J. Phys. D: Appl. Phys. 29 (1996) 2098–2103. Printed in the UK Electron energy dynamics in a RF discharge with trapezoidal driving voltage: comparison of experiment and particle-in-cell Monte Carlo collision simulation E Quandt, H-M Katsch and P Mark Institut für Laser- und Plasmaphysik, Universität Essen, D-45117 Essen, Germany Received 13 February 1996, in final form 29 April 1996 Abstract. We report on the properties of a special RF discharge characterized by a trapezoidal shape of the driving voltage pulse. This driving mode offers an advantage in comparison to the common sinusoidal voltage—in allowing the separation in time of effects which are connected with the time derivative of the driving voltage (displacement current, α-mechanism) from effects connected with the amplitude of the driving voltage (production of electrons at the electrodes, γ -mechanism). The energy gain and loss of electrons in this RF discharge are studied in a collision-dominated helium discharge with special emphasis on the α-mechanism. Experimental results of space- and time-resolved plasma-induced emission spectroscopy are compared and combined with the results of a particle-in-cell Monte Carlo collision simulation. It is demonstrated that the electrons gain energy during the temporal change of the discharge voltage at high neutral particle pressure (400 Pa) in the vicinity of both sheaths and that they dissipate energy in these regions by inelastic collisions. At a lower neutral particle pressure (100 Pa) the electrons gain energy in the vicinity of the expanding sheath and lose energy at the contracting sheath. In this case the energy loss by inelastic collisions takes place in the bulk plasma. 1. Introduction Low-temperature RF plasmas are becoming increasingly interesting because of the technical application potential for materials treatment [1]. The parallel plate configuration is applied on a large scale in the semiconductor industry, e.g. for etching and layer deposition. A basic understanding of the mechanisms of radio frequency discharges is required to overcome the widespread method of ‘trial and error’ in process control and to arrive at an optimum choice of the most important plasma parameters. These discharges have therefore been investigated experimentally [2, 3], by analytical modelling [4, 5] and by computer simulations [6–8] over recent years. The experimental and theoretical studies refer so far to sinusoidal excitation of the discharges whereby the heating mechanisms are investigated mostly by spaceand time-resolved plasma-induced spectroscopy. With the exception of RF discharges in the upper kilohertz domain, interpretation of time-resolved plasma-induced emission leads to the following problem. The largest contribution to electron heating on the basis of the displacement current c 1996 IOP Publishing Ltd 0022-3727/96/082098+06$19.50 (α-mechanism) is expected with only a short temporal delay in connection with the highest rate of change of the voltage, e.g. at the zero-crossing of the driving voltage. A quarter period later, the highest voltage is reached at the electrodes so that at the respective cathode a contribution to the electron gain is expected by secondary electron emission (γ -mechanism). Both mechanisms lead to excitation and ionization with a continuous transition between the two mechanisms. Furthermore, with the common 13.56 MHz discharge the time delay between the zero-crossing and the maximum of the discharge voltage is of the same order of magnitude as the typical lifetime of excited states of atoms, so that identification of the heating mechanisms on the basis of the time-resolved light emission is often ambiguous. For this reason a special type of discharge was developed whereby the driving voltage exhibits a trapezoidal profile in time. This allows one to distinguish between effects which are present during the steep voltage edges which are connected to the α-mechanism and between effects which are present during the voltage plateau and which can be connected to the γ -mechanism. With RF discharge with trapezoidal driving voltage this mode of excitation the question of energy gain and loss of electrons based on the α-mechanism in a collisiondominated helium discharge is investigated. In order to arrive at this goal the results of space- and time-resolved plasma-induced emission spectroscopy are compared and combined with results of particle-in-cell (PIC) Monte Carlo collision (MCC) simulations with special emphasis on the space- and time-resolved total excitation of neutrals and the electron energy gain (j · E). Variation of the amplitude of the driving voltage allows one to demonstrate the transition of a discharge driven mainly by the displacement current and predominantly by secondary electron emission (α-mode to γ -mode transition). 