Littérature scientifique sur le sujet « Parallel Hybrid-Electric Propulsion System »
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Articles de revues sur le sujet "Parallel Hybrid-Electric Propulsion System"
Lents, Charles E. « Hybrid Electric Propulsion ». Mechanical Engineering 142, no 06 (1 juin 2020) : 54–55. http://dx.doi.org/10.1115/1.2020-jun5.
Texte intégralLeśniewski, Wojciech, Daniel Piątek, Konrad Marszałkowski et Wojciech Litwin. « Small Vessel with Inboard Engine Retrofitting Concepts ; Real Boat Tests, Laboratory Hybrid Drive Tests and Theoretical Studies ». Energies 13, no 10 (20 mai 2020) : 2586. http://dx.doi.org/10.3390/en13102586.
Texte intégralRizzo, Gianfranco, Shayesteh Naghinajad, Francesco Tiano et Matteo Marino. « A Survey on Through-the-Road Hybrid Electric Vehicles ». Electronics 9, no 5 (25 mai 2020) : 879. http://dx.doi.org/10.3390/electronics9050879.
Texte intégralVankan, Jos, et Wim Lammen. « Parallel hybrid electric propulsion architecture for single aisle aircraft - powertrain investigation ». MATEC Web of Conferences 304 (2019) : 03008. http://dx.doi.org/10.1051/matecconf/201930403008.
Texte intégralLitwin, Wojciech, Wojciech Leśniewski et Jakub Kowalski. « Energy Efficient and Environmentally Friendly Hybrid Conversion of Inland Passenger Vessel ». Polish Maritime Research 24, no 4 (20 décembre 2017) : 77–84. http://dx.doi.org/10.1515/pomr-2017-0138.
Texte intégralLitwin, Wojciech, Daniel Piątek, Wojciech Leśniewski et Konrad Marszałkowski. « 50’ Sail Catamaran with Hybrid Propulsion, Design, Theoretical and Experimental Studies ». Polish Maritime Research 29, no 2 (1 juin 2022) : 12–18. http://dx.doi.org/10.2478/pomr-2022-0012.
Texte intégralFigueiras, Iara, Maria Coutinho, Frederico Afonso et Afzal Suleman. « On the Study of Thermal-Propulsive Systems for Regional Aircraft ». Aerospace 10, no 2 (24 janvier 2023) : 113. http://dx.doi.org/10.3390/aerospace10020113.
Texte intégralKost, Gabriel, et Andrzej Nierychlok. « Virtual Driver of Hybrid Wheeled Vehicle ». Solid State Phenomena 180 (novembre 2011) : 39–45. http://dx.doi.org/10.4028/www.scientific.net/ssp.180.39.
Texte intégralHung, J. Y., et L. F. Gonzalez. « On parallel hybrid-electric propulsion system for unmanned aerial vehicles ». Progress in Aerospace Sciences 51 (mai 2012) : 1–17. http://dx.doi.org/10.1016/j.paerosci.2011.12.001.
Texte intégralSeitz, Arne, Markus Nickl, Anne Stroh et Patrick C. Vratny. « Conceptual study of a mechanically integrated parallel hybrid electric turbofan ». Proceedings of the Institution of Mechanical Engineers, Part G : Journal of Aerospace Engineering 232, no 14 (27 juillet 2018) : 2688–712. http://dx.doi.org/10.1177/0954410018790141.
Texte intégralThèses sur le sujet "Parallel Hybrid-Electric Propulsion System"
Harmon, Frederick G. « Neural network control of a parallel hybrid-electric propulsion system for a small unmanned aerial vehicle / ». For electronic version search Digital dissertations database. Restricted to UC campuses. Access is free to UC campus dissertations, 2005. http://uclibs.org/PID/11984.
Texte intégralKaloun, Adham. « Conception de chaînes de traction hybrides et électriques par optimisation sur cycles routiers ». Thesis, Centrale Lille Institut, 2020. http://www.theses.fr/2020CLIL0019.
