, one or more reduced size beam spots may be used to irradiate multiple irradiation zones1010a-dwith various spacings between the irradiation zones to allow monolithic separation of the layers of the workpiece while minimizing cracking.FIGS. 10A-Dshow irradiation zones1010a-dformed by sequential irradiations using a single beam spot with varying degrees of overlap as the beam spot moves stepwise across the workpiece. Four irradiation zones1010a-dare shown for purposes of illustration, but multiple irradiation zones may be sequentially formed across an entire workpiece to separate the layers of the workpiece. To move the beam spot stepwise across the workpiece, the beam may be moved relative to the workpiece or the workpiece may be moved relative to the beam, as will be described in greater detail below. The beam spot may also be moved in different directions or patterns other than a stepwise direction across a workpiece, as will be described in greater detail below.

As shown inFIG. 10A, for example, the irradiation zones1010a-dmay have zero overlap (i.e., each step is substantially the same as the width of the beam spot). In other words, each location along the interface between the layers is exposed to a single shot or pulse of laser radiation. In one example where an epitaxial layer is separated from a sapphire substrate, a single beam spot with a spot size of about 227 microns by 213 microns at 1 J/cm2may be used with zero overlapping and when applied with a pulse frequency of about 400 Hz may be capable of lifting off a 2 inch wafer in about 3 minutes.

As shown inFIGS. 10B and 10C, the irradiation zones1010a-dmay have positive overlap such that each location along the interface between the layers is exposed to multiple shots or pulses of laser irradiation. In one embodiment, the positive overlap is controlled such that each location is exposed to the same number of pulses to avoid uneven exposures across the workpiece. As shown inFIG. 10B, a square shaped beam spot may be overlapped by using a step size about ½ the width of the beam spot such that each location is exposed to four (4) shots or pulses of laser irradiation. Beams spots with other shapes may also be used to control the overlap. As shown inFIG. 10C, for example, a hexagonal shaped beam spot may be overlapped by using a step size about ½ the width of the beam spot such that each location is exposed to three (3) shots or pulses of laser irradiation. The energy density may be set (e.g., at about the ablation threshold) such that the multiple pulses will result in separation without causing cracking.

In other embodiments, the irradiation zones may have a gradually decreasing energy density at the edges and may overlap only at the edges such that the combined energy density of the overlapping portions is optimized for separation without cracking. In these embodiments, a gradient mask may be used to form the beam spots with the decreasing energy density at the edges.

In other embodiments, a narrow line shaped beam may be scanned across a portion of a workpiece or across an entire workpiece with zero or relatively small positive overlapping. Such a narrow line beam may perform lift off without being homogeneous across the width of the narrow line beam. In one example, a narrow line beam may have a length of about 52 mm and a width of about 20 microns and may be applied with an energy density of about 1 J/cm2. Using such a narrow line beam generated by an excimer laser with a pulse frequency of 400 Hz may allow speeds of 8 mm/sec and separation of an epi layer from a wafer in about 10 sec. A line beam with a more narrow width may also be used.

As shown inFIG. 10D, the irradiation zones1010a-dmay be non-contiguous or spaced with a negative overlap (i.e., the step size is greater than the width of the beam spot). As used herein, “non-contiguous” refers to zones that do not overlap or touch. In this embodiment, the beam spot may have a size and/or shape such that the lift off zone extends beyond the irradiation zone. Thus, the adjacent non-contiguous irradiation zones1010a-dmay be separated by a spacing that is as wide as possible while still resulting in separation of the layers. The pitch or separation may depend upon the type of material being separated, the size of the lift off zone relative to the irradiation zone, and other laser processing parameters. In one example where an epitaxial layer is separated from a sapphire substrate, a single reduced size beam spot (e.g., about 200 by 200 microns) may be smaller than the step size or pitch by about 3 microns.

AlthoughFIGS. 10A-10Dshow a single beam spot performing sequential irradiations across a workpiece, an array or pattern of multiple reduced size beam spots may also be formed to perform simultaneous irradiations. The reduced size beam spots within an array or pattern may have varying degrees of spacing or pitch. The array or pattern of beam spots may also be used to provide sequential irradiations with varying degrees of overlap similar to a single beam spot (i.e., zero overlap, positive overlap, or negative overlap). AlthoughFIGS. 10A-10Dshow sequential irradiations of either zero overlap, positive overlap, or negative overlap, various combinations of these overlaps may be used in different axes or scan directions.

