Surface emitting laser structures that include a partially reflecting element disposed in the laser optical cavity are disclosed. Some embodiments involve vertical external cavity surface emitting laser (VECSEL) structures that include a pump source configured to emit radiation at a pump wavelength, λpump, an external out-coupling reflector, a distributed Bragg reflector (DBR) and an active region arranged between the DBR and the out-coupling reflector, the active region configured to emit radiation at a lasing wavelength, λlase. The structure also includes partially reflecting element (PRE) arranged between the gain element and the external out-coupling reflector. The partially reflecting element (PRE) has reflectivity of between about 30% and about 70% for the radiation at the lasing wavelength and reflectivity of between about 30% and about 70% for the radiation at the pump wavelength.
In some implementations, the PRE has reflectivity of between about 40% and about 60% for radiation at the lasing wavelength and reflectivity of between about 40% and about 60% for radiation at the pump wavelength. In some structures, the PRE comprises a lattice of III-V material layers.
During operation of the VECSEL structure, the partially reflecting element can be configured to provide a peak E2 field in the active region that is greater than the average E2 field in the substrate by a factor of more than 2, 3, 4 or even greater.
In some configurations, the pump source is arranged so that the radiation emitted by the pump source is incident on a surface of the substrate at an angle θ such that sin(θ)=nsub sin [cos−1(λpump/λlase)] where the index of refraction of the substrate is nsub. The external out-coupling mirror, DBR, gain region, and PRE can be arranged so that more than about 50% or even more than about 75% of the pump radiation is absorbed in the active region.
According to some aspects, the PRE comprises a distributed Bragg reflector comprising a number of layer pairs, each layer pair comprising a first layer of AlGaN and a second layer of GaN. The first and second layers can be epitaxially grown on a GaN substrate. For example, the PRE may include between 2 and 20 layer pairs or between about 10 and 12 layer pairs. A thickness of the first layer can be about λlase/4nAlGaN(λlase) and a thickness of the second layer cam be about λlase/4nGaN(λlase). For example, in one implementation, the thickness of the first layer is about 50 nm and a thickness of the second layer is about 46 nm. In some cases an antireflective coating is disposed between the substrate and the out-coupling reflector. The antireflective coating can have an index of refraction nAR and a thickness tAR such that tAR=(λpump/4nAR) cos [sin−1((1/nAR)sin θ)].
Some embodiments are directed to a surface emitting laser structure including a first reflector, a second reflector, and an active region arranged between the first reflector and the second reflector, the active region configured to emit radiation at a lasing wavelength, λlase. At least a portion of a substrate is arranged between the gain element and the first reflector. The substrate has a first surface proximate the gain element and a second surface proximate the first reflector. A partially reflecting element (PRE) is epitaxially grown on the first surface of the substrate. The partially reflecting element having reflectivity of between about 40% and about 60% for radiation at the lasing wavelength and reflectivity of between about 40% and about 60% for radiation at a pump wavelength. In some implementations, the substrate portion has a thickness of about 100 μm.
Surface emitting lasers (SELs), such as vertical cavity surface emitting lasers (VCSELs) and vertical external cavity surface emitting lasers (VECSELs) are of interest due to the high quality of spectral and spatial optical lasing characteristics. Realization of SELs within the III-nitride material system is challenging because of the pump power required to produce sufficient power output for many applications. Embodiments discussed herein involve SELs that include three reflecting elements. In addition to the reflecting elements that form the optical cavity for the laser, a third reflector, which is partially reflecting, is disposed within the optical cavity of the laser. The third reflector increases recycling of the laser radiation through the active region of the laser, reducing the threshold power needed for lasing in the SEL and leading to greater lasing efficiency. Some embodiments provided below illustrate operation of a third reflector disposed within the laser optical cavity of optically pumped lasers. These approaches exemplified by these embodiments can be extended to lasers that use diode current injection as an excitation mechanism.
Some embodiments discussed herein use an active region configured to resonate at two distinct wavelengths, the wavelength of the laser radiation and the wavelength of the pump radiation. Quantum well structures within the active region are positioned so that they overlap both the antinodes of the pump standing wave field and the antinodes of the laser standing wave field.