Texte intégralDesigning hybrid powertrains is a complex task, which calls for experts from various fields. In addition to this, finding the optimal solution requires a system overview. This can be, depending on the granularity of the models at the component level, highly time-consuming. This is even more true when the system’s performance is determined by its control, as it is the case of the hybrid powertrain. In fact, various possibilities can be selected to deliver the required torque to the wheels during the driving cycle. Hence, the main obstacle is to achieve optimality while keeping the methodology fast and robust. In this work, novel approaches to exploit the full potential of hybridization are proposed and compared. The first strategy is a bi-level approach consisting of two nested optimization blocks: an external design optimization process that calculates the best fuel consumption value at each iteration, found through control optimization using an improved version of dynamic programming. Two different systemic design strategies based on the iterative scheme are proposed as well. The first approach is based on model reduction while the second approach relies on precise cycle reduction techniques. The latter enables the use of high precision models without penalizing the calculation time. A co-optimization approach is implemented afterwards which adjusts both the design variables and parameters of a new efficient rule-based strategy. This allows for faster optimization as opposed to an all-at-once approach. Finally, a meta-model based technique is explored
BOGGERO, LUCA. « Design techniques to support aircraft systems development in a collaborative MDO environment ». Doctoral thesis, Politecnico di Torino, 2018. http://hdl.handle.net/11583/2710702.
Texte intégralKaloun, Adham. « Conception de chaînes de traction hybrides et électriques par optimisation sur cycles routiers ». Thesis, Ecole centrale de Lille, 2020. http://www.theses.fr/2020ECLI0019.
Texte intégralDesigning hybrid powertrains is a complex task, which calls for experts from various fields. In addition to this, finding the optimal solution requires a system overview. This can be, depending on the granularity of the models at the component level, highly time-consuming. This is even more true when the system’s performance is determined by its control, as it is the case of the hybrid powertrain. In fact, various possibilities can be selected to deliver the required torque to the wheels during the driving cycle. Hence, the main obstacle is to achieve optimality while keeping the methodology fast and robust. In this work, novel approaches to exploit the full potential of hybridization are proposed and compared. The first strategy is a bi-level approach consisting of two nested optimization blocks: an external design optimization process that calculates the best fuel consumption value at each iteration, found through control optimization using an improved version of dynamic programming. Two different systemic design strategies based on the iterative scheme are proposed as well. The first approach is based on model reduction while the second approach relies on precise cycle reduction techniques. The latter enables the use of high precision models without penalizing the calculation time. A co-optimization approach is implemented afterwards which adjusts both the design variables and parameters of a new efficient rule-based strategy. This allows for faster optimization as opposed to an all-at-once approach. Finally, a meta-model based technique is explored
Ren, Zhongling. « Optimization Methods for Hybrid Electric Vehicle Propulsion System ». Thesis, KTH, Energiteknik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-235932.
Texte intégralHybridfordon är ett aktuellt ämne, på grund av den strikta regleringen gällande fordonsutsläpp. Den optimala designen av hybridfordon är nödvändig för att reducera kostnaden eller utsläppen. Motorsystemet hos ett elektriskt hybridfordon blir mer komplicerat än det hos ett konventionellt fordon, eftersom man måste ta hänsyn till försörjningen av elektrisk energi. Designprocessen involverar design av topologi, design av komponenter samt design av kontrollsystem. Idéen om att sammanfoga alla tre designfaser kallas systemnivådesign. På grund av komplexiteten är det tidsmässigt inte möjligt att evaluera samtliga möjliga designval. Därför behövs optimeringsalgoritmer för att snabba på processen. Olika typer av variabler berörs i de olika designfaserna och därför behövs olika algoritmer. I avhandlingen undersöks olika algoritmers robusthet för kontinuerliga och diskreta variabler samt deras prestanda mot en intern optimeringsplattform. Standardiserade testfall används för att validera algoritmerna vartefter algoritmerna görs mer effektiva och generella. Baserat på teoretiska och experimentella studier föreslås rekommendationer för val av algoritmer baserat på olika typer av variabler. Baserat på optimeringsplattformen introduceras flera olika optimeringskoordinationsarkitekturer för systemnivådesign, och samtidiga och samordnade koordinationsarkitekturer testas för ett specifikt industrifall i den andra delen av avhandlingen. Båda metoderna tycktes vara lovande enligt resultatet av testfallet, och de lyckades sänka konvergensperioden dramatiskt. Den använda fordonsmodellen var inte tillräckligt exakt för att bevisa vilken metod som är den överlägsna, men en mer exakt modell kan introduceras i framtiden för att underlätta en sådan slutsats.