As shown inFIGS. 10E and 10F, for example, multiple beams or beamlets1000a-dmay form an array of reduced size beam spots that irradiate multiple non-contiguous irradiation zones1010a-dsimultaneously. In one embodiment, the array of beam spots may have a shape and size such that the lift off zones1012a-dextend beyond the respective irradiation zones1010a-dand the layers1002,1004may be separated without overlapping the irradiation zones1010a-d, thereby avoiding cracking due to multiple exposures. Where an array of non-contiguous irradiation zones1010a-dhave larger lift off zones1012a-d, for example, the aggregate lift off zone may be equivalent to one larger laser beam spot10.

As discussed above, the plume pressure is reduced by using the smaller beam size and/or by otherwise reducing the interaction volume. A plurality of non-contiguous irradiation zones1010a-dmay be irradiated with a plume pressure that is less than the plume pressure of the equivalent larger beam spot10because the lift off zones1012a-dallow less energy to be spread over the same area with a smaller interaction volume. Forming arrays of non-contiguous irradiation zones1010a-dmay thus allow a larger aggregate lift off zone with less energy. The size and spacing of the beam spots may depend on the amount of energy density that is desired to provide separation with minimal pressure and stress.

Using a pattern of beam spots that simultaneously irradiate a corresponding pattern of non-contiguous irradiation zones1010a-dincreases the aggregate lift off zone of each irradiation and increases the lift off speed in addition to lowering the plume pressure and stress on the layers. AlthoughFIGS. 10E and 10Fshown non-contiguous irradiation zones with larger lift off zones, an array or pattern of beam spots may also irradiate non-contiguous irradiation zones with lift off zones substantially the same as the irradiation zones. Various shapes and patterns for beam spots and irradiation zones are described in greater detail below.

The laser beams1000a-dand/or the workpiece1001may be moved such that the array of beam spots may perform irradiations in different locations around the workpiece1001to separate the layers1002,1004. The array or pattern of beam spots may be scanned or moved, for example, in a stepwise direction with varying degrees of overlapping irradiations similar to the single beam spot described above. Various scanning strategies may be used across the workpiece1001to minimize the stresses that occur as a result of the separation processes (e.g., leaving some rows or areas unprocessed and then filling in those unprocessed areas). Various patterns and scanning techniques are shown and described in greater detail below.

Embodiments of laser lift off systems are shown inFIGS. 11-13. In general, the laser lift off systems include a laser for generating a raw laser beam and a beam delivery system for modifying the beam and delivering the modified beam (or beamlets) to the workpiece1001. As shown inFIG. 11, a laser lift off system1101may include a laser1120for generating a raw laser beam1121, a beam shaper1122for producing a shaped laser beam1123, and a diffractive optical element1124for forming multiple shaped beamlets1100a-d. The beam delivery system of the laser lift off system1101may also include one or more reflective elements1126for reflecting the laser beams.

The laser1120may include, without limitation, an excimer laser, a diode pumped solid state (DPSS) laser, a fiber laser, or an ultrafast laser at the desired wavelength. An ultrafast laser is generally a laser capable of emitting ultrashort pulses having pulse durations less than 1 nanosecond, i.e., pulses with durations of femtoseconds or picoseconds. An ultrafast laser may be capable of producing the laser beam1000at different wavelengths (e.g., about 0.35 μm, 0.5 μm or 1 μm or any increments therebetween) and at different ultrashort pulse widths (e.g., less than about 10 ps). Using an ultrafast laser capable of changing the wavelength and/or pulse width allows control over the ablation depth and interaction volume as described above. One example of an ultrafast laser is a Trumicro series 5000 picosecond laser available from TRUMPF.

The beam shaper1122may include, for example, a mask with an aperture that produces the desired beam shape of the shaped laser beam1123when the raw laser beam1121passes through the aperture. The beam shaper1122may also include beam shaping optics (e.g., lenses) that change the shape and/or size of the raw beam1121before a mask or the shaped beam1123after a mask. In one embodiment, the beam shaper1122includes beam shaping optics capable of controlling the energy density of the beam spot, for example, as described in greater detail in U.S. Pat. No. 7,388,172, which is fully incorporated herein by reference. The beam shaper1122may thus be used to vary the energy density of the beam spot on the workpiece (e.g., to reduce the absorption depth and the interaction volume) without having to adjust the laser power. The beam shaper1122may further include beam shaping optics that produce the desired beam shape of the shaped laser beam1123without using a mask. Using a beam shaper1122(e.g., a mask and/or beam shaping optics) to control the shape and size of the beam spots and the energy density of the beam on the workpiece allows further control over the depth of spreading of the energy and the geometrical spreading of the energy.

