Power system for an aircraft with dual hybrid energy sources

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United States of America Patent

PATENT NO 10128662
APP PUB NO 20160204615A1
SERIAL NO

14914871

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Abstract

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A power system for an aircraft having a plurality of power-consuming components, some of which have transient power requirements, which is greater than the average power requirement, the power system includes at least one generator, a power distribution buss, a non-battery power source, a battery power source, and a power controller selectively coupling the non-battery power source and the battery power source to the power distribution buss to satisfy the transient power requirements.

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Patent Owner(s)

  • GE AVIATION SYSTEMS, LLC

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Epps, Phillip Henry Richard Pompano Beach, US 3 19
Radun, Arthur Vorwerk Dayton, US 22 97

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