Dreier, Dennis. « Assessing the potential of fuel saving and emissions reduction of the bus rapid transit system in Curitiba, Brazil ». Thesis, KTH, Energi och klimatstudier, ECS, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-176398.
Texte intégralLundin, Johan. « Flywheel in an all-electric propulsion system ». Licentiate thesis, Uppsala universitet, Elektricitetslära, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-222030.
Texte intégralLin, Qing. « Small-Signal Modeling and Stability Specification of a Hybrid Propulsion System for Aircrafts ». Thesis, Virginia Tech, 2021. http://hdl.handle.net/10919/103515.
Texte intégralM.S.
Electric aircraft propulsion (EAP) technologies have been a trend in the aviation industry for their potential to reduce environmental emissions, increase fuel efficiency and reduce noise for commercial airplanes. Achieving these benefits would be a vital step towards environmental sustainability. However, the development of all-electric aircraft is still limited by the current battery technologies and maintenance systems. The single-aisle turboelectric aircraft with aft boundary-layer (STARC-ABL) propulsion concept is therefore developed by NASA aiming to bridge the gap between the current jet fuel-powered aircraft and future all-electric vehicles. The plane uses electric motors powered by onboard gas turbines and transfers the generated power to other locations of the airplane like the tail fan motor to provide distributed propulsion. Power electronics-based converter converts electricity in one form of electricity to another form, for example, from ac voltage to dc voltage. This conversion of power is very important in the whole society, from small onboard chips to Mega Watts level electrical power system. In the aircraft electrical power system context, power electronics converter plays an important role in the power transfer process especially with the recent trend of using high voltage dc (HVDC) distribution instead of conventional ac distribution for the advantage of increased efficiency and better voltage regulation. The power generated by the electric motors is in ac form. Power electronics converter is used to convert the ac power into dc power and transfer it to the dc bus. Because the power to drive the electric motor to provide distributed propulsion is also in ac form, the dc power needs to be converted back into ac power still through a power electronics converter. With a high penetration of power electronics into the onboard electrical power system and the increase of electrical power level, potential stability issues resulted from the interactions of each subsystem need to be paid attention to. There are mainly two stability-related studies conducted in this work. One is the potential cross-domain dynamic interaction between the mechanical system and the electrical system. The other is a design-oriented study to provide sufficient stability margin in the design process to ensure the electrical system’s stable operation during the whole flying profile. The methodology used in this thesis is the impedance-based stability analysis. The main analyzing process is to find an interface of interest first, then grouped each subsystem into a source subsystem and load subsystem, then extract the source impedance and load impedance respectively, and eventually using the Nyquist Criterion (or in bode plot form) to assess the stability with the impedance modeling results. The two stability-related issues mentioned above are then studied by performing impedance analysis of the system. For the electromechanical dynamics interaction study, this thesis mainly studies the rotor dynamics’ impact on the output impedance of the turbine-generator-rectifier system to assess the mechanical dynamics’ impact on the stability condition of the electrical system. It is found that the rotor dynamics of the turbine is masked by the rectifier; therefore, it does not cause stability problem to the pre-tuned system. For the design-oriented study, this thesis mainly explores and provides the impedance shaping guidelines of each subsystem to ensure the whole system's stable operation. It is found that the stability boundary case is at rated power level, the generator voltage loop bandwidth is expected to be higher than 300Hz, 60˚ to achieve a 6dB, 45˚ stability margin, and load impedance mainly depends on the motor-converter impedance.
Nakka, Sai Krishna Sumanth. « Co-design of Hybrid-Electric Propulsion System for Aircraft using Simultaneous Multidisciplinary Dynamic System Design Optimization ». University of Cincinnati / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1602153187738909.