The pump source emits pump radiation 125 which is focused towards the substrate. For example, the VECSEL device may include focusing optics configured to focus the pump radiation onto a spot on the substrate (or anti-reflection coating, if present) by focusing optics. The pump radiation may be incident on the semiconductor structure at an angle, θ with respect to the optical axis of the device indicated by dashed line 126. In some cases, the substrate may be thinned to a thickness that facilitates handling the device, e.g., on the order of about 100 μm, for example. Some radiation 130 generated within the active region of the semiconductor structure (denoted herein as laser radiation) travels through the substrate, out of the semiconductor structure, and toward the external out-coupling mirror, which is designated the first reflector. Some of the radiation generated in the active region passes through the concave out-coupling mirror and is output from the VECSEL device, as indicated by arrow 135 which designates the output laser radiation. A majority of the laser radiation is reflected back to the semiconductor structure, as indicated by arrows 120. The substrate may optionally be coated with anti-reflection coating to reduce the reflection of the recycled laser radiation 120 and/or the pump radiation 125. The antireflection coating can have an index of refraction, nAR, and a thickness, tAR, such that tAR=(λpump/4nAR) cos [sin−1((1/nAR)sin θ)], where λpump is the wavelength of the pump radiation.
Some implementations include an optional frequency converter 136, such as a nonlinear optical crystal that generates radiation at harmonics or at sum or difference frequencies of the laser radiation, disposed within the external cavity. Using a frequency converter, laser outputs 135 in the deep UV spectrum, e.g., less than 300 nm, or even less than about 250 nm, can be obtained from laser wavelengths less than 600 nm.
In one embodiment, the pump source is a gallium nitride (GaN)-based laser diode (or, alternatively, a plurality of laser diodes) emitting in the range of 370-460 nm, and in some embodiments, at 405 nm or 445 nm. The output power of the pump source may be in the range of 1-10 watts. The pump source may include optics that provide a focusing system comprising one or more lenses to focus the pump radiation to a pump beam spot size of 50-200 μm diameter in order to achieve a power density of more than 50 kW/cm2. The output of pump source forms the optical pump that drives the active region. The active region outputs a laser radiation beam at a desired wavelength, for example in the range of 440 nm-550 nm. The external out-coupling mirror may be coated by dielectric layers in order to provide mirror reflectivity at the output wavelength of semiconductor gain region of 99.5% or more.
During operation, the semiconductor structure can become hot. To reduce the possibility of damage to the device due to excess heat generation, the device may be mounted on a heat sink with the second reflector proximate to the heat sink. The heat sink may, for example, be comprised of copper, diamond, or other heat-conducting material. In some cases, an optional second heat sink may be added using laser lift off techniques. In this scenario, laser lift-off is performed to remove the substrate, or the substrate is thinned to a thin substrate remnant. A second heat sink is then mounted to the exposed backside of the third reflector or thin substrate remnant. The completed structure includes two heat sinks, one proximate the second reflector and one proximate the third reflector, with the substrate removed. In the latter example, the second heat sink includes an aperture through which the device is pumped and laser radiation is emitted.
The third reflector 210, designated herein as a partially reflecting element (PRE), is partially reflective to both the pump radiation and the laser radiation. The third reflector 210 is grown over the substrate and may comprise a superlattice of III-V materials, such as a III-nitride superlattice of 5-20 pairs 211 of AlGaN/GaN or InAlN/GaN. For example, in the example of
In some implementations, the second reflector 230 may comprise a dielectric DBR comprising a number of pairs of dielectric material to achieve a specified amount of reflectivity. For example, the dielectric DBR may comprise 8 pairs of 52 nm TiO2/79 nm SiO2 ¼-wavelength layers yielding 99.9% reflectivity at the laser and pump wavelengths of about 460 nm. The second reflector 230 may be formed over the gain structure by such methods as electron beam evaporation (EBE) and/or by sputtering.
