Results 31 to 40 of about 21,305 (311)
ObjectivesFor the economic and environmental requirements of polar ice-breakers, a hybrid propulsion system composed of diesel generator sets and a rechargeable battery is proposed.
Wenlong DU, Fengxiang GUO, Li CHEN
doaj +1 more source
Displaced geostationary orbits using hybrid low-thrust propulsion [PDF]
In this paper, displaced geostationary orbits using hybrid low-thrust propulsion, a complementary combination of Solar Electric Propulsion (SEP) and solar sailing, are investigated to increase the capacity of the geostationary ring that is starting to ...
Biggs, James +13 more
core +1 more source
Design of DC grid system for green intelligent hybrid bulk carrier
ObjectiveAccording to the characteristics of the complex waterways of inland rivers, a DC grid solution based on a multi-energy parallel hybrid green intelligent bulk carrier is proposed.
Li SU
doaj +1 more source
Hybrid Propulsion Systems for Remotely Piloted Aircraft Systems
The development of more efficient propulsion systems for aerospace vehicles is essential to achieve key objectives. These objectives are to increase efficiency while reducing the amount of carbon-based emissions.
Mithun Abdul Sathar Eqbal +3 more
doaj +1 more source
IMOTHEP: designing hybrid electric propulsion concepts
Presentation at ONERA-DLR-IRT AESE European workshop on multidisciplinary optimization, Bures-sur-Yvette (FR), 20-21 Sept ...
Novelli, Philippe +3 more
openaire +2 more sources
Ducted fans for hybrid electric propulsion of small aircraft [PDF]
AbstractThis paper presents a method for modeling ducted fan propulsion systems for hybrid-electrically driven small aircraft based on mean line flow analysis methods. Studies of the essential design parameters provide the basis for a discussion of potential advantages when compared to free propellers, as well as possible new fields of application for ...
Daniel Weintraub +3 more
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This work aimed to develop an automatic new methodology based on establishing if a mechanical component, designed for a conventional propulsion system, is also suitable for hybrid electric propulsion.
Umberto Previti +3 more
doaj +1 more source
Development of a Lumped Parameter Model for an Aeronautic Hybrid Electric Propulsion System
This paper describes a case study for applying a hybrid electric propulsion system for general aviation aircraft. The work was performed by a joint team from the Centro Italiano Ricerche Aerospaziali (CIRA) and the Department of Industrial Engineering of
Emma Frosina +4 more
doaj +1 more source
This article presents a preliminary suitable sizing methodology for the design process of the powertrain architecture for a hybrid-electric propulsion system for ultra-light and general aviation aircraft.
Enrico Fornaro +2 more
doaj +1 more source
Reliability Considerations of the Common Unit in Hybrid Electric Propulsion [PDF]
Abstract Since the beginning of aviation, reliability has been one of the most important elements in terms of flight safety and certification. Reliability starts from the smallest part of the aircraft and covers all components up to the entire system.
Gizem Gül, Cemre +3 more
openaire +2 more sources

