IEE Colloquium on Power Electronics for Demanding Applications 1999
DOI: 10.1049/ic:19990332
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Power electronics for aircraft application

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Cited by 9 publications
(5 citation statements)
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“…Low input current distortions to reduce waste, high power supply component to reduce reactive needs, transformer separation for security, a reduction in the proportion of current to the ground point, and minimal size and weight to increase mobility and power intensity are just a few of the characteristics that power electronic converters must have in order to be used in aircraft. [9].…”
Section: Electric Power Systemmentioning
confidence: 99%
“…Low input current distortions to reduce waste, high power supply component to reduce reactive needs, transformer separation for security, a reduction in the proportion of current to the ground point, and minimal size and weight to increase mobility and power intensity are just a few of the characteristics that power electronic converters must have in order to be used in aircraft. [9].…”
Section: Electric Power Systemmentioning
confidence: 99%
“…In order to have a good transformer's efficiency, full interleaved windings (Fig. 9) are fixed to reduce the resistive factor r F (11):…”
Section: Application Design: From Area Product To Thermal Behaviormentioning
confidence: 99%
“…The DC resistances can easily be expressed knowing the windings' dimensions (14). Finally, the windings' AC resistances can be calculated based on (11), (12) and (14). Fig.…”
Section: Application Design: From Area Product To Thermal Behaviormentioning
confidence: 99%
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“…All of the converters components had to be selected so that normal service maintenance would ensure the retention of their specified characteristics through the full range of operational and environmental conditions likely to be encountered through the life of the aircraft, or support facility, in which they are installed (Taha M 1999).…”
Section: Hardware Designmentioning
confidence: 99%