2018
DOI: 10.1007/978-981-10-8213-9
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Analysis and Design of Power Converter Topologies for Application in Future More Electric Aircraft

Abstract: of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilms or in any other physical way, and transmission or information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed. The use of general descriptive names, registered names, trademarks, service marks, etc. in this publication does not imply, even in the absence of a specif… Show more

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Cited by 3 publications
(3 citation statements)
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“…El circuito de conmutación está compuesto por transistores de potencia, usualmente IGBT, que son controlados por un PWM retroalimentado por el controlador MPPT. En el lado de la carga, se ubica otro capacitor igual a C que está conectado en paralelo con una resistencia (R) [32].…”
Section: Convertidor Elevador Cc-ccunclassified
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“…El circuito de conmutación está compuesto por transistores de potencia, usualmente IGBT, que son controlados por un PWM retroalimentado por el controlador MPPT. En el lado de la carga, se ubica otro capacitor igual a C que está conectado en paralelo con una resistencia (R) [32].…”
Section: Convertidor Elevador Cc-ccunclassified
“…Figura 7: Topología básica del convertidor elevador CC-CC [32] Para el diseño del convertidor elevador usado en esta investigación, algunas consideraciones y valores son fijados previamente. De esta forma, la frecuencia de conmutación (fsw) será 5 kHz, el voltaje de entrada (Vin) igual a 26,4 V, el voltaje de salida (Vout) será 42 V, y la eficiencia del convertidor (ⴄ) del 90% para considerar las corrientes parasitas del circuito.…”
Section: Convertidor Elevador Cc-ccunclassified
“…These topologies suffer from bulky and heavy low-frequency transformer size, lack of DC-link voltage regulation flexibility, high degree of harmonic contents in the input currents, and additional cooling arrangement requirements [4]. In order to avoid the aforementioned issues of the conventional TRUs, an alternative approach is to design a regulated transformer rectifier unit (RTRU) [5] using an actively controlled three-phase AC/DC power factor correction (PFC) [6][7][8][9] and rectification stage followed by a DC/DC isolated converter stage [10][11][12][13][14][15][16] for next generation more-electric airplanes (MEAs).…”
Section: Introductionmentioning
confidence: 99%