Mostrando 9 resultados de: 9
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IEEE Transactions on Transportation Electrification(2)
2018 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2018(1)
2019 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2019(1)
2020 AIAA/IEEE Electric Aircraft Technologies Symposium, EATS 2020(1)
2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020(1)
A Direct Current Power System Testbed for a More Electric Aircraft Application
Conference ObjectAbstract: The design concept of more electric aircraft requires a systematic migration of pneumaticand hydraulPalabras claves:Autores:Angel Andres Recalde, Atkin J.A., Bozhko S.V., Sumsurroah S.Fuentes:scopusA reliability approach for the MEA power system architecture design optimization problem
Conference ObjectAbstract: In the literature, there has been thorough research on reliability-based design in different fields.Palabras claves:Aircraft power system architecture, more electric aircraft, network design optimization, reliabilityAutores:Angel Andres Recalde, Atkin J.A., Bozhko S.V., Hill C.Fuentes:scopusDesign of more electric aircraft dc power distribution architectures considering reliability performance
Conference ObjectAbstract: The More Electric Aircraft (MEA) concept has started to define the future of aircraft electrificatioPalabras claves:Autores:Angel Andres Recalde, Atkin J.A., Bozhko S.V.Fuentes:scopusEnergy Storage System Selection for Optimal Fuel Consumption of Aircraft Hybrid Electric Taxiing Systems
ArticleAbstract: Aircraft taxiing is conventionally performed using the main engines' inefficient idle thrust. TherefPalabras claves:Electric taxiing (ET), energy storage system (ESS), lithium-ion batteries, more electric aircraft, taxiing system optimizationAutores:Angel Andres Recalde, Atkin J.A., Bozhko S.V., Connor P.H., Galea M., Giangrande P., Hebala A., Klumpner C., Lukic M., Nuzzo S.Fuentes:scopusOptimal Design and Synthesis of MEA Power System Architectures Considering Reliability Specifications
ArticleAbstract: Aircraft electrification requires novel designs to supply the growing demand for electric power onboPalabras claves:Aircraft power system, Design methodology, linear programming, Optimization methods, reliabilityAutores:Angel Andres Recalde, Atkin J.A., Bozhko S.V.Fuentes:scopusOptimal Weight Power System Design and Synthesis for More Electric Aircraft
Conference ObjectAbstract: The synthesis of a power distribution architecture for More Electric Aircraft requires weight optimiPalabras claves:Autores:Angel Andres Recalde, Atkin J.A., Bozhko S.V.Fuentes:scopusOptimal voltage for more electric aircraft direct current cabling system
Conference ObjectAbstract: More Electric Aircraft will experience a substantial increase in electrical power budget of electricPalabras claves:Autores:Angel Andres Recalde, Atkin J.A., Bozhko S.V., Sumsurroah S.Fuentes:scopusMethodologies for the synthesis of reliable MEA electrical power system architectures
Conference ObjectAbstract: This paper reviews the main optimization approaches and design frameworks found in the literature foPalabras claves:Aircraft power system architecture, more electric aircraft, Network design, Reliability-based design, System reliabilityAutores:Angel Andres Recalde, Atkin J.A., Bozhko S.V.Fuentes:scopusLinear power flow characterization of DC power distribution systems for MEA optimization
Conference ObjectAbstract: The increased utilization of electrical energy in future aviation requires an efficient method to pePalabras claves:Autores:Angel Andres Recalde, Atkin J.A., Bozhko S.V.Fuentes:scopus