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✷✷ ◆❡✇ ❆♣♣❧✐❝❛t✐♦♥s ♦❢ ❊❧❡❝tr✐❝ ❉r✐✈❡s [3] AskinT.IsikverenandMichaelSchmidt.FutureTransportAircraftUltra-LowEmissions Technology Options. In GARS Workshop Air Transport and Climate Change, Worms, Germany, 2014. [4] Askin T. Isikveren, Arne Seitz, Patrick C Vratny, Clément Pornet, Kay O Plötner, and Mirko Hornung. Conceptual Studies of Universally-Electric Systems Architectures Suitable for Transport Aircraft. In Deutscher Luft- und Raumfahrt Kongress, DLRK, Berlin, 2012. Bauhaus Luftfahrt. [5] Clément Pornet. Hybrid and Universally-Electric Aircraft Concepts. AccessScience, McGraw-Hill Yearbook of Sciences and Technology (McGraw-Hill Education, 2014), http://dx.doi.org/10.1036/1097-8542.YB150553. [6] Timothy P Dever, Kirsten P Duffy, Andrew J Provenza, Patricia L Loyselle, Benjamin B Choi, Carlos R Morrison, and Angela M Lowe. Assessment of Technologies for Noncryogenic Hybrid Electric Propulsion. Technical Report January, NASA/Technical Report 2015-216588, Cleveland, Ohio, 2015. [7] Jeffrey Freeman, Philip Osterkamp, Michael Green, Andrew Gibson, and Benjamin Schiltgen. Challenges and opportunities for electric aircraft thermal management. Aircraft Engineering and Aerospace Technology, 86(6):519–524, September 2014. [8] Susan Liscouët-Hanke. A Model-Based Methodology for Integrated Preliminary Sizing and Analysis of Aircraft Power System Architectures. PhD thesis, Institut National des Sciences Appliquée - Université Paul Sabatier, 2008. [9] James Felder, Hyun Kim, and Gerald Brown. Turboelectric Distributed Propulsion Engine Cycle Analysis for Hybrid-Wing-Body Aircraft. In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, pages 1–25, Orlando, Florida, January 2009. American Institute of Aeronautics and Astronautics. [10] Andrew R Gibson, David Hall, Mark Waters, Benjamin Schiltgen, Trevor Foster, Jonathan Keith, and Philippe J Masson. The Potential and Challenge of TurboElectric Propulsion for Subsonic Transport Aircraft. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, number January, Orlando, Florida, 2010. [11] Gerald V Brown. Weights and Efficiencies of Electric Components of a Turboelectric Aircraft Propulsion System. In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, 2011. [12] HyunDaeKim,JamesL.Felder,MichaelT.Tong,JeffreyJ.Berton,andWilliamJ.Haller. Turboelectric distributed propulsion benefits on the N3-X vehicle. Aircraft Engineering and Aerospace Technology, 86(6):558–561, September 2014. [13] Devaiah Nalianda and Riti Singh. Turbo-electric distributed propulsion: opportunities, benefits and challenges. Aircraft Engineering and Aerospace Technology, 86(6):543–549, September 2014.PDF Image | Electric Drives for Propulsion System of Transport Aircraft
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