2. Experimental set-up The discharge is operated in helium between two circular, parallel, stainless steel electrodes (diameter 12 cm, distance 4 cm) in the pressure range 100 Pa to 400 Pa. The arrangement is similar to the GEC reference cell. The background pressure in the vacuum chamber is approximately 10−6 Pa, the average gas flow amounts to 30 sccm. The discharge is radially confined by a floating cylindrical electrode to provide a defined loss and defined pressure independent of the discharge volume so that better comparability with the one-dimensional model can be expected. Openings within this electrode, covered by fine meshes or provided with long tubes, allow both gas supply and optical diagnostics. The discharge voltage has a trapezoid-like profile with exponential wings (τwing ' 30 ns); the frequency is 300 kHz. Alternating between the electrodes, the instantaneous anode is grounded, and the cathode is driven with the trapezoid voltage pulse (voltage of the plateau 160 V < Utrapez < 300 V, negative with respect to ground). The input power is less than 5 W. A schematic plot of the power circuit is shown in figure 1. 3. Diagnostics A schematic overview of the diagnostics is given in figure 2. The plasma density is measured during the voltage plateau, resolved in time and space with a Langmuir probe. The temporal resolution of the probe measurement is essential, because strong fluctuations of the probe current during the voltage change and in the first quarter of the voltage plateau are observed. These fluctuations would lead to an error in time-integrated measurements. A temporal dependence of the probe characteristic is not observed during the rest of the voltage plateau. A technique developed for pulsed plasmas [9] has been used; it is based on the measurement of the probe current as a function of time for a specific setting of the probe voltage. By changing the voltage setting in a sequence of steps and combining the relevant probe currents the probe characteristic can be constructed for each temporal point within the period. The temporal resolution of this method is 100 ns, the spatial resolution is about 1 mm. For spatiotemporally resolved optical emission spectroscopy a small section of the plasma on the symmetry axis is imaged onto the entrance slit of a monochromator with a movable mirror and lens system. Several lines (e.g. 31 P–21 S, 33 P–23 S, 41 S–21 P, 43 S–23 P) were observed but did not show significantly different results. The emission profiles discussed in addition refer to the atomic transition 31 D–21 P (667.8 nm). This line was chosen for three reasons. First, excitation in the upper 31 D state from the metastable 21(3) S state (excitation energy 2.5(3.3) eV) can be neglected. An estimation shows that the rate for excitation in the upper state is much larger for excitation from the ground level than from the metastable level: Z f (E)σexc(11 S−31 D) n(11 S) dE Z f (E)σexc(21(3) S−31 D) n(21(3) S) dE. Second, the radiative lifetime of the upper level is very short (τlif e ' 15 ns). The application of a commonly used numeric deconvolution algorithm to reconstruct the temporal evolution of excited levels [10] (which is often questionable [11, 12]) is not necessary. The lifetime of the upper level is much shorter than the time constant of the voltage change (τwing ' 30 ns) and the duration of the voltage plateau (tplateau ' 1.7 µs), thus a temporal superposition of the emission initiated by the voltage change (α-mechanism) and by the voltage plateau (γ -mechanism) should not be expected. Due to the small velocity of the excited atoms (gas temperature approximately 300 K) the effect of the lifetime of the upper level on the spatial structure of the emission can be neglected. Third, as estimated, radiation trapping of this line can be neglected (optical thickness approximately 0.001). Consequently, the emitted light reflects directly the excitation of the upper level of the observed transition from the ground state (excitation energy 23.1 eV) and therefore the electron energy loss and the ionization (ionization potential 24.6 eV). The spatial profile of the density of metastables is obtained by exciting the 31 P level from the metastable 21 S state with a dye laser (501.5 nm) and detecting the emission of the same transition. 