The use of an LMIS and argon ion sputtering in studies of thin film strain gauges

Vacuum ◽  
1984 ◽  
Vol 34 (1-2) ◽  
pp. 321-325 ◽  
Author(s):  
AG Taylor ◽  
RE Thurstans ◽  
DP Oxley
2011 ◽  
Vol 14 ◽  
pp. 164-166
Author(s):  
Fukunori Izumida ◽  
Rongbin Ye ◽  
Koji Ohta ◽  
Mamoru Baba ◽  
Michiko Kusunoki

1995 ◽  
Vol 46 (1-3) ◽  
pp. 213-217 ◽  
Author(s):  
H. Grange ◽  
C. Maeder ◽  
C. Bieth ◽  
S. Renard ◽  
G. Delapierre
Keyword(s):  

2015 ◽  
Vol 26 ◽  
pp. 355-358 ◽  
Author(s):  
Ju-Hyung Kim ◽  
Yuchen Liang ◽  
Soonmin Seo
Keyword(s):  

1991 ◽  
Vol 235 ◽  
Author(s):  
Q. Z. Hong ◽  
J. M. E. Harper

ABSTRACTThe temperature dependence of 300 eV argon ion sputtering of CoSi2 thin films in the range 50–600°C has been investigated. At temperatures above 400°C, the etch rate of CoSi2 on Si is significantly reduced, while the underlying Si reacts with the Co atoms diffusing from the silicide surface. As a result, the silicide layer effectively moves into the substrate during Ar bombardment. During sputtering of CoSi2 on Sio2, the thickness of the silicide layer decreases almost linearly with bombarding time until all the silicide is removed. Similar behavior is observed in low temperature sputtering of CoSi2 on (100) Si and evaporated Si. However, at elevated temperatures (400°C< <600°C), sputtering of CoSi2 on Si undergoes two consecutive stages. During the initial stage, the thickness of the silicide layer decreases at the same rate as that of the silicide on SiO2, and is accompanied by an enrichment in Co concentration near the surface. During the second stage, the etch rate of the silicide is reduced to only one third of the rate during the initial stage.


Author(s):  
Jih-Fen Lei ◽  
Lisa C. Martin ◽  
Herbert A. Will

Advanced thin film sensor techniques that can provide accurate surface strain and temperature measurements are being developed at NASA Lewis Research Center. These sensors are needed to provide minimally intrusive characterization of advanced materials (such as ceramics and composites) and structures (such as components for Space Shuttle Main Engine, High Speed Civil Transport, Advanced Subsonic Transports and General Aviation Aircraft) in hostile, high-temperature environments, and for validation of design codes. This paper presents two advanced thin film sensor technologies: strain gauges and thermocouples. These sensors are sputter deposited directly onto the test articles and are only a few micrometers thick; the surface of the test article is not structurally altered and there is minimal disturbance of the gas flow over the surface. The strain gauges are palladium-13% chromium based and the thermocouples are platinum-13% rhodium vs. platinum. The fabrication techniques of these thin film sensors in a class 1000 cleanroom at the NASA Lewis Research Center are described. Their demonstration on a variety of engine materials, including superalloys, ceramics and advanced ceramic matrix composites, in several hostile, high-temperature test environments are discussed.


1995 ◽  
Vol 02 (02) ◽  
pp. 191-196 ◽  
Author(s):  
ANTONI BUKALUK

Auger electron spectroscopy (AES) in conjunction with argon-ion sputtering was used to determine the diffusion profiles in the thin-film Au-Ag multilayer system. Interdiffusion coefficients, obtained in the temperature range of 175–250°C, have been derived from the change of the concentration amplitude of the structure and from the variation of the composition at the interface of two consecutive layers of the multilayer system. The influence of the depth resolution on the diffusion data have been analyzed and discussed.


2011 ◽  
Author(s):  
Se-Jun Kang ◽  
Mi Ji Lee ◽  
Jae Yoon Baik ◽  
Hyeong-Do Kim ◽  
Anup Thakur ◽  
...  

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