Results 211 to 220 of about 15,184 (243)
Some of the next articles are maybe not open access.

Hybrid-electric propulsion integration in unmanned aircraft

Energy, 2017
Abstract Hybrid-Electric Propulsion Systems (HEPS) have emerged as a promising area of research in aerospace engineering as they combine the complementary advantages of internal combustion and electric propulsion technologies while limiting the environmental emissions.
Alessandro Gardi   +2 more
exaly   +2 more sources

Conceptual design of hybrid-electric transport aircraft

Progress in Aerospace Sciences, 2015
Abstract The European Flightpath 2050 and corresponding Strategic Research and Innovation Agenda (SRIA) as well as the NASA Environmentally Responsible Aviation N+ series have elaborated aggressive emissions and external noise reduction targets according to chronological waypoints. In order to deliver ultra-low or even zero in-flight emissions levels,
C. Pornet, A.T. Isikveren
exaly   +2 more sources

Cross-Validation of Hybrid-Electric Aircraft Sizing Methods

open access: yesJournal of Aircraft, 2022
The number of studies on hybrid-electric aircraft is steadily increasing because these configurations can lead to lower operating costs and environmental impact than traditional aircraft.
D Felix Finger   +2 more
exaly   +2 more sources

Review of Electric Machines in More-/Hybrid-/Turbo-Electric Aircraft

open access: yesIEEE Transactions on Transportation Electrification, 2021
Aircraft electrification is currently the best alternative to address the rising demand for more air transportation and deal with anticipated economic and environmental impacts.
Ehab Sayed   +2 more
exaly   +2 more sources

Preliminary Sizing Method for Hybrid-Electric Distributed-Propulsion Aircraft

open access: yesJournal of Aircraft, 2019
The use of hybrid-electric propulsion (HEP) entails several potential benefits such as the distribution of power along the airframe, which enables synergistic configurations with improved aerodynamic and propulsive efficiency.
Reynard De Vries, Roelof Voß
exaly   +2 more sources

Flight-Path Optimization for a Hybrid-Electric Aircraft

Volume 5: Cycle Innovations, 2023
Abstract This study aims to illustrate a sequence that optimizes the flight-path trajectory for a hybrid-electric propulsion system at mission level, in addition to identifying the respective optimum power management strategy. An in-house framework for hybrid-electric propulsion system modeling is utilized.
Konstantinos I. Papadopoulos   +3 more
openaire   +1 more source

Preliminary Sizing of a Hybrid-Electric Aircraft with Structural Batteries

2023
Electric and hybrid propulsion systems have received a great deal of attention in recent years in various branches of transportation including aviation. The unpredictability of oil price in this era, makes a less-oil dependent source of power more attractive for owners and operators in terms of operating costs.
Gennaro Di Mauro   +5 more
openaire   +2 more sources

Energy Storage for Commercial Hybrid Electric Aircraft

SAE Technical Paper Series, 2016
<div class="section abstract"><div class="htmlview paragraph">Energy storage options for a hybrid electric commercial single aisle aircraft were investigated. The propulsion system features twin Geared Turbofan™ engines in which each low speed spool is assisted by a 2,500 HP electric motor during takeoff and climb.
Jonathan M. Rheaume, Charles Lents
openaire   +1 more source

A hybrid electrical power system for aircraft application

1971 IEEE Power Electronics Specialists Conference, 1971
The trend of commercial aircraft today is toward larger size and more electric service power. As the aircraft becomes larger and environmental conditions become more severe, stringent design requirements such as a high degree of reliability, minimum operating cost, and minimum weight are imposed on the aircraft electrical power system. In reviewing the
C. H. Lee, C. Y. Chin
openaire   +1 more source

A design procedure for a hybrid-electric aircraft

2016
The presentation describes a design procedure based on multi-objective genetic algorithms and a backward simulation tool named PLA.N.E.S. The input parameters were the size of engine and electric motor, the specification of the battery and the battery management strategy. The procedure was applied to an unmanned aerial vehicle.
DONATEO, Teresa, SPEDICATO, LUIGI
openaire   +1 more source

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