Texte intégralGeiß, Ingmar [Verfasser]. « Sizing of the Series Hybrid-electric Propulsion System of General Aviation Aircraft / Ingmar Geiß ». München : Verlag Dr. Hut, 2021. http://nbn-resolving.de/urn:nbn:de:101:1-2021100123334382521757.
Texte intégralLivres sur le sujet "Parallel Hybrid-Electric Propulsion System"
Simpson, Andrew. Energy storage system considerations for grid-charged hybrid electric vehicles. Washington, D.C.] : U.S. Dept. of Energy, National Renewable Energy Laboratory, Office of Energy Efficiency & Renewable Energy, 2005.
Trouver le texte intégralMin-Huei, Kim, et Lewis Research Center, dir. Advanced propulsion power distribution system for next generation electric/hybrid vehicle : Phase I, preliminary system studies : final report. Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1995.
Trouver le texte intégralBose, Bimal K. Advanced propulsion power distribution system for next generation electric/hybrid vehicle : Phase I, preliminary system studies : final report. Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1995.
Trouver le texte intégralChapitres de livres sur le sujet "Parallel Hybrid-Electric Propulsion System"
Pettes-Duler, Matthieu, Xavier Roboam et Bruno Sareni. « Integrated Design Process and Sensitivity Analysis of a Hybrid Electric Propulsion System for Future Aircraft ». Dans Lecture Notes in Electrical Engineering, 71–85. Cham : Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-37161-6_6.
Texte intégralBancă, Gheorghe, Florian Ivan, Gheorghe Frățilă et Valentin Nișulescu. « Modeling the Performances of a Vehicle Provided with a Hybrid Electric Diesel Propulsion System (HEVD) ». Dans CONAT 2016 International Congress of Automotive and Transport Engineering, 415–26. Cham : Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-45447-4_46.
Texte intégralLee, Bohwa, Poomin Park et Chuntaek Kim. « Power Managements of a Hybrid Electric Propulsion System Powered by Solar Cells, Fuel Cells, and Batteries for UAVs ». Dans Handbook of Unmanned Aerial Vehicles, 495–524. Dordrecht : Springer Netherlands, 2014. http://dx.doi.org/10.1007/978-90-481-9707-1_115.
Texte intégralThomas, Jose, Allen Thomas, Akhil Biju, Aswin Mathew, C. Parag Jose et K. M. Haneesh. « A GPS-Gradient Mapped Database-Based Fuzzy Energy Management System for a Series—Parallel Hybrid Electric Vehicle ». Dans Advances in Electrical Control and Signal Systems, 515–27. Singapore : Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-5262-5_38.
Texte intégralYamin, Mohamad, Cokorda P. Mahandari et Rasyid H. Sudono. « Dynamic Simulation of Wheel Drive and Suspension System in a Through-the-Road Parallel Hybrid Electric Vehicle ». Dans Proceedings of Second International Conference on Electrical Systems, Technology and Information 2015 (ICESTI 2015), 263–70. Singapore : Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-287-988-2_28.
Texte intégral« Electric drive system technologies ». Dans Propulsion Systems for Hybrid Vehicles, 243–324. Institution of Engineering and Technology, 2010. http://dx.doi.org/10.1049/pbrn007e_ch5.
Texte intégral« Design of electromechanical system for parallel hybrid electric vehicle ». Dans Energy Efficiency Improvement of Geotechnical Systems, 39–46. CRC Press, 2013. http://dx.doi.org/10.1201/b16355-6.
Texte intégralSerpi, Alessandro, Mario Porru et Alfonso Damiano. « A Novel Highly Integrated Hybrid Energy Storage System for Electric Propulsion and Smart Grid Applications ». Dans Advancements in Energy Storage Technologies. InTech, 2018. http://dx.doi.org/10.5772/intechopen.73671.
Texte intégralJeevan Danaraj, Edgar. « Electrification for Aero-Engines : A Case Study of Modularization in New Product Development ». Dans Advances in Turbomachinery [Working Title]. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.109006.
