1 MeVARC-5 2015 Tel Aviv University Electrical Discharge and Plasma Laboratory Depart of Electrical Engineering - Physical Electronics Experimental Study.

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Presentation transcript:

1 MeVARC Tel Aviv University Electrical Discharge and Plasma Laboratory Depart of Electrical Engineering - Physical Electronics Experimental Study of Vacuum Arcs with Refractory Anodes I.I. Beilis and R.L. Boxman

2 MeVARC Outline Vacuum arc-refractory anode: –Conventional vacuum arc –Open cylindrical electrode configuration, HRAVA –Closed electrode configuration, “Black Body” Measurements. –a) Electrode effective voltage –b) Anode temperature –c) ion current –d) Thin film deposition Summary

3 MeVARC Conventional vacuum arc Cathode Spot Ring Anode Jet Water Experiment: U cef =6.2V- Daalder, 1977 (100A) 8V – Reece, 1963 (30A) Theory: U cef =8V- Beilis, High Temp Effective cathode voltage. Definition: U cef [V]=Q/I Q –cathode heat flux [W], I [A] Cathode spot, jet: Current supported by cathode spots - electron emission and cathode heating High local evaporation rate and dense plasma and MP’s generation Supersonic, fully ionized, high kinetic energy eV plasma jet generation Different applications including vacuum arc deposition (MP) V- Arc is low voltage discharge V’s

4 MeVARC Cathode Spot & Cathode Plasma Jet Beilis, VAST-1995; IEEE TPS: : APL Cathode Cathode Spot Region Hydrodynamic Plasma Flow Sheath Electron emission Energy relaxation zone. Ion diffusion Kinetic flow Knudsen Layer Plasma Jet Expansion  Acceleration: e  i and e  a. Velocity depends on ratio Je/(Ji+Ja)

5 Macroparticle – Plasma cleaning MeVARC Magnetic Filtered Vacuum Arc Disadvantages: Usually low efficiency of material utilizationUsually low efficiency of material utilization Complex equipmentComplex equipment MethodMaterialRate, µm/min PVD (Magnetron sputtering) IPVD (Ionized PVD) Ti Al on SiO CVDCu on TiN Cu on Si wafer PACVD (Plasma assisted) Cu on SiO2, Al SSMD (Self Sputtering)Cu on Si wafer ElectrolessCu on Si wafer Magnetic Filtered Vacuum Arc Deposition Cu on glass0.1 Deposition Methods

6 Vacuum arc with Refractory Anode MeVARC One hole Anode: Shower Anode: MP Vacuum Arc with Black Body Assembly Assembly(VABBA): Hot Refractory Anode Vacuum Arc (HRAVA): HRAVA development

7 Vacuum arc with Refractory Anode MeVARC  calorimetric test,  Thermocouple  Optical Microscopy, SEM  Photography  Electrical probe  Profilometry Experimentalmethodology Water cooled Cathode, Gr,Cu, Cr, Ti Length: 40mm; Diameter: D=30mm VABBA-Anode Length: 22mm; D=50mm, W-250 holes (D=1mm) Ta-1 hole, D=4mm HRAVA Anode A-C distance Anode thickness W, Mo h=5-10mm 5, 10, 20, 30mm Arc current, I150, 175, 200, 225, 250 A Arc time, t~180s W-Thermocouple T-Thermocouple K-type (chromel-alumel) W/5%Re-W/26%Re Water flow rate, F0.193, 0.29 L/s Ion Probe Plasma probe W rod 1.5mm diameter, V bias =-20V Chamber-total current Conditions

8 MeVARC Experimental Setup. Experimental Setup. VABBA Deposition. Shutter Calorimetric test. Ion current

9 MeVARC HRAVA plasma. Effective cathode (Cu) & anode (Gr) voltages Cathode: U cef ~7V Anode: U aef ~ 11-12V (t<10s) 6.5V (t>60s) Jet energy IU j =anode+ surrounding! (t>60s) (t>60s) Rosenthal, Beilis, Goldsmith, Boxman, JPhysD 1995 Beilis, Goldsmith, Boxman, PoP 2000 and 2002

10 MeVARC VABBA plasma and effective cathode voltage Shower W Anode, 250 holes-1mm: One hole (4mm) Ta Anode:

11 MeVARC U cef (VABBA)=11-12V consists of: 1) U cef = 6.5V (conventional from the spot) and 2) part of returned plasma jet energy U j (12V) that not expands to surroundings and remains in the closed electrode configuration! IEEE Trans. Plasma Sci., 41, N8, Part II, 1992, 2013

12 MeVARC W Anode surface temperature vs. time with anode thickness as parameter (HRAVA) IEEE Trans. Plasma Sci., 39, N6, Part I, 1307, 2011

13 MeVARC Ion current (HRAVA) Ion current as function of arc current h=10mm Ion current fraction f i as function on gap I=200A --at first few seconds (8%) --at steady state (11%) J. Appl. Phys., 111, Part I, , 2012 Appl. Phys. Lett. 88, , 2006

14 MeVARC Ion current dependence on probe distance L, Cu, I=200A (VABBA) W shower anode 250 holes, 1mm diameter Ta anode with one hole (4mm diameter) IEEE Trans. Plasma Sci., 41, N8, Part II, 1987, 2013

15 MeVARC Plasma parameters, HRAVA Plasma density vs. I Plasma temperature vs. I Ion energy E i vs. distance I=200 A, h = 10 mm. Plasma Sour. Sci. & Techn., 18 (2009)

16 MeVARC Metallic film deposition, W anode At L=80mm: Cr, I=200, 250, 300A, Cu, I=200A At L=100mm: Ti, I=200 and 300A ConventionalArc Dependence on current, A Temporal evolution (HRAVA) Refractory anode 100  m Glass substrate h=10mm Shutter open for 15s Surf. &Coat. Techn., 203, Is.5-7, 501, 2008

17 Microelectronics Trenches filling by Cu, HRAVA MeVARC nm wide  300 nm deep The deposition rate was ~0.5 µm/min. Film deposited with 2 min exposure at a distance of 110 mm, using pulsed biasing with amplitude -100 V, 80% duty cycle and a frequency of 60 KHz. Microelectronic Engineering, 85,1713, 2008

18 MeVARC Cu deposition rate on glass, h=10mm, VABBA W shower anode (250 holes, 1mm), 200A Ta shower anode (250 holes, 0.6mm), 200A Surf. &Coat. Techn., 258, 908, 2014

19 MeVARC SUMMARY  The refractory anode arc characterized by plasma plume expanding radially (HRAVA) or directly (VABBA). Plasma – is the cathode material!  Cathode U cef in VABBA increases to ~6.5 V for cold anodes (like conventional cathodic arc) & then to steady state of ~11-12 V after anode is heated  The ion flux fraction (12%) in arc with refractory anode was larger in comparison to conventional arc (8%)  Plasma temperature was T e ~ eV, density>10 14 cm -3, and plasma was accelerated up to ~15 eV during its expansion.  The arc is a simple metallic plasma source for coatings. The high efficiency is determined by MP’s conversion into plasma  Steady-state HRAVA deposition rate reach 3.6(Cu), 1.8(Ti) and 1.4µm/min (Cr) for I=300A, while PVD, CVD, FVAD showed about 0.1µm/min ( Review: Surf. & Coat. Techn., 204, N6-7, 865, 2009 ).

20 MeVARC Thank You Samuel Goldsmith Michael Keidar Alexey Shashurin David Arbilly Arye Snaiderman Dmitry Grach. Yosef Koulik Thanks to our colleagues: