Knowledge-based functional assessment for the electrical power system design of the all-electric aircraft

dc.contributor.advisorShehab, Essames_ES
dc.contributor.authorMoliner Cantos, Fermínes_ES
dc.date.accessioned2013-09-18T12:41:20Z
dc.date.available2013-09-18T12:41:20Z
dc.date.created2010-09
dc.date.issued2013-09-18
dc.description.abstractConsulta en la Biblioteca ETSI Industriales (8495)es_ES
dc.description.abstract[EN] The all-electric aircraft aims to be the solution for the future generation of aircrafts to enter into service from 2030. There are regulations that are pushing the industry to strive meeting the goals for low emissions in CO2 and NOx, noise and fuel burn. In addition there are some technologies that are under research and could enable these novel systems. The aim of this research is to complete a functional analysis supported by knowledge capture using knowledge sources from within the company and published information of the electrical power system for an all-electric aircraft. The base for the functional analysis is a thorough knowledge acquisition stage conducted within the company and external sources. The functional analysis is completed in a manner that the resulting function model is not solution dependent. The generic functionalities provide a wide frame for different solutions associated to each function. The technical solutions are brought by creative thinking during brainstorm sessions and as output of the previous knowledge acquisition phase. Finally whole system concepts are presented according to four different scenarios, following the functional means analysis method. The results is a new approach the electrical power system of the all-electric aircraft based in system thinking, which facilitate innovation in order to reduce the overall weight of the system. As a conclusion the paper presents the first iteration of a more complex research project that leads to an optimum design of the electrical power system for the All-Electric Aircraft. The methodology used has brought innovative ideas to the research scenario and is the starting point of a longer research project in the way of reducing the weight and cost of the aircraft systems in order to reach feasible levels.en_EN
dc.description.accrualMethodArchivo delegadoes_ES
dc.description.bibliographicCitationMoliner Cantos, F. (2010). Knowledge-based functional assessment for the electrical power system design of the all-electric aircraft. https://riunet.upv.es/handle/10251/32176.es_ES
dc.identifier.urihttps://riunet.upv.es/handle/10251/32176
dc.languageIngléses_ES
dc.publisherUniversitat Politècnica de Valènciaes_ES
dc.rightsReserva de todos los derechoses_ES
dc.rights.accessRightsCerradoes_ES
dc.subjectConsulta en la Biblioteca ETSI Industrialeses_ES
dc.subjectAeronaveses_ES
dc.subject.classificationINGENIERIA ELECTRICAes_ES
dc.subject.otherIngeniero Industrial-Enginyer Industriales_ES
dc.titleKnowledge-based functional assessment for the electrical power system design of the all-electric aircraftes_ES
dc.typeProyecto/Trabajo fin de carrera/gradoes_ES
dspace.entity.typePublication
upv.uuid74c6433b-e04d-4b70-8ed7-8a0ad5714e97es_ES

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