The semiconductor structure 201 includes an epitaxial gain region 220 grown over the partially reflecting element 210. In some implementations, gain region 220 comprises a plurality of (e.g., 5-20) quantum wells 224 separated by spacer layers, 225, 227. Quantum well structures 221 may comprise one quantum well or multiple closely spaced quantum wells.
In some implementations, each quantum well structure 221 includes a pair of InxGa1-xN quantum well layers 224, where 0.10≦x≦0.5 separated by a thin spacer of GaN. In general, the quantum well structures can have one or more quantum wells. Each quantum well layer 224 has a thickness of about 3 nm and the thin GaN spacer layer 225 disposed between the quantum well layers 224 has a thickness of about 5 nm. The quantum well structures 221 are separated from each other by thick GaN spacers 227 having a thickness of about 80 nm. The first quantum well structure of the active region 220 may be separated from the third reflector 210 by a GaN layer 222 having a thickness of about 87 nm and the last quantum well structure of the active region 220 may be separated from the second reflector 230 by a GaN layer 223 having a thickness of about 87 nm.
The pump radiation beam forms a standing wave within gain region 220 with a plurality of stationary first antinodes. The laser radiation also forms a standing wave within the active region 220 with a plurality of stationary second antinodes. The quantum well structures 221 are spaced apart from one another such that each quantum well structure 221 is located at an anti-node position of the standing wave pattern of the laser radiation 260 and the pump radiation 250.
Gain structure 220, comprised of a total of N layers, has an optical thickness, OT, determined as:
where the layers, n, include the quantum well layers 224, the thin spacer layers 225, the thick spacer layers 227, and the two end spacer layers 221, 222 separating the first and last quantum well layers from the reflectors 230, 210. That is, gain region 220 has an optical thickness which is the sum of the product of the thickness of each layer multiplied by that layer's refractive index. The active region is designed such that its optical thickness is close to an integer multiple of ½ λlase, where λlase is the laser radiation wavelength. Because the optical thickness depends on the indices of refraction, which may vary with wavelength, the optical thickness may vary with wavelength. A possible design of the active region is therefore one in which OT(λlase)=(Npairs+1) ½ λlase, where Npairs is the integer number of pairs of quantum wells. In this design the antinodes of the standing wave pattern of the lasing radiation have a large overlap with the quantum wells. By properly choosing the angle of incidence and wavelength of the pump laser it is possible to achieve a standing wave pattern having antinodes that overlap with the quantum wells.
The PRE 230 may comprise a superlattice of III-V materials. In one example, the PRE 230 includes 10 layers of AlGaN with a target index of refraction of 2.30. The thickness of each AlGaN layer is about 50 nm. The AlGaN layers are separated by a GaN layer having a thickness of 46.4 nm. The index for AlGaN is consistent with a reflectivity measurement for an AlGaN/GaN DBR. It is also possible to employ other III-V or III-nitride combinations for the partially reflecting element. For example, as previously discussed, InAlN may be used instead of AlGaN to form the PRE. The use of InAlN may facilitate forming good lattice matching between the InAlN and the GaN, leading to reduced strain and enhanced crystalline quality and performance. In general the PRE is designed so that it allows an amount of transmissivity of both the pump radiation and the lasing radiation beam that provides optimal absorption in the quantum wells. For example, in some embodiments, the PRE may be designed to have a transmissivity of about 50% for a pump wavelength and a transmissivity of about 50% for laser radiation having a wavelength, as discussed in more detail below.
As previously mentioned, if the active region (the quantum wells and spacer layers) exhibits fundamental resonance at the pump wavelength the absorption efficiency is greatly enhanced. The active region thickness may cover several periods of the laser mode standing wave and/or the pump mode standing wave.
OT(end spacer)+½NwellsOT(Well)+½(Nwells−1)OT(thin spacer)=½λlase*m′
and
OT(thick spacer)+NwellsOT(Well)+(Nwells−1)OT(thin spacer)=½λlase*m
where OT(end spacer), OT(thick spacer), OT(thin spacer), and OT(Well) denote the optical thicknesses of the end spacer, the thick spacer, the thin spacer, and the optical well, respectively, Nwells is here the number of quantum wells in each period, and m′ and m are integers greater than or equal to one. Typically m′=m=1. In some instances it may be beneficial to increase m or m′ to 2 or more.