The diffractive optical element1124may include a holographic optical element (HOE) that uses the principles of diffraction to subdivide the shaped laser beam1123into the beamlets1100a-d. The beamlets1100a-dform an array of beam spots that simultaneously irradiate a pattern of non-contiguous irradiation zones1010. The HOE uses substantially all of the energy of the shaped beam1123to form the beamlets1100a-d. When the lift off zones exceed the irradiation zones of the beam spots, the energy of the shaped beam1123may be spread over a larger area more efficiently when using the HOE to form a pattern of smaller beamlets, as compared to using a mask to image a single large beam spot. Using the HOE to form an array of smaller beam spots may also avoid the need to homogenize the laser beam with a homogenizer. In one example, the HOE may generate a spot array from a laser beam with an aggregate lift off zone that is greater than 4 times the lift off zone of a single beam spot formed by the same laser beam. One embodiment of a holographic optical element also allows control over the beam spot size and the spacing (or pitch) of the array or pattern of beam spots formed by the HOE.

As shown inFIGS. 12A and 12B, a mask1128with an array of apertures may also be used to form an array or pattern of beam spots. One or more laser beams may illuminate the mask1128to form the beamlets1100a-dthat pass through the apertures of the mask1128. The shape, size and spacing of the apertures on the mask1128determines the shape, size and spacing of the beam spots produced by the beamlets1100a-don the target. In one embodiment shown inFIG. 12A, a single homogenized beam1123may be used to illuminate the mask1128. In another embodiment shown inFIG. 12B, multiple beamlets1123a-dmay be used to illuminate the mask1128such that the beamlets1123a-dprovide optimum illumination to match the apertures of the mask1128, thereby reducing the amount of beam energy that is rejected by the mask1128and increasing the beam utilization factor. Other types of spot array generators may also be used to form an array of beam spots.

The laser lift off system1101may also include a motion stage1130that supports the workpiece1001and positions the workpiece1001for the sequential irradiations. The motion stage1130may be an X-Y and/or theta positioning stage capable of moving the workpiece1001in an X-Y direction and/or rotating the workpiece1001. A motion control system (not shown) may be coupled to the laser1120and motion stage1130to control the laser irradiations and the positioning of the workpiece1001, for example, using a “fire on the fly” technique.

The laser lift off system1101may also control the manner in which the layers are allowed to detach to minimize cracking. When the substrate1002detaches as the lift off progresses across the workpiece1001, stress is caused because part of the workpiece1001is being lifted off while part of the workpiece1001is not, which enhances cracking at the lift off front. The laser lift off system1101may thus include one or more workpiece holders1136(e.g., clamps) for mechanically holding the substrate1002down as the lift off process takes place. The edges of the workpiece1001may be exposed first, for example, and then the workpiece holders1136may hold the edges down while processing the inside region of the workpiece1001. The workpiece holders1136may then slowly release the substrate1002. Alternatively, another transparent material, such as a thin piece of sapphire, may be used over the workpiece1001, which allows the laser to pass through to perform the lift off and mechanically prevents bowing as a result of the lift off. By forcing the substrate, the global stresses and related cracking caused by the lift off process may be minimized, thereby improving the yield when manufacturing LEDs.

According to another embodiment, shown inFIG. 13, a laser machining system1301may include a galvanometer1326for scanning one or more beam spots on the workpiece1001to provide a pattern of non-contiguous irradiation zones1010. The galvanometer1326may be used instead of or in addition to moving the workpiece1001with a motion stage. The galvanometer1326may be a 1-D or 2-D galvanometer known to those skilled in the art for scanning a laser beam. Using the galvanometer1326to scan the beam spot(s) increases the speed at which the beam spot(s) may be moved across the workpiece1001and thus increases the lift off speeds. In this embodiment of the laser lift off system1301, a beam shaper1322(e.g., a mask and/or beam shaping optics) may be used before the galvanometer1326to provide the desired shape of the beam spot(s) to be scanned across the workpiece1001and/or to control the energy density of the beam spot(s).FIG. 13Ashows another embodiment in which a galvanometer1326scans a line shaped beam.

