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Instrumentation System Diagnoses a ThermocoupleAn improved self-validating thermocouple (SVT) instrumentation system not only acquires readings from a thermocouple but is also capable of detecting deterioration and a variety of discrete faults in the thermocouple and its lead wires. Prime examples of detectable discrete faults and deterioration include open- and short-circuit conditions and debonding of the thermocouple junction from the object, the temperature of which one seeks to measure. Debonding is the most common cause of errors in thermocouple measurements, but most prior SVT instrumentation systems have not been capable of detecting debonding. The improved SVT instrumentation system includes power circuitry, a cold-junction compensator, signal-conditioning circuitry, pulse-width-modulation (PWM) thermocouple-excitation circuitry, an analog-to-digital converter (ADC), a digital data processor, and a universal serial bus (USB) interface. The system can operate in any of the following three modes: temperature measurement, thermocouple validation, and bonding/debonding detection. The software running in the processor includes components that implement statistical algorithms to evaluate the state of the thermocouple and the instrumentation system. When the power is first turned on, the user can elect to start a diagnosis/ monitoring sequence, in which the PWM is used to estimate the characteristic times corresponding to the correct configuration. The user also has the option of using previous diagnostic values, which are stored in an electrically erasable, programmable read-only memory so that they are available every time the power is turned on.
Document ID
20090016257
Acquisition Source
Kennedy Space Center
Document Type
Other - NASA Tech Brief
Authors
Perotti, Jose
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Santiago, Josephine
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Mata, Carlos
(ASRC Aerospace Corp. United States)
Vokrot, Peter
(ASRC Aerospace Corp. United States)
Zavala, Carlos
(ASRC Aerospace Corp. United States)
Burns, Bradley
(ASRC Aerospace Corp. United States)
Date Acquired
August 24, 2013
Publication Date
June 1, 2008
Publication Information
Publication: NASA Tech Briefs, June 2008
Subject Category
Instrumentation And Photography
Report/Patent Number
KSC-12875
Distribution Limits
Public
Copyright
Public Use Permitted.
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