4. Simulation set-up The PIC MCC simulation codes PDP1 (PC version) and XPDP1 (workstation version) developed by Birdsall [8] are used. The PDP1 simulation runs with approximately 9000 computer particles, a spatial cell width of 0.2 mm and a mean time interval of 5 × 10−11 s. These values are chosen under the conditions ωpe 1t < 2 and λD /1x > 2 [13, 14]. The number of computer particles is chosen with regard to stability and minimization of computation time and is in agreement with the literature [e.g. 15] taking into account the lower plasma density in the trapezoid-like driven discharge. The cross sections for particle–particle collisions are taken from experimental and theoretical data (electron–atom: elastic collisions [16, 17], excitation [18], ionization [19] ; ion–atom: elastic collisions [19], charge 2099 E Quandt et al Figure 1. Schematic plot of the power circuit: 1, electrodes; 2, power resistors; 3, MOSFET transistors; 4, amplifier; 5, inverting amplifier; 6, opto coupler; 7, pulse generator. Figure 2. Schematic of experiment and diagnostics. transfer collisions [20]) and are fitted to the general profiles (cross section versus incident particle energy) for electron– atom and ion–atom collisions given by Birdsall [8]. A value of γ = 0.18 [18] is adopted for the coefficient of secondary electron emission due to the incidence of ions on the electrodes. For more details on the simulation code the reader is referred to the literature [8, 13]. At first, simulated discharges with parameters of the experiment always ‘died’. On the basis of this observation we decided to consider the role of metastables neglected so far in the simulation. In order to take account of their influence, a sinusoidal spatial profile was adopted (this relative spatial variation of the metastables was inferred from laser-induced fluorescence measurements). Ionization of these metastables with a cross section σmax = 1.5 × 10−19 m−2 [18] and secondary electron emission due to the incidence of metastable atoms (γ = 0.7, see [21]) was taken into account. The maximum value of the metastable concentration was then varied in the simulation until the resulting spatial-resolved 2100 plasma density was in agreement with the experimentally determined value (e.g. np = 3 × 1014 m−3 at p = 100 Pa, Utrapez = 160 V). In this way, a density of metastables of 1.5 × 1016 m−3 was determined for the trapezoid discharge at 100 Pa and 160 V. Riley et al [22] measured in a 13.6 MHz helium discharge (np = 2 × 1015 m−3 , p = 0.5 Torr, 50 V zero-to-peak voltage) a total density of metastables of approximately 1.5 × 1017 m−3 . Taking into account that in the 300 kHz trapezoid discharge the plasma density is lower by nearly one order of magnitude than in the 13.6 MHz sinusoidal discharge, a density of metastables of 1.5 × 1016 m−3 seems realistic for this discharge. Comparing ionization rates of metastables and of ground level atoms (in the simulation) leads to the result that, in the investigated discharge, the dominant role of metastables is the emission of secondary electrons. At densities of metastables higher than around 1 × 1017 m−3 Penning ionization has to be taken into account as an additional process [23]. RF discharge with trapezoidal driving voltage Figure 3. Emission on the 667.8 nm helium line. Utrapez = 300 V, T = 3.33 µs, electrodes at x = 0 m and x = 0.04 m. (a ) p = 100 Pa, (b ) p = 400 Pa. 5. Results Figure 3 shows the spatio–temporal emission profiles of a discharge running at high voltage (300 V) and different pressures (100 Pa, 400 Pa). The emission signal is maximum during the trapezoid plateau and drops from the cathode to the anode. This light is obviously caused by secondary electrons. Assuming that excitation out of the ground level and ionization are caused by collisions of neutrals with electrons of similar energy, this discharge is driven by secondary electrons and can be described