Results 1 to 10 of about 2,678,759 (230)
Optimization and Analysis of Hybrid Electric System for Distributed Propulsion Tilt-Wing UAV
IEEE Access, 2020 Hybrid electric distributed propulsion tilt-wing UAVs show unlimited application prospects due to their high propulsion efficiency and vertical take-off and landing capabilities.
Cheng He, Yuhong Jia, Dongli Ma
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Applied Sciences, 2020 This paper presents an investigation of the aerodynamic and aeroacoustic interaction of propellers for distributed electric propulsion applications.
Giovanni Bernardini +7 more
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Conceptual Design and Optimization of Distributed Electric Propulsion General Aviation Aircraft
Aerospace, 2023 The interaction between the slipstream of the propellers and the wing of an aircraft with distributed electric propulsion (DEP) could benefit aerodynamics. A conceptual design and optimization are carried out in order to increase the range of an electric
Jiang Wu +3 more
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Research on Modeling and Fault-Tolerant Control of Distributed Electric Propulsion Aircraft
Drones, 2022 Distributed electric propulsion (DEP) aircrafts have high propulsion efficiency and low fuel consumption, which is very promising for propulsion. The redundant thrusters of DEP aircrafts increase the risk of fault in the propulsion system, so it is ...
Jiacheng Li, Jie Yang, Haibo Zhang
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Computational Fluid Dynamics Analyses of a Wing with Distributed Electric Propulsion
Aerospace, 2023 The efficiency increase that distributed propulsion could deliver for future hybrid-electric aircraft is in line with the urgent demand for higher aerodynamic performances and a lower environmental impact.
Oreste Russo +4 more
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Development of a Turbo Electric Distribution System for Remotely Piloted Aircraft Systems [PDF]
Journal of Aerospace Technology and Management, 2021 Turboelectric distributed propulsion systems are paving the way for more electric aircraft systems (TeDP). This type of system provides a solution for some of the drawbacks of current low-energy-density batteries, which limit the ability of long ...
Mithun Eqbal +3 more
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Primary parameters design method for distributed electric propulsion unmanned aerial vehicle
Xibei Gongye Daxue Xuebao, 2021 Distributed electric propulsion technology brings new ideas to the design of unmanned aerial vehicle(UAV), such as improving aerodynamic efficiency and propulsive efficiency, and new concept of vertical/short takeoff and landing configurations.
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Aerospace, 2023 The need for environmentally responsible solutions in aircraft technology is now considered the priority for global challenges related to the limited supply of traditional fuel sources and the potential global hazards associated with emissions produced ...
Vincenzo Cusati +3 more
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Entropy, 2022 The excellent thermophysical properties of supercritical CO2 (sCO2) close to the pseudocritical point make it possible to replace water as the coolant of microchannels in application of a high heat flux radiator.
Yi Tu, Yu Zeng
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Aerospace, 2022 Current environmental policies for the aviation sector motivate the use of cleaner propulsion alternatives in order to reduce their CO2 footprint and noise pollution in the coming years.
Darwin Jimenez +4 more
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