FIGS. 14A-14Mshow various possible shapes for the beam spots and irradiation zones1010. Depending upon the size and energy density of the beam spots and the materials being separated, each of the irradiation zones1010may have corresponding lift off zones (LOZs)1012shown in broken lines. The size and energy density of the beam spots may also be adjusted such that the LOZ1012is essentially the same as the irradiation zone1010. The possible shapes include, but are not limited to, a square (FIG. 14A), circle (FIG. 14B), rectangular line (FIG. 14C), triangle (FIG. 14D), cross (FIG. 14E), L shape (FIG. 14F), hollow square (FIG. 14G), hollow circle (FIG. 14H), hexagon (FIG. 14I), elliptical line (FIG. 14J), and arc (FIG. 14K). For applications where a maximized lift off zone is desired, any shape may be used that provides a lift off zone that is maximized or relatively large compared to the irradiation zone. The beam spots may be formed with the various shapes using a mask and/or beam shaping optics.

Beam spots may also be formed with combinations of complimentary shapes, such as an L shape together with a square (FIG. 14L) and two L shapes (FIG. 14M). Various combinations of shapes may be formed together, for example, to maximize the aggregate lift off zone formed relative to the corresponding irradiation zones.

Multiple non-contiguous beam spots may be irradiated simultaneously on a workpiece such that the corresponding irradiation zones form an irradiation pattern. The irradiation pattern may be scanned or positioned at various locations across a workpiece by sequentially irradiating the irradiation zones in the irradiation pattern, thereby forming a lift off pattern including multiple sequential irradiation patterns that achieve lift off across the workpiece. Each sequential irradiation may involve a single pulse of laser energy with the irradiation pattern at a different location on the workpiece. The sequential irradiations may have varying degrees of overlap (e.g., zero overlap, positive overlap or negative overlap), which may be different in different axes or scan directions.

FIGS. 15A-15Gshow various irradiation patterns that may be formed by an array or pattern of non-contiguous beam spots and the various lift off patterns that may be formed by scanning or positioning the irradiation patterns across a workpiece with varying degrees of negative overlap of the irradiation zones. In the irradiation patterns shown inFIGS. 15A-15G, the concept of a lift off zone extending beyond the irradiation zone allows the irradiation patterns to be scanned with negative overlap of the irradiation zones. Although the irradiation patterns are shown with corresponding lift off zones (in broken lines) extending beyond the irradiation zones, the lift off zones may have a different size than shown.

FIG. 15Ashows an irradiation pattern1500aformed by a column of square-shaped non-contiguous beam spots that are spaced such that respective LOZs are touching or overlapping. The aggregate lift off zone formed by the irradiation pattern1500athus forms a line. The irradiation pattern1500amay be scanned across a workpiece with sequential irradiations to form different lift off patterns. The irradiation pattern1500amay be scanned to provide a lift off pattern1502awith the lift off zones of the sequential irradiations touching or having minimal overlap. The irradiation pattern1500amay also be scanned to provide a lift off pattern1504awith the lift off zones of the sequential irradiations overlapping. The irradiation pattern1500amay also be scanned to provide a lift off pattern1506awith the irradiation zones of the sequential irradiations being contiguous.

FIG. 15Bshows an irradiation pattern1500bformed by a column of rectangular-shaped non-contiguous beam spots, which may be scanned across the workpiece similar to the irradiation pattern1500a. This irradiation pattern1500bmay be equivalent to a narrow line beam scanned across a workpiece.

FIG. 15Cshows an irradiation pattern1500cformed by a multiple columns of square-shaped non-contiguous beam spots that are spaced such that respective lift off zones are touching or overlapping. The irradiation pattern1500cmay also be scanned to provide lift off patterns1502c,1504c,1506cwith varying degrees of overlap of the lift off zones of sequential irradiations. Although two columns are shown, the irradiation pattern1500cmay also include more than two columns of square-shaped non-contiguous beam spots.

FIG. 15Dshows an irradiation pattern1500dformed by a multiple staggered columns of square-shaped non-contiguous beam spots that are spaced such that respective lift off zones are touching or overlapping. The irradiation pattern1500dmay also be scanned to provide lift off patterns1502d,1504d,1506dwith varying degrees of overlap of the lift off zones of sequential irradiations.

