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Method and apparatus for conducting structural health monitoring in a cryogenic, high vibration environmentSensors affixed to various such structures, where the sensors can withstand, remain affixed, and operate while undergoing both cryogenic temperatures and high vibrations. In particular, piezoelectric single crystal transducers are utilized, and these sensors are coupled to the structure via a low temperature, heat cured epoxy. This allows the transducers to monitor the structure while the engine is operating, even despite the harsh operating conditions. Aspects of the invention thus allow for real time monitoring and analysis of structures that operate in conditions that previously did not permit such analysis. A further aspect of the invention relates to use of piezoelectric single crystal transducers. In particular, use of such transducers allows the same elements to be used as both sensors and actuators.
Document ID
20130008978
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Qing, Xinlin
Beard, Shawn J.
Li, Irene
Date Acquired
August 27, 2013
Publication Date
January 8, 2013
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-12/358,108
Patent Number: US-Patent-8,347,722
Funding Number(s)
CONTRACT_GRANT: NNM06AA19C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,347,722
Patent Application
US-Patent-Appl-SN-12/358,108
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