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In this section we briefly discuss the reflection properties of multilayer structures placed at some angle (0i) to the incident light, this is assumed to comprise only plane waves (see figure 2.2). In this case the phase shift (6) of light passing through a tilted layer is given by equation 2.4.14. The angle 0t refers to the direction of light within the layer and is given through successive application of Snells law of refraction, expressed for the first layer (layer 1) in equation 2.4.15.

Nq sinOj = N, sin0j

(2.4.14) (2.4.15) Initially we may study the basic DBRs, introduced in section 2.4. At normal incidence the reflectivity o f a DBR is independent of the polarisation o f the incident light. This is not the case for a tilted DBR. Denoting waves with electric or magnetic field vectors parallel to the material layers as transverse electric (TE) and transverse magnetic (TM) respectively allows calculation o f the reflectance properties of tilted DBRs. Arbitrary polarisations may be constructed through suitable addition of these two polarisations.

1.0 TE (45°) 0.8 0.4 TM (45°) 0.2 Normal 0.0 950 1000 1050 1100 800 850 900 Wavelength (nm)

Figure 2.19 Theoretical reflection spectra fo r 980nm 7J4 DBR at normal and 45° incidence, showing effect o f polarisation on reflectance.

Figure 2.19 shows the reflection spectra for a DBR, for each of the two polarisations, when light is incident at an angle of 45° to the normal (growth direction). A shift in the central wavelength of the stop-band is observed which is different, in magnitude, for each polarisation. Furthermore the DBR peak reflectivity and stop-band width is decreased for TM polarised light, relative to the TE polarisation. The reflection spectrum shift with angle is of prime importance in assessing the performance of a number of devices. For example vertical cavity surface emitting amplifiers, and optical logic elements, often require input beams incident at some angle to the normal [Raj et al. ‘93]. Also, the optical pumping of VCSELs is regularly performed at an angle so that more light may be injected into the structure. This utilises the reduced reflectivity for specific polarisations and has the added advantage that any reflected pump beam is removed from the system by the oblique incidence (see chapter 4)

The effect of tilting a FP cavity, for example the structure of figure 2.9(a) (Ntop=18, Nbot=20, d=lX), is to shift the FP resonance to shorter wavelengths. This is demonstrated in figure 2.20 which shows the FP mode wavelength (calculated using the transfer matrix model) plotted against the angle of incidence (TE polarisation is assumed).

980 S 975 a 955 60 -60 -40 -20 0 20 40 Angle (degrees)

Figure 2.20 FP wavelength v^. angle fo r m icrocavity structure.

The FP resonance can be seen to shift very quickly for angles greater than 10 degrees. Again this is important for vertical cavity optical logic devices in which case the incident (off- axis) beam wavelength must be altered to match the shifted FP wavelength. This calculation assumes light incident from outside the structure. It is interesting however to note that light emission from within the structure also emits into these off axis modes. We have studied the longitudinal (on axis) mode case in figure 2.14, where it was shown that the wavelength of emission is dictated by the wavelength of the FP mode. Above threshold only this longitudinal mode is of importance as the dominant photon generation process is stimulated emission. However, below threshold the predominant mechanism is that of spontaneous emission. This emission will occur into any modes that are present, with little angular dependence, and as such

will readily radiate light off-axis [Yamanishi ‘92]. Evidently, no emission from the microcavity structure will occur for spontaneous emission at wavelengths longer than the normal incidence FP mode wavelength. Again the emission will have a linewidth dictated by the quality factor (Q, off-axis) of the cavity. This is of particular importance in the design of narrow divergence microcavity light emitting diodes (LEDs) where this off-axis emission imposes limits on the minimum divergence that may be obtained. This effect may be studied by placing a spontaneous emission source (in this case with a guassian profile, and a peak intensity of 1) within the microcavity structure of figure 2.9. The resulting emission from the structure has the radiation pattern shown as the solid line in figure 2.21(a), where a QW emission linewidth of lOnm is assumed (similar to a good quality single QW at room temperature). In this case the peak of the QW emission spectrum coincides with the normal incidence FP mode of the structure (980nm).

Because the divergence in this case is due to spontaneous emission occurring at wavelengths coinciding with off-axis FP modes we might expect that a narrowing of the QW emission spectrum will result in a narrower divergence emission pattern. This is indeed the case and is shown by the dashed pattern in figure 2.21, where a spontaneous emission linewidth of ~5nm is assumed (as might be obtained at low temperature).

1.0 0.0 1.0

(b)

1.0 0.0 1.0

Normalised intensity Normalised intensity

Figure 2.21 Emission patterns (polar) fo r a microcavity structure containing a QW. (a) QW emission peak at FP mode, (b) QW emission peak is 5nm off FP mode.

Interestingly, if the peak of the QW emission is shifted, say by an altering of the QW well- width, to shorter wavelengths then the result is a lobed emission pattern as shown in figure 2.21(b). In this case the solid line is for a QW emitting with a peak at 975nm (linewidth lOnm), the dashed line shows a calculation assuming a linewidth of ~5nm. Yamanishi has used this detuning effect to produce, at low temperature, a variable divergence light emitting diode (LED) [Yamanishi ‘92]. Unfortunately at room temperature the two emission lobes coalesce and the functionality of the device is reduced (as demonstrated by the solid curve in figure 2.21(b)). Thus, without the introduction of narrow band filters to select a fixed FP mode, it seems that

simple one-dimensional optical cavity LEDs will be limited in their divergence performance by the quality (and hence emission linewidth) of their QWs. This will in turn affect LEDs designed to operate at other wavelengths (using different materials) in different ways, dependent strongly upon both the materials forming the cavity and the QWs. Overall, we see that the emission patterns from a microcavity device are dictated by both the optical properties of the cavity and by the emission properties of the QW material. Furthermore, it has been shown that the emission properties (for example the radiative lifetime) of a QW, placed within a microcavity, are influenced strongly by the optical properties of that cavity [Yokoyama et al. ‘90]. These findings add yet more functional parameters into the design of microcavity devices, thereby increasing their range of possible applications.