FIG. 15Eshows an irradiation pattern1500eformed by square-shaped non-contiguous beam spots arranged in a triangular pattern and spaced such that respective lift off zones are touching or overlapping. The irradiation pattern1500emay also be scanned to provide lift off patterns with varying degrees of overlap of the lift off zones of sequential irradiations, such as the lift off pattern1502e.

FIG. 15Fshows an irradiation pattern1500fformed by a square-shaped non-contiguous beam spots arranged in a diamond pattern and spaced such that respective LOZs are touching or overlapping. The irradiation pattern1500fmay also be scanned to provide lift off patterns with varying degrees of overlap of the lift off zones of sequential irradiations, such as the lift off pattern1502f. The triangular shaped irradiation pattern1500eand the diamond shaped irradiation pattern1500fmay reduce point stresses when they are scanned to separate the layers.

Instead of linearly scanning the irradiation patterns stepwise in one direction across the workpiece, the irradiation patterns may also be positioned in different locations across the workpiece.FIG. 15Gshows an irradiation pattern1500gformed by square-shaped non-contiguous beam spots arranged in an open square pattern. In this irradiation pattern1500g, the beam spots are spaced such that the lift off zones around the irradiation zones are non-contiguous. This irradiation pattern is formed at different locations to interdigitate the sequential irradiations. As shown, the beam spots in this irradiation pattern1500gare spaced such that multiple passes (i.e., sequential irradiations) are required to fill in an array of irradiation zones. For example, a second pass of the irradiation pattern1500gforms the pattern1502g, a third pass of the irradiation pattern1500gforms the pattern1504g, and a fourth pass of the irradiation pattern1500gforms the complete lift off pattern1506gthat results in separation of the layers. Using this type of interdigitated scanning technique with the irradiation pattern1500gproviding on/off areas of irradiation, the separation of the layers may be performed more gradually across an area of the workpiece, thereby minimizing the stresses caused by releasing the layer from the substrate. In one example, the irradiation pattern1500gmay include an array of 100 micron square beam spots with a center to center spacing of 500 microns.

FIGS. 16A and 16Bshow irradiation patterns that are formed by an array of beam spots that are spaced such that the irradiation patterns may be scanned or overlayed with zero overlap between the irradiation zones. In these irradiation patterns, the lift off zone may not extend beyond the irradiation zones.FIG. 16Ashows an irradiation pattern1600aformed by two square-shaped non-contiguous beam spots that are spaced by about the width of the beam spots (e.g., 200 by 200 microns spaced by 200 microns). The irradiation pattern1600amay be scanned stepwise with each step being substantially the same as the width of the square beam spot such that the irradiation zones are contiguous in the stepwise direction. A single pass1601aof the irradiation pattern1600aforms two rows of sequential irradiation zones that are spaced by a row that is not irradiated or processed. The irradiation pattern1600amay be scanned with another pass to irradiate or “fill in” the unprocessed row and form a complete lift off pattern1602aof irradiation zones that causes separation of the layers. Although the irradiation pattern1600ashown inFIG. 16Ais formed by two square-shaped beam spots with a spacing equivalent to one beam spot, similar irradiation patterns may be formed by more than two beam spots with a spacing of one beam spot or a spacing of some multiple of the beam spot.

FIG. 16Bshows an irradiation pattern1600bformed by square-shaped non-contiguous beam spots arranged in a staggered or “zig-zag” pattern with a spacing equivalent to about the width of the beam spots. The irradiation pattern1600bmay be scanned stepwise with each step being substantially the same as the width of the square beam spot such that the irradiation zones are contiguous in the stepwise direction, thereby forming a lift off pattern1602bof irradiation zones that causes separation of the layers. Although the irradiation pattern1600bshown inFIG. 16Bis formed by four square-shaped beam spots with a spacing equivalent to one beam spot, similar irradiation patterns may be formed by more than four beam spots with a spacing of one beam spot or a spacing of some multiple of the beam spot.FIG. 16B-1shows photomicrographs of a wafer irradiated with the “zig-zag” irradiation pattern1600b.

