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High-temperature optically activated GaAs power switching for aircraft digital electronic controlGallium arsenide high-temperature devices were fabricated and assembled into an optically activated pulse-width-modulated power control for a torque motor typical of the kinds used in jet engine actuators. A bipolar heterojunction phototransistor with gallium aluminum arsenide emitter/window, a gallium arsenide junction field-effect power transistor and a gallium arsenide transient protection diode were designed and fabricated. A high-temperature fiber optic/phototransistor coupling scheme was implemented. The devices assembled into the demonstrator were successfully tested at 250 C, proving the feasibility of actuator-located switching of control power using optical signals transmitted by fibers. Assessments of the efficiency and technical merits were made for extension of this high-temperature technology to local conversion of optical power to electrical power and its control at levels useful for driving actuators. Optical power sources included in the comparisons were an infrared light-emitting diode, an injection laser diode, tungsten-halogen lamps and arc lamps. Optical-to-electrical power conversion was limited to photovoltaics located at the actuator. Impedance matching of the photovoltaic array to the load was considered over the full temperature range, -55 C to 260 C. Loss of photovoltaic efficiency at higher temperatures was taken into account. Serious losses in efficiency are: (1) in the optical source and the cooling which they may require in the assumed 125 C ambient, (2) in the decreased conversion efficiency of the gallium arsenide photovoltaic at 260 C, and (3) in impedance matching. Practical systems require improvements in these areas.
Document ID
19850004593
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Berak, J. M.
(United Technologies Research Center East Hartford, CT, United States)
Grantham, D. H.
(United Technologies Research Center East Hartford, CT, United States)
Swindal, J. L.
(United Technologies Research Center East Hartford, CT, United States)
Black, J. F.
(United Technologies Research Center East Hartford, CT, United States)
Allen, L. B.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-174711
NAS 1.26:174711
UTRC-R83-925312-25
Report Number: NASA-CR-174711
Report Number: NAS 1.26:174711
Report Number: UTRC-R83-925312-25
Accession Number
85N12901
Funding Number(s)
CONTRACT_GRANT: NAS3-22535
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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