OT(end spacer)=IS nGaN, where nGaN is the index of refraction of GaN,
OT(Well)=W nInGaN, where nInGaN is the refractive index of InGaN,
OT(thin spacer)=T nGaN and OT(thick spacer)=L nGaN.
Making the substitutions for the OTs into the equations above for m=m′=1,
ISnGaN+½NwellsWnInGaN+½(Nwells−1)TnGaN=½λlase, and
LnGaN+NwellsWnInGaN+(Nwells−1)TnGaN=½λlase.
The minimum end spacer thickness is: IS=½ λlase−½ NwellsW nInGaN−½(Nwells−1) T nGaN. In some cases, a thicker end spacer may be used. The thickness of the end spacer may be increased by adding an integer multiple, K, of ½ λlase/nGaN to the thickness of the end spacer.
In one design example, gain occurs in an active region comprising a 10×2 series of InGaN quantum wells as previously described in connection with
Note in
As will be appreciated from
Losses in the GaN substrate may arise from weak absorption or scattering of the sub-band-gap radiation. The extinction coefficient k in some GaN substrates may be estimated as k=5×10−6. Based on this extinction coefficient, an absorption constant, α, in the GaN substrate can be estimated as 1.4 cm−1, (α=2ωk/c=4πk/λ, where ω is the frequency of the radiation, λ is the wavelength of the radiation and c is the speed of radiation in a vacuum). Using α=1.4 cm−1 and Tloss=exp(−2 αLGaN), the loss arising from this absorption can be calculated for various thicknesses, LGaN, of the GaN substrate as shown in Table 1.
The estimated pump power required to achieve lasing in the device is given by:
Pth=NthEphNwLwAp/fabsτ(Nth) [1]
where Nth is the carrier density at threshold, Eph is the photon energy, NW is the number of InGaN quantum wells, Lw is the thickness of the wells, Ap is the area of the focused pump beam, fabs is the fraction of power absorbed and τ(Nth) is the carrier lifetime at the carrier density threshold. The dependence of gain on carrier density can be determined as:
g=g0 ln(N/N0), [2]
where g0 is the material gain, N is the carrier density and N0 is the transparency carrier density. For InGaN, g0 can be estimated as 2400 cm−1. The required power to achieve lasing depends on how much radiation is absorbed in the resonant periodic gain region. The fraction of radiation absorbed in the active region as a function of the wavelength of pump radiation was estimated by simulation, and the result is shown in
The carrier lifetime, T, as a function of the carrier density, N, is given as follows:
1/τ(N)=A+BN+CN2, [3]
where coefficients for A, B, and C can be measured. For example, A, B, and C have been measured for InxGa1-x,N (x≈15%) by Y. C. Shen et al. as reported in Applied Phys. Lett. 91, 141101 (2007).
The threshold carrier density is:
Nth=N0[1/(R1R2Tloss)]1/G, [4]
where N0 is the transparency carrier density, R1 is the reflectivity of the external out-coupling mirror (first reflector) and R2 is the reflectivity of the dielectric DBR (second reflector), and Tloss is the factor arising from loss in the GaN substrate.
The gain factor G in the exponent depends on the material gain g0 of the quantum wells, the number of wells, Nw, the thickness of each well, Lw. Γrel is equal to the ratio of peak E2 in the quantum wells to the average value of E2 in the loss region, as indicated in
G=2Γrelg0NwLw. [5]
The third reflector disposed in the laser optical cavity makes it possible to achieve large values of Γrel.
Note that, while the optically pumped VECSEL device used as an example above has been described in terms of particular materials, configuration of the active region, e.g., type, number and thickness of the quantum well region, it is to be understood that other material systems and device configurations could also be used in conjunction with a third reflector as discussed herein. Thus, the present disclosure is not limited to the material systems and device configurations that are described herein. It is contemplated that devices employing a variety of material systems, e.g., other III-V or III-nitride material systems, would benefit from the third reflector. In addition, the specific configuration of the active region could vary, e.g., a cluster of three quantum wells may be used instead of the quantum well pair described. In addition, although only one optical pumping source is described, it will be appreciated, that multiple pumping sources could be used.