FIG. 16Cshows an irradiation pattern1600cformed by square-shaped non-contiguous beam spots arranged in a triangular pattern. The irradiation pattern1600cmay be scanned stepwise with each step being substantially the same as the width of the square beam spot such that the irradiation zones are contiguous in the stepwise direction, thereby forming a lift off pattern1602cof irradiation zones that causes separation of the layers.

FIG. 16Dshows an irradiation pattern1600dformed by a square-shaped non-contiguous beam spots arranged in a square matrix pattern. Similar to the irradiation pattern1500g, this irradiation pattern is formed at different locations to interdigitate the sequential irradiations. As shown, the beam spots in this irradiation pattern1600dare spaced such that multiple passes (i.e., sequential irradiations) are required to fill in an array of irradiation zones. For example, a second pass of the irradiation pattern1600dforms the pattern1602d, a third pass of the irradiation pattern1600dforms the pattern1604d, and a fourth pass of the irradiation pattern1600dforms the complete lift off pattern1606dthat results in separation of the layers. Other numbers and spacings of the beam spots may also be used to form a matrix pattern.

FIG. 16Eshows an irradiation pattern1600eformed by a hexagonal-shaped non-contiguous beam spots arranged in a square matrix pattern. This irradiation pattern is formed at different locations to interdigitate the sequential irradiations such that each of the hexagonal-shaped beam spots overlap similar to the hexagonal beam spot shown inFIG. 10C. As shown, the beam spots in this irradiation pattern1600eare spaced such that multiple passes (i.e., sequential irradiations) are required to fill in an array of irradiation zones with the desired overlap. For example, a second pass of the irradiation pattern1600eforms the pattern1602e, a third pass of the irradiation pattern1600eforms the pattern1604e, and nine passes of the irradiation pattern1600eforms the complete lift off pattern1606ewith three overlapping exposures in each location, resulting in separation of the layers. Other numbers and spacings of the hexagonal beam spots may also be used to form a matrix pattern. An irradiation pattern may also be formed with hexagonal-shaped beam spots being spaced such that lift off zones overlap without overlapping the irradiation zones.

The irradiation patterns may also be scanned or positioned such that the irradiation zones in sequential irradiations overlap in selected areas of the lift off patterns, which may affect the amount of ablation that occurs in those areas. The irradiation pattern and the scanning may be configured to control the overlap and thus control the amount of ablation in the overlap areas, thereby providing various texturing or roughening effects on at least one of the layers (e.g., the GaN film being lifted off).FIGS. 17A-17Cshow irradiation patterns formed by non-contiguous beam spots, which may be scanned to form lift off patterns with some overlap of the edges of the irradiation zones in sequential irradiations to provide texturing or roughening.FIG. 17Ashows an irradiation pattern1700athat may be scanned to form a lift off pattern1702awith intermittent overlapping irradiation zones.FIG. 17Bshows an irradiation pattern1700bthat may be scanned to form a lift off pattern1702bwith overlapping irradiation zones formed along lines in the scanning direction.FIG. 17Cshows an irradiation pattern1700cthat may be scanned to form a lift off pattern1702cwith intermittent overlapping irradiation zones extending in a direction orthogonal to the scanning direction. In the illustrated examples, the non-contiguous beam spots forming the irradiation patterns1700a-care relatively narrow in the scanning direction and relatively wide in the direction orthogonal to the scanning direction.

Although the irradiation patterns discussed above are shown with square, rectangular and hexagonal beam spots, these patterns may be formed using beam spots of any shape, number and spacing.FIGS. 18A and 18B, for example, show irradiation patterns1800a,1800bformed by high density arrays of circular beam spots. The irradiation patterns1800a,1800bmay be formed, for example, by passing a laser through a high density mask such as an on-off mask with 10 micron diameter holes on 20 micron center to center pitch.

FIGS. 18C-18Fshow photomicrographs of irradiation patterns formed at the interface of a sapphire substrate and epi layer by arrays of beam spots with different pitches, different shapes and different fluence levels. The lift off zone may be seen in these photomicrographs around the irradiation zones.FIG. 18Cshows photomicrographs of irradiation patterns formed by arrays of circular beam spots having different sizes and pitches and with a high fluence.FIG. 18Dshows photomicrographs of irradiation patterns formed by arrays of circular beam spots having different sizes and pitches and with a low fluence.FIG. 18Eshows photomicrographs of irradiation patterns formed by arrays of square beam spots having different sizes and pitches and with a high fluence.FIG. 18Fshows photomicrographs of irradiation patterns formed by arrays of square beam spots having different sizes and pitches and with a low fluence. In these examples, the low fluence is just above the ablation threshold.

