Applied Science and Convergence Technology 2017; 26(6): 189-194
Published online November 30, 2017
https://doi.org/10.5757/ASCT.2017.26.6.189
© The Korean Vacuum Society.
Junghoon Joo
Department of Materials Science and Engineering, Kunsan National University, Gunsan, Jeonbuk 573-701, Korea
Correspondence to: E-mail: jhjoo@kunsan.ac.kr
This is an Open Access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/4.0) which permits unrestricted non-commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.
Effects of gas injection scheme and rf driving current configuration in a dual turn inductively coupled plasma (ICP) system were analyzed by 3D numerical simulation using CFD-ACE+. Injected gases from a tunable gas nozzle system (TGN) having 12 horizontal and 12 vertical nozzles showed different paths to the pumping surface. The maximum velocity from the nozzle reached Mach 2.2 with 2.2 Pa of Ar. More than half of the injected gases from the right side of the TGN were found to go to the pump without touching the wafer surface by massless particle tracing method. Gases from the vertical nozzle with 45 degree slanted angle soared up to the hottest region beneath the ceramic lid between the inner and the outer rf turn of the antenna. Under reversed driving current configuration, the highest rf power absorption region were separated into the two inner islands and the four peaked donut region.
Keywords: Plasma, Etching, Gas flow, Rf current, Uniformity, ICP