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Preliminary study, analysis and design for a power switch for digital engine actuatorsInnovative control configurations using high temperature switches to operate actuator driving solenoids were studied. The impact on engine control system life cycle costs and reliability of electronic control and (ECU) heat dissipation due to power conditioning and interface drivers were addressed. Various power supply and actuation schemes were investigated, including optical signal transmission and electronics on the actuator, engine driven alternator, and inside the ECU. The use of a switching shunt power conditioner results in the most significant decrease in heat dissipation within the ECU. No overall control system reliability improvement is projected by the use of remote high temperature switches for solenoid drivers.
Document ID
19820015520
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Beattie, E. C.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Zickwolf, H. C., Jr.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1979
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-CR-159559
NAS 1.26:159559
PWA-5643-6
Report Number: NASA-CR-159559
Report Number: NAS 1.26:159559
Report Number: PWA-5643-6
Accession Number
82N23394
Funding Number(s)
CONTRACT_GRANT: NAS3-21809
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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