2,4,4 Effect o f layer thickness variations within microrcavities

The production of DBR mirrors places high demands on the growth (deposition) technology employed. Random errors may be introduced into the thicknesses of individual layers because of short term fluctuations in the source fluxes at the sample surface. These may then reduce the peak reflectivity that may be achieved. Also thickness variations between neighbouring layers may occur due to poor control of element flux and/or substrate temperature. Furthermore a systematic variation of thickness, within all layers, often occurs because of the relative orientations of the growth sources and the sample wafer. This leads to a growth geometry dependent wafer uniformity. Further complications may also arise due to thermal transients across the wafer, which further alter growth rates. These factors can, in general, be reduced by sample rotation and growth rate calibration. Some of these factors are studied, and utilised to advantage, in chapter 4 but a brief introduction is given here.

Figure 2.3(a) shows the reflectivity spectrum for a 20 period A/4 GaAs/AlAs DBR designed for 980nm. Also shown are the shifts in the spectrum when a growth error, or growth non­ uniformity, of 2%, 4% and 6% are applied to each layer in the DBR. The percentages refer to the amount subtracted from each layer of the structure.

Such systematic shifts in DBR centre wavelength are regularly observed across an MBE or MOCVD grown wafer and are dependent on the growth system geometry. They are often utilised to allow the selection of useful areas of the wafer. More generally such shifts in centre wavelength, with the shift given by the percentage growth error, are a problem as they limit the number of useful devices that can be extracted from a wafer. Figure 2.22(b) shows how the reflectivity, at the design wavelength of 980nm, varies with growth error. As previously stated.

in chapter 1, a low threshold VCSEL requires approximately 99% reflectivity within each DBR. It can be seen from figure 2.22(b) that, at 980nm, the peak reflectivity falls below this value when the growth error exceeds 4%. This imposes stringent limits on the growth technology when large numbers of devices, emitting with the same output characteristics (i.e. the same threshold current, voltage and wavelength values), are required from a given wafer.

-4% - i . - 6 % - H « 0.4 \ nominal 800 900 1000 Wavelength (nm) 1100 1.000 0.998 0.996 > 0.994 u C 0.992 u a 0.990 0.988 Reflectivity at 980nm 0.986 0 2 3 4 5 Growth error (%) Figure 2.22 (a) Change in reflectivity with growth error (non-uniformity).

(b) Change in reflectivity at 980nm v^. growth error.

A number of authors [Weber et al. ‘90, Law et al. ‘93] have studied the effect o f altering the thickness of a single X/4 layer from its nominal value. The general conclusion is that small changes (-1% ) do not affect the peak reflectivity appreciably. Unfortunately the phase shift of the DBR, see figure 2.5(b), does change such that VCSELs containing these errors undergo a shift in their emission wavelengths of a few angstroms. Such fluctuations, confined to individual layers, are generally random in nature but it has been proposed that these variations impose limits on the ultimate linewidth achievable with VCSELs [Weber et al. ‘90]. This is due to the lateral thickness variations that may occur across a single device.

If we now take a full microcavity structure and vary only the thickness of the cavity by some percentage, from its nominal value (d), the FP mode position shifts in wavelength. This is shown in figure 2.23. The percentage shift of the FP mode, relative to the design wavelength, is now only approximately given by the percentage variation in the cavity length. This is because o f field penetration into the DBRs, which increases the effective cavity length. This has the effect of decreasing the FP mode shift with changes in d. In general, however, a shift of the cavity resonance is accompanied by a corresponding shift o f the DBR reflection spectrum, see figure 2.22 (i.e. the layer variations occur to all layers). The overall effect, if all layers are

altered by the same percentage, is to shift the FP resonance away from the design wavelength by an amount which is again given by the percentage change in thickness.

u u Cu 1.0 -

ir V"

1

r 0.8 -

Ik Ik

\

0.6 - n d - 2 % ji d - 1 % Nominal : : 1 ! cavity (d) 0.4 - ■ D = a 0.2 - Ntop= 16 Nbot = 20 n n , , 974 976 978 980 Wavelength (nm) 982 984

Figure 2.23 Shift o f FP resonance accompanying variations in cavity length.

Again this effect may be used to advantage to select useful devices from a wafer. Unfortunately this shift in FP wavelength is, in general, not accompanied by an equivalent shift in the gain spectrum, thus a detuning between the peak gain and the mode occurs. This results in devices with a greatly reduced power output and, in cases of extreme shift, to devices that cannot lase. For example, if the gain bandwidth of a QW is 20nm, peaking at 980nm, then a 2% layer thickness variation in all of the layers forming the structure will shift the FP mode to 960nm thereby preventing lasing. The corresponding shift in gain due to the QW width change (nominally 80Â, assuming an Ino.iGaogAs QW, becoming 78Â) will only shift the peak gain by a few nanometres.

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