The active region includes multiple active region elements, such as about 10 periods of active region elements, is grown on the PRE. Each of the active region elements includes a double quantum well structure based on InGaN. Each active region element may include in order the following layers: an InGaN pre-strain layer (In0.03Ga0.97N, 35.3 nm thick), a first thin spacer (GaN, 5 nm thick), a first quantum well, (In0.18Ga0.82N, 3 nm thick), a second thin spacer (GaN, 5 nm thick), a second quantum well, (In0.18Ga0.82N, 3 nm thick), a thick spacer (GaN, 21.7 nm thick), and an AlGaN carrier confinement and strain management layer (Al0.2Ga0.8N, 20 nm thick).
The second reflector may comprise one or more of epitaxial semiconductor layers and non-epitaxial dielectric layers arranged as a DBR. For example, in come configurations, the second reflector may comprise an epitaxial DBR comprising GaN/AlGaN, such as 10.5 periods of GaN/Al0.2Ga0.8N, where the GaN layers are about 46.8 nm thick and the AlGaN layers are about 48.8 nm thick. A second reflector portion comprising a non-epitaxial dielectric DBR may be deposited on the epitaxial DBR. For example, the dielectric DBR may comprise 4 periods of SiO2/TiO2, wherein the SiO2 layers are 78.8 nm thick and the TiO2 layers are 52.3 nm thick. If two DBR mirrors are joined together to create a single hybrid DBR the highest reflectivity at the target wavelength is obtained when the high refractive index material of the first DBR is in contact with the low refractive index material of the second DBR. Thus the hybrid DBR will have contact between GaN and SiO2 because GaN has a higher refractive index than AlGaN and SiO2 has a lower refractive index than TiO2. The dual DBR that includes an epitaxial semiconductor portion and a non-epitaxial dielectric can be used to achieve a specified thermal conductivity and reflectivity. The epitaxial semiconductor portion can have higher thermal conductivity than the non-epitaxial dielectric portion, whereas the non-epitaxial dielectric portion provides higher reflectivity than the epitaxial-semiconductor portion. In some cases, both the epitaxial DBR and the non-epitaxial DBR are ¼-wavelength DBRs.
Analysis of the reflectivity of an isolated PRE embedded in GaN (as depicted in
The PRE may be designed to achieve a predetermined amount of reflectivity that produces a specified absorption of the pump and/or laser radiation in the active region. A two-step process was employed in the analysis. In the first step, the number of PRE layer pairs was determined based on calculations of the absorption in the active region as a function of wavelength, A(λ), and as a function of number of layers of the PRE. In the second step, the reflectivity of an isolated PRE embedded in GaN (as depicted, for example, in
In connection with step 1,
In connection with step 2, a measure of reflectivity of the PRE can be obtained by embedding the PRE in GaN and modeling reflectivity, R, for incident radiation. The reflectivity as a function of wavelength is calculated below as a function of the number of layers of AlGaN in the PRE. The simulated structure is illustrated in
A number of values and ranges are provided in various aspects of the implementations described. These values and ranges are to be treated as examples only, and are not intended to limit the scope of the claims. For example, embodiments described in this disclosure can be practiced throughout the disclosed numerical ranges. In addition, a number of materials are identified as suitable for various facets of the implementations. These materials are to be treated as exemplary, and are not intended to limit the scope of the claims.
The foregoing description of various embodiments has been presented for the purposes of illustration and description and not limitation. The embodiments disclosed are not intended to be exhaustive or to limit the possible implementations to the embodiments disclosed. Many modifications and variations are possible in view of the above teaching.
This invention was made with Government support under U.S. Army Cooperative Agreement No. W911NF-10-02-0008 awarded by the U.S. Defense Threat Reduction Agency (DTRA). The Government has certain rights in this invention.
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