as γ type. Comparing the emission at low (figure 3(a)) and high pressure (figure 3(b)), the dependence of the penetration depth of secondary electrons in the plasma on the pressure can be noted. Figure 4(a) shows in contrast the spatio–temporal emission profile of a discharge running at low voltage (160 V) and high pressure (400 Pa). Here, emission during the plateau is reduced, and a signal during the voltage change appears with a peak in the vicinity of the expanding sheath (switching the neighbouring electrode from anodic to cathodic). This emission is caused by electrons gaining energy by mechanisms due the change of discharge voltage. Therefore, this discharge can be described as α-type. Figure 4. Trapezoidally driven helium discharge at 400 Pa pressure. Utrapez = 160 V, T = 3.33 µs, electrodes at x = 0 m and x = 0.04 m. (a ) Experiment: emission on the 667.8 nm helium line (corresponds to electron energy loss). (b ) Simulation: total excitation (corresponds to electron energy loss). (c ) Simulation: j · E (corresponds to electron energy gain). Figure 4(b) shows the spatio–temporal excitation of a simulated discharge with the same set of parameters as figure 4(a) (160 V, 400 Pa). It is also maximum during the voltage change in the vicinity of the expanding sheath. The agreement of measured emission (figure 4(a)) and simulated excitation (figure 4(b)) is obvious. 2101 E Quandt et al Figure 5. Trapezoidally driven helium discharge at 100 Pa pressure Utrapez = 160 V, T = 3.33 µs, electrodes at x = 0 m and x = 0.04 m. (a ) Experiment: emission on the 667.8 nm helium line (corresponds to electron energy loss). (b ) Simulation: total excitation (corresponds to electron energy loss). (c ) Simulation: j · E (corresponds to electron energy gain). The fate of an electron from gaining to losing energy is marked by two kinds of collisions—the directional energy gained in the electric field is randomized by elastic collisions with atoms and is lost by inelastic exciting or ionizing collisions with atoms. The mean free path for these collisions leads to an estimate of the spatial distance 2102 of energy gain and loss. At a pressure of 400 Pa λel is approximately 0.2 mm and λinel approximately 4.5 mm. This shows that, compared with the dimensions of the discharge (40 mm), energy gain and loss occur in close proximity. This is confirmed by the appropriate simulated energy gain (j ·E, figure 4(c)), which exhibits a peak in the vicinity of the expanding sheath also. An additional smaller energy gain in the plasma bulk and in the vicinity of the contracting sheath (switching the neighbouring electrode from cathodic to anodic) is obviously related to electrons with an energy below the excitation energy. According to a previously published analytical model [24], the energy gain in the different discharge regions can be explained as follows. Close to the expanding sheath energy gain occurs due to collision-dominated sheath oscillation heating (reflection and acceleration of electrons at a sheath edge moving towards them) and ohmic heating due to elastic collisions of the plasma electrons carrying the displacement current. In the plasma bulk, energy gain can be attributed only to ohmic heating. In the vicinity of the contracting sheath, energy gain is again the sum of sheath oscillation heating and ohmic heating. In this case, however, the effect of the sheath edge moving away from the electrons results in a negative sheath oscillation heating (diffusion cooling). Because the amount of (negative) oscillation heating is smaller than the amount of (positive) ohmic heating, a positive energy gain results. This corresponds to the field reversal heating observed in a sinusoidal RF discharge [25, 26] . At low pressure, the assumption that energy loss and gain occur close together never holds. The mean free paths for elastic and inelastic collisions for a pressure of 100 Pa are approximately λel = 0.7 mm and λinel = 18 mm respectively, figure 5(a) shows the measured emission profile at 100 Pa and a voltage of 160 V. The emission is again maximum during the voltage change, but is broadened in space. In the simulation, the total excitation (figure 5(b)) at a pressure of 100 Pa shows similar behaviour. The energy gain of the electrons in the simulation for a pressure of 100 Pa (figure 5(c)) shows a positive peak