DocumentCode :
1683482
Title :
Fault tolerant distributed power
Author :
Shi, Fong ; Brockschmidt, Art
Author_Institution :
Boeing Defense & Space Group, Seattle, WA, USA
Volume :
2
fYear :
1996
Firstpage :
671
Abstract :
Redundant power systems are used where safety or power availability is critical. An alternate approach is proposed and compared to existing power system configurations. An example as applied to critical avionics on aircraft is presented, illustrating cost and weight savings in addition to improved power system performance. The reliability models, fault tolerant modular redundant systems and power distribution are discussed as is the proposed fault tolerant system
Keywords :
aircraft; avionics; power supplies to apparatus; redundancy; reliability theory; avionics; cost saving; fault tolerant distributed power; fault tolerant modular redundant systems; power availability; power distribution; reliability models; safety; weight saving; Aerospace electronics; Aircraft; Availability; Costs; Fault tolerance; Fault tolerant systems; Power system faults; Power system modeling; Power system reliability; Safety;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Applied Power Electronics Conference and Exposition, 1996. APEC '96. Conference Proceedings 1996., Eleventh Annual
Conference_Location :
San Jose, CA
Print_ISBN :
0-7803-3044-7
Type :
conf
DOI :
10.1109/APEC.1996.500512
Filename :
500512
Link To Document :
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