FIG. 18Gshows a square-shaped irradiation pattern1800gformed by multiple narrow line-shaped beam spots. In one example, line-shaped beam spots with a length of about 300 microns and width of about 3 microns may be spaced about 10 microns to form a square-shaped irradiation pattern of about 300 microns by 300 microns. The square-shaped irradiation pattern1800gmay be used in any of the irradiation patterns discussed above, for example, instead of a solid square-shaped beam spot and may be scanned or positioned across a workpiece using any of the techniques described above to achieve lift off. As shown inFIG. 18H, for example, multiple square-shaped irradiation patterns1800gmade up of narrow line-shaped beam spots may be arranged to form a larger irradiation pattern1800h.

Multiple line-shaped beam spots of different sizes may also be arranged to form irradiation patterns of different sizes, shapes and/or geometries. As shown inFIG. 18I, for example, multiple narrow line-shaped beam spots may be arranged end-to-end to form a longer line-shaped irradiation pattern1800i. In one example, line-shaped beam spots may be spaced only a few microns apart. The longer line-shaped irradiation pattern1800imay be scanned across a workpiece, for example, instead of scanning a homogeneous line-shaped beam spot.

Instead of forming a square-shaped irradiation pattern with multiple narrow line-shaped beam spots as shown inFIG. 18G, small on/off beam spots may be used to form a larger irradiation pattern (e.g., a square shaped pattern of about 300 microns by 300 microns).FIG. 18Jshows an irradiation pattern1800fformed by multiple square-shaped irradiation patterns made up of small beam spots.

FIG. 18Kshows a hexagonal shaped irradiation pattern1800kformed by multiple nested hexagon shaped lines beams (i.e., instead of a solid hexagonal beam spot). The hexagonal shaped irradiation pattern1800kmay be arranged with other hexagonal shaped irradiation patterns1800kin a larger irradiation pattern. The hexagonal shaped irradiation pattern1800kmay also be scanned or positioned with varying degrees of overlap as described above with a solid hexagonal beam spot.

FIG. 18Lshows a chevron shaped irradiation pattern1800lformed by multiple angled line beams. The chevron shaped irradiation pattern1800lmay be scanned with varying degrees of overlap, for example, as described above with other patterns. Multiple chevron shaped irradiation patterns1800lmay also be formed in a larger irradiation pattern.FIG. 18Mshows an irradiation pattern1800mformed by multiple chevron-shaped irradiation patterns1800l.

FIG. 18Nshows an irradiation pattern1800nformed by multiple zig-zag shaped line beams andFIG. 18Oshows an irradiation patterns1800oformed by multiple dashed line beams. These irradiation patterns1800n,1800omay also be scanned with varying degrees of overlap and/or may be formed in a larger irradiation pattern.

By forming irradiation patterns from multiple lines (e.g., as opposed to solid beam spots), the irradiation patterns may be overlapped with sequential radiation patterns with reduced cracking and ghosting effects. The multiple lines provide substantially uniform irradiation and allow the edges of the irradiation pattern to be blended with overlapping irradiation patterns. The irradiation patterns formed by multiple lines may also be overlapped to achieve a roughening effect on the layer being separated, for example, to roughen GaN for enhancing the LED performance. According to another variation, a solid beam spot may be formed in any of the shapes described herein with multiple lines at one or more edges of the solid beam spots to allow overlap with minimal or no ghosting. According to a further variation, a beam spot may be solid at the center with feathered edges.

The irradiation patterns including a plurality of lines or a solid beam spot with lines at the edges, as described above, may be formed by a photomask etched with the desired line pattern. One type of mask that may be used is a chrome/quartz on/off mask. The irradiation patterns including a plurality of lines may also be formed by shaping a beam from a high speed solid state laser to form the line pattern. A beam spot with feathered edges may be formed by a gray scale mask.

FIGS. 19A-19Dshow irradiation patterns (with an aggregate LOZ shown in broken lines) that are designed to irradiate a circular workpiece1001such as a semiconductor wafer. InFIG. 19A, an irradiation pattern1600ais formed by non-contiguous beam spots arranged in a pie-shaped pattern extending from the center to the circumference of the circular workpiece1001. The irradiation pattern1600aand/or the workpiece1001may be rotated to scan the irradiation pattern1600aaround the workpiece. Although the pie-shaped irradiation pattern1600ais shown as a one-quarter circle, larger or smaller pie-shaped patterns may be used.

