NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Triac failure detectorA failure detector is provided for detecting unidirectional failures in triacs, particularly as used in power factor controllers for induction motors. In a first embodiment, the triac voltage waveform is sensed and upon detection of an unbalanced signal, corresponding to failure of the triac in either the positive or negative direction, the triac is turned full on in both directions. In a second embodiment, a pair of pulsed signals are derived, the pulse durations of which are proportional to the phase difference between the load current and voltage for each half cycle, and the triac is turned full on responsive to a difference in pulse duration between the half cycle signals. An unidirectional open circuit detector is adapted to use a signal from either of the first and second embodiment to turn the triac off in response to an open circuit failure in either direction.
Document ID
19830025919
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Nola, F. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
August 23, 1983
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
Patent Number: NASA-CASE-MFS-25607-1
Patent Application Number: US-PATENT-APPL-SN-325886
Patent Number: US-PATENT-4,400,657
Accession Number
83N34190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MFS-25607-1|US-PATENT-4,400,657
Patent Application
US-PATENT-APPL-SN-325886
No Preview Available