during the voltage change in the vicinity of the expanding sheath and a negative peak (electron cooling) in the vicinity of the contracting sheath. The energy gain in the different discharge regions occurs on the basis of the different heating mechanisms in an analogous way to the highpressure (400 Pa) case. However, there is now a weaker influence of the ohmic heating as compared to sheath oscillation heating in the vicinity of the sheaths due to a reduction of elastic electron–atom collisions. In the vicinity of the contracting sheath the addition of positive ohmic heating and negative sheath oscillation heating (slowing down of the electrons) therefore results in negative electron heating, equivalent to electron cooling. The influence of stochastic sheath oscillation heating [27, 28] can still be neglected, but has to be taken into account at lower pressures. 6. Conclusion Comparing and combining experimental measurements and particle-in-cell Monte Carlo collision simulations allowed RF discharge with trapezoidal driving voltage us to identify the spatial and temporal characteristics of energy gain and loss of electrons in a special radio frequency discharge driven by a trapezoidal voltage profile. In this collision-dominated discharge, the energy gain of the electrons occurs predominantly in the vicinity of the sheaths; at low pressure, this gain becomes negative in front of the contracting sheath. Energy loss of the electrons occurs at high pressure similarly in the vicinity of the sheaths; at low pressure, however, it occurs in the plasma bulk. The applicability of the results to a sinusoidal driven discharge was verified by an analogous investigation of a 3.2 MHz symmetrically coupled sinusoidal discharge. Good agreement between experiment and simulation was also obtained in this way. Due to the nature of the sinusoidal driven discharge, there is a complex superposition of α- and γ -mechanisms over most of the cycle—the related emission profiles are thus difficult to interpret. Acknowledgments We are grateful to W Saure for the development of the trapezoid pulse generator. This work is supported by the ‘Deutsche Forschungsgemeinschaft’ in the frame of Sonderforschungsbereich 191. References [1] Rossnagel S M, Cuomo J J and Westwood W D (eds) 1989 Handbook of Plasma Processing Technology: Fundamentals, Etching, Deposition and Surface Interactions (Park Ridge, NJ: Noyes) [2] Oelerich-Hill G, Pukropski I and Kujawka M 1991 J. Phys. D: Appl. Phys. 24 593 [3] Godyak V A, Piejak R B and Alexandrovich B M 1992 Phys. Rev. Lett. 68 40 [4] Graves D B 1987 J. Appl. Phys. 62 88 [5] Belenguer Ph and Boeuf J P 1990 Phys. Rev. A 41 4447 [6] Sommerer T J, Hitchon W N G and Lawler J E 1989 Phys. Rev. Lett. 63 2361 [7] Surendra M and Graves D B 1991 IEEE Trans. Plasma Sci. 19 144 [8] Birdsall C K 1991 IEEE Trans. Plasma Sci. 19 65 [9] Katsch H-M and Quandt E 1992 J. Phys. D: Appl. Phys. 25 430 [10] de Rosny G, Mosburg E R Jr, Abelson J R, Devaud G and Kerns R C 1986 J. Appl. Phys. 59 1052 [11] Gerassimou D E, Cavadias S, Mataras D and Rapakoulias D E 1990 J. Appl. Phys. 67 146 [12] Moore C A, Davis G P and Gottscho R A 1983 Phys. Rev. Lett. 52 538 [13] Birsall C K and Langdon A B 1991 Plasma Physics via Computer Simulation, The Adam Hilger Series on Plasma Physics (Bristol: Adam Hilger) [14] Hockney R W and Eastwood J W 1988 Computer Simulation Using Particles (Bristol: Adam Hilger) [15] Turner M M, Doyle R A and Hopkins M B 1993 Appl. Phys. Lett. 62 3247 [16] LaBahn R W and Callaway 1970 Phys. Rev. A 2 366 [17] de Heer F J and Jansen R H J 1977 J. Phys. B: At. Mol. Phys. 10 3741 [18] Takeishi Y and Hagstrum H G 1964 Phys. Rev. 137 641 [19] Vriens L 1964 Phys. Lett. 8 260 [20] Cramer W H and Simons J H 1957 J. Chem. Phys. 26 1272 [21] Dunning F B, Rundel R D and Stebbings F F 1975 Rev. Sci. Instrum. 46 697 [22] Riley M E, Greenberg K E, Hebner G A and Drallos P 1994 J. Appl. Phys. 75 2789 [23] Sommerer T J and Kushner M J 1992 J. Appl. Phys. 71 1654 [24] Katsch H-M, Müller K G and Quandt E 1993 J. Phys. D: Appl. Phys. 26 2168 [25] Turner M M and Hopkins M B 1992 Phys. Rev. Lett. 69 3511 [26] Surendra M and Dalvie M 1993 Phys. Rev. E 48 3914 [27] Godyak V A 1972 Sov. Phys.–Tech. Phys. 16 1073 [28] Goedde C G, Lichtenberg A J and Liebermann M A 1988 J. Appl. Phys. 64 4375 2103
© Copyright 2026 Paperzz