2021
DOI: 10.1109/tte.2021.3050269
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Insulation Materials and Systems for More- and All-Electric Aircraft: A Review Identifying Challenges and Future Research Needs

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Cited by 89 publications
(45 citation statements)
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“…Direct current (dc) distribution systems of current aircrafts are operated at 28 V, 270 V (±135 V) or 540 V (±270 V), whereas alternating current (ac) distribution systems are operated at 230 V or 115 V phase voltage with variable or wide frequency (typically 320–800 Hz) [ 11 ], or 230 V or 115 V phase voltage with constant frequency (400 Hz) [ 12 , 13 ]. In AEA, voltage levels in the range 2 to 3 kV seem advantageous [ 13 ]. It is believed that ac distribution systems in the voltage range between 0.6 and 2 kV lead to wiring systems with less weight, reduced power losses and higher efficiency.…”
Section: Introductionmentioning
confidence: 99%
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“…Direct current (dc) distribution systems of current aircrafts are operated at 28 V, 270 V (±135 V) or 540 V (±270 V), whereas alternating current (ac) distribution systems are operated at 230 V or 115 V phase voltage with variable or wide frequency (typically 320–800 Hz) [ 11 ], or 230 V or 115 V phase voltage with constant frequency (400 Hz) [ 12 , 13 ]. In AEA, voltage levels in the range 2 to 3 kV seem advantageous [ 13 ]. It is believed that ac distribution systems in the voltage range between 0.6 and 2 kV lead to wiring systems with less weight, reduced power losses and higher efficiency.…”
Section: Introductionmentioning
confidence: 99%
“…It is believed that ac distribution systems in the voltage range between 0.6 and 2 kV lead to wiring systems with less weight, reduced power losses and higher efficiency. However, above 2 kV, additional insulation requirements add extra mass to the system, thus needing careful analysis [ 13 ]. Because of the need of more electrical power, next generations MEA aircrafts will probably raise the distribution voltage above 1 kV [ 14 , 15 ].…”
Section: Introductionmentioning
confidence: 99%
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“…A severe challenge stems from the wide range of pressure levels that an aircraft undergoes [6]. It is known that the low-pressure conditions intensify aging mechanisms, such as partial discharge (PD) [7], but the problem goes beyond that. The rapid changes in the pressure level during ascent/descent may lead to condensation, accelerating the aging [8].…”
Section: Introductionmentioning
confidence: 99%