Texte intégralBelvisi, Daniele, Raphael Zaccone, Massimo Figari, Sergio Simone et Bruno Spanghero. « BESS-Based Hybrid Propulsion : An Application to a Front Line Naval Vessel Preliminary Design ». Dans Progress in Marine Science and Technology. IOS Press, 2022. http://dx.doi.org/10.3233/pmst220020.
Texte intégralActes de conférences sur le sujet "Parallel Hybrid-Electric Propulsion System"
Papadopoulos, Konstantinos I., Christos P. Nasoulis, Elissaios G. Ntouvelos, Vasilis G. Gkoutzamanis et Anestis I. Kalfas. « Power Flow Optimization for a Hybrid-Electric Propulsion System ». Dans ASME Turbo Expo 2022 : Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/gt2022-84037.
Texte intégralSahoo, Smruti, Xin Zhao, Konstantinos G. Kyprianidis et Anestis Kalfas. « Performance Assessment of an Integrated Parallel Hybrid-Electric Propulsion System Aircraft ». Dans ASME Turbo Expo 2019 : Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gt2019-91459.
Texte intégralMarto, Diogo, et Francisco Brójo. « Hybrid-Electric Propulsion Solutions for UAV Application ». Dans ASME 2022 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/imece2022-95375.
Texte intégralSahoo, Smruti, Mavroudis D. Kavvalos, Dimitra Eirini Diamantidou et Konstantinos G. Kyprianidis. « System-Level Assessment of a Partially Distributed Hybrid Electric Propulsion System ». Dans ASME Turbo Expo 2022 : Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/gt2022-81917.
Texte intégralGhelani, Raj, Ioannis Roumeliotis, Chana Anna Saias, Christos Mourouzidis, Vassilios Pachidis, Justin Norman et Marko Bacic. « Design Methodology and Mission Assessment of Parallel Hybrid Electric Propulsion Systems ». Dans ASME Turbo Expo 2022 : Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/gt2022-82478.
Texte intégralYan, Xingda, James Fleming et Roberto Lot. « Modelling and Energy Management of Parallel Hybrid Electric Vehicle with Air Conditioning System ». Dans 2017 IEEE Vehicle Power and Propulsion Conference (VPPC). IEEE, 2017. http://dx.doi.org/10.1109/vppc.2017.8330923.
Texte intégralLi, Xuefang, Simos A. Evangelou et Roberto Lot. « Integrated Management of Powertrain and Engine Cooling System for Parallel Hybrid Electric Vehicles ». Dans 2018 IEEE Vehicle Power and Propulsion Conference (VPPC). IEEE, 2018. http://dx.doi.org/10.1109/vppc.2018.8604994.
Texte intégralFinger, D. Felix, Carsten Braun et Cees Bil. « Comparative Assessment of Parallel-Hybrid-Electric Propulsion Systems for Four Different Aircraft ». Dans AIAA Scitech 2020 Forum. Reston, Virginia : American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-1502.
Texte intégralOchiai, Kazuki, Yusuke Wada, Yushi Kamiya, Yasuhiro Daisho et Kenji Morita. « Power system modeling and performance evaluation of series/ parallel-type plug-in hybrid electric vehicles ». Dans 2010 IEEE Vehicle Power and Propulsion Conference (VPPC). IEEE, 2010. http://dx.doi.org/10.1109/vppc.2010.5729241.
Texte intégralSun, Xiaoxia, Chunming Shao, Guozhu Wang, Rongpeng Li, Danhua Niu et Jun Shi. « Global Energy Management for Propulsion, Thermal Management System of A Series-parallel Hybrid Electric Vehicle ». Dans 3rd International Conference on Vehicle Technology and Intelligent Transport Systems. SCITEPRESS - Science and Technology Publications, 2017. http://dx.doi.org/10.5220/0006370403320338.
Texte intégralRapports d'organisations sur le sujet "Parallel Hybrid-Electric Propulsion System"
Richter, Tim, Lee Slezak, Chris Johnson, Henry Young et Dan Funcannon. Advanced Hybrid Propulsion and Energy Management System for High Efficiency, Off Highway, 240 Ton Class, Diesel Electric Haul Trucks. Office of Scientific and Technical Information (OSTI), décembre 2008. http://dx.doi.org/10.2172/1092149.
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