InFIG. 19B, an irradiation pattern1600bis formed by non-contiguous beam spots arranged in a spoke pattern extending from the center to the circumference of the circular workpiece1001. The irradiation pattern1600band/or the workpiece1001may be rotated to scan the irradiation pattern1600aaround the workpiece. Although the spoke irradiation pattern1600bis shown with four (4) spokes, other numbers of spokes may also be used.

InFIG. 19C, an irradiation pattern1600cis formed by non-contiguous beam spots arranged in an annular pattern around the workpiece1001. The annular irradiation pattern1600cmay be scanned from the circumference to the center of the workpiece1001by moving the beam spots inwardly.

InFIG. 19D, an irradiation pattern1600dis formed by non-contiguous beam spots arranged in a semi-annular or arc pattern around the workpiece1001. The semi-annular irradiation pattern1600dmay be scanned around the circumference workpiece1001and may be scanned inwardly from the circumference to the center of the workpiece1001.

The size, shape and number of beam spots used to form the irradiation patterns1600a-dmay be varied depending upon the size of the workpiece, the materials and the desired energy density.

FIGS. 20A and 20Bshow other techniques for scanning beam spots to perform laser lift off on a circular shaped workpiece1001. InFIG. 20A, a beam spot1710a(e.g., having a cross shape) may be scanned around the workpiece1001in a spiral pattern. In one embodiment, the beam spot1710amay be moved in the spiral pattern, for example, using a galvanometer. In another embodiment, the beam spot1710amay be moved radially toward the center while the workpiece1001is rotated. Although a cross-shaped beam spot is shown, a beam spot or array of beam spots with other shapes may also be scanned in a spiral direction.

InFIG. 20B, an annular beam spot1710bmay be scanned inwardly with a decreasing diameter and width as the beam spot moves. The annular beam spot1710bmay be formed, for example, using an acoustic lens. The annular beam spot1710bmay also be formed as a defocused annular beam that maintains energy density while the width and arc length changes as the beam is scanned inwardly. In another variation, a variable diameter narrow ring of laser light may be scanned from the outside to the center, for example, using an electro optic effect.

Consistent with one embodiment, a laser lift off method is provided for separating layers of material. The method includes: providing a workpiece including at least first and second layers of material; generating at least one laser beam; and irradiating non-contiguous irradiation zones at an interface between the first and second layers with a beam spot formed by the at least one laser beam, wherein lift off zones are formed around each of the irradiation zones at the interface and extending beyond the dimensions of the irradiation zones, wherein laser energy from the laser beam irradiating the irradiation zones is sufficient to cause separation of the layers in the lift off zones.

Consistent with another embodiment, a laser lift off method is provided for separating at least one layer of material from at least one substrate. The method includes: providing at least one substrate having at least one layer of material formed thereon; generating a plurality of laser beamlets; simultaneously irradiating an irradiation pattern with a pattern of beam spots formed by the laser beamlets, the irradiation pattern including non-contiguous irradiation zones at an interface between the layer and the substrate; and moving the irradiation pattern to different locations for sequential irradiations until the layer is separated from the substrate.

Consistent with a further embodiment, a laser lift off method includes: providing a workpiece including at least first and second layers of material; generating at least one laser beam; and irradiating overlapping irradiation zones at an interface between the first and second layers with a beam spot formed by the at least one laser beam and moved in a stepwise direction, wherein the irradiation zones are overlapped such that a substantial number of the locations at the interface are exposed to the same number of pulses of laser irradiation, wherein the number of pulses of laser irradiation at the locations is sufficient to cause separation of the layers.

Consistent with yet another embodiment, a laser lift off system includes: a laser for generating a raw laser beam; a beam shaper for shaping the raw laser beam into a shaped beam; and a spot array generator for receiving the shaped beam and generating an array of non-contiguous beam spots arranged in a predefined pattern.

Consistent with yet another embodiment, a laser lift off system includes: a laser for generating a raw laser beam; a beam shaper for shaping the raw laser beam into a shaped beam and for changing the energy density of the beam; and a galvanometer for scanning the shaped beam spot on the workpiece.