Results 1 to 10 of about 18,648,888 (228)

Optimization and Analysis of Hybrid Electric System for Distributed Propulsion Tilt-Wing UAV

open access: yesIEEE 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
doaj   +3 more sources

Parametric Investigation of a Distributed Propulsion System on a Regional Aircraft

open access: yesAerospace, 2022
With the mandatory requirement for more efficient aircraft due to both economic and environmental purposes, academy and industry are exploring new aircraft design opportunities including the concepts of hybrid-electric and fully electric vehicles. Within
Donato de Rosa   +2 more
doaj   +3 more sources

Aerodynamic and Structural Aspects of a Distributed Propulsion System for Commuter Airplane

open access: yesAerospace, 2022
In this paper, an aerodynamic and structural computation framework was produced to develop a more efficient aircraft configuration considering a wing with a distributed electric propulsion and its use in different flight missions.
Pavel Hospodář   +3 more
doaj   +3 more sources

Research on the Aerodynamic–Propulsion Coupling Characteristics of a Distributed Propulsion System

open access: yesApplied Sciences
In recent years, the distributed propulsion system has received extensive attention due to its advantages such as high propulsion efficiency, low noise, high safety redundancy, and good flexibility and maneuverability.
Xiaojun Yang, Tao Liu, Wei Jia
doaj   +3 more sources

Impact of propeller arrangement on aerodynamic performance for a high-lift distributed propulsion system

open access: yesEngineering Applications of Computational Fluid Mechanics
Distributed electric propulsion is an emerging research topic, with a key advantage being its potential for enhanced lift performance through aerodynamic propeller-wing interactions.
Suqi Chen, Zheng Guo, Duoneng Liu
doaj   +3 more sources

Safety boundary protection control for distributed propulsion vehicle operating in plateau environment [PDF]

open access: yesScientific Reports
In plateau environment, aircraft encounter significant challenges stemming from low air density, strong and turbulent winds, insufficient lift and stability, as well as a tendency toward lateral–longitudinal coupling instability. To mitigate these issues,
Zehong Dong   +3 more
doaj   +2 more sources

Development of a Turbo Electric Distribution System for Remotely Piloted Aircraft Systems [PDF]

open access: yesJournal 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
doaj   +3 more sources

Primary parameters design method for distributed electric propulsion unmanned aerial vehicle

open access: yesXibei 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.

doaj   +1 more source

Evaluation of Series and Parallel Hybrid Propulsion Systems for UAVs Implementing Distributed Propulsion Architectures

open access: yesAerospace, 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
doaj   +1 more source

Influences of distributed propulsion system parameters on aerodynamic characteristics of a BLI-BWB UAV

open access: yesXibei Gongye Daxue Xuebao, 2021
Focusing on the aerodynamic characteristics of the blended wing body (BWB) aircraft with boundary layer ingestion(BLI) distributed propulsion system; the influences of propulsion system parameters under the condition of cruise and takeoff are studied ...

doaj   +1 more source

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