TY - GEN
T1 - The formation of diamond-like carbon film at atmospheric pressure by the pulsed laser/plasma hybrid deposition method
AU - Wang, Han Pei
AU - Lin, Jehnming
N1 - Copyright:
Copyright 2012 Elsevier B.V., All rights reserved.
PY - 2012
Y1 - 2012
N2 - A pulsed laser/plasma hybrid deposition method has been developed to produce the diamond-like carbon (DLC) film at atmospheric pressure in this work. A plasma torch was used to heat up the carbon particles which were simultaneously ablated by a pulsed laser, thus the kinetic energy of the carbon particle can be increased to form the carbon atoms with amorphous bonding structure of the DLC film. The influences of the plasma flow have been examined at various inlet pressures. According to the experimental results of the carbon film inspected by the Raman spectroscopy, it reveals that the intensity ratio of the D-band to G-band of the carbon film can be reduced to 0.5 by the implementation of plasma flow. Therefore the DLC film was solidly formed. The adhesive strength of the DLC film was also characterized by the scratch test, it can be found that the critical loading of the film on the iron substrate is up to 19 N.
AB - A pulsed laser/plasma hybrid deposition method has been developed to produce the diamond-like carbon (DLC) film at atmospheric pressure in this work. A plasma torch was used to heat up the carbon particles which were simultaneously ablated by a pulsed laser, thus the kinetic energy of the carbon particle can be increased to form the carbon atoms with amorphous bonding structure of the DLC film. The influences of the plasma flow have been examined at various inlet pressures. According to the experimental results of the carbon film inspected by the Raman spectroscopy, it reveals that the intensity ratio of the D-band to G-band of the carbon film can be reduced to 0.5 by the implementation of plasma flow. Therefore the DLC film was solidly formed. The adhesive strength of the DLC film was also characterized by the scratch test, it can be found that the critical loading of the film on the iron substrate is up to 19 N.
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U2 - 10.4028/www.scientific.net/AMM.110-116.3737
DO - 10.4028/www.scientific.net/AMM.110-116.3737
M3 - Conference contribution
AN - SCOPUS:81255171961
SN - 9783037852620
T3 - Applied Mechanics and Materials
SP - 3737
EP - 3741
BT - Mechanical and Aerospace Engineering
T2 - 2nd International Conference on Mechanical and Aerospace Engineering, ICMAE 2011
Y2 - 29 July 2011 through 31 July 2011
ER -