Results 151 to 160 of about 15,184 (243)

Fuel Cell systems in hybrid-electric aircraft

open access: yes
With their actual power densities, fuel cell systems are too heavy for aviation. The power density of a fuel cell system can be increased by further developing the subcomponents. Intelligent integration of individual components in the aircraft could be a solution.
Meindl, Markus   +3 more
openaire   +2 more sources

Multi-Disciplinary Design of a Regional Hybrid Aircraft With Different Green Solutions

open access: yes
This study presents an advanced Multidisciplinary Design Optimization (MDO) tailored for the design of next-generation green aircraft, integrating innovative propulsion system.
Franco Mastroddi   +3 more
core  

PON PROSIB (PON 2015-2020) ARS01_00297

open access: yes, 2018
The project will investigate configurations for regional aircraft and rotary wing platform (VTOL - Vertical Take-off & Landing) and architecture for the propulsion systems including distributed hybrid/electric technologies to identify the best strategy ...
NICOLOSI   +4 more
core  

Hybrid Electric Aircraft

open access: yes, 2016
The main concerns of air travel are the operating costs of general aviation aircraft. Hybrid-electric system design provides a great opportunity for future aircraft models to be environmentally friendly.
Righi, Hajar
core  

Aerial drones for graft transport - ready for takeoff? [PDF]

open access: yesTranspl Int
Mesnard B   +3 more
europepmc   +1 more source

The use of hybrid electric aircraft for skydiving

open access: yesRussian Electronic Scientific Journal, 2019
A.M.F. AL-DARABSE   +2 more
openaire   +1 more source

A new type of aircraft icing detection system. [PDF]

open access: yesSci Rep
Renno NO   +12 more
europepmc   +1 more source

Application of Hybrid-Electric Propulsion to ‘Large-Cabin’ Business Aircraft

open access: yesWorld Electric Vehicle Journal
This paper aims to fill a critical cap in hybrid-electric propulsion (HEP) research by investigating the feasibility of its application on a ‘large-cabin’ business aircraft by 2040, for which key requirements are a long range of at least 6297 km (3400 nmi), and a cruise speed of Mach 0.85.
openaire   +1 more source

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