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Thin Film Sensors for Minimally-Intrusive Measurements in Harsh High Temperature EnvironmentAdvanced thin film sensors are being developed to provide accurate surface temperature, heat flux and strain measurements for components used in hostile propulsion environments. These sensors are sputter deposited and microfabricated directly onto the test articles with no additional bonding agent. The thickness of the sensors is only a few micrometers which creates minimal disturbance of the gas flow over the test surface. Thus thin film sensors have the advantage over conventional wire- based sensors by providing minimally intrusive measurement and having a faster response. These thin film sensors are being developed for characterization of advanced materials and structures in hostile, high-temperature environments, and for validation of design codes. This paper presents the advances of three high temperature thin film sensor technologies developed at NASA Lewis Research Center: thermocouples, heat-flux gages and strain gages. The fabrication techniques of these thin film sensors which include physical vapor deposition, photolithography patterning and lead Wire attachment are described. Sensors demonstrations on a variety of engine materials, including superalloys, ceramics and advanced ceramic matrix composites, in several hostile, high-temperature test environments are presented. The advantages and limitations of thin film sensor technology are also discussed.
Document ID
19980237139
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lei, Jih-Fen
(Army Research Lab. Cleveland, OH United States)
Will, Herbert A.
(NASA Lewis Research Center Cleveland, OH United States)
Martin, Lisa C.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 18, 2013
Publication Date
January 1, 1998
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA Paper 98-3610
Meeting Information
Meeting: Propulsion
Location: Cleveland, OH
Country: United States
Start Date: July 13, 1998
End Date: July 15, 1998
Sponsors: Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, American Society of Mechanical Engineers
Funding Number(s)
PROJECT: RTOP 537-04-22
Distribution Limits
Public
Copyright
Other

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