Results 151 to 160 of about 15,184 (243)
Fuel Cell systems in hybrid-electric aircraft
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
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
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
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]
Mesnard B +3 more
europepmc +1 more source
The use of hybrid electric aircraft for skydiving
A.M.F. AL-DARABSE +2 more
openaire +1 more source
An In-Depth Review on Sensing, Heat-Transfer Dynamics, and Predictive Modeling for Aircraft Wheel and Brake Systems. [PDF]
Ramachandra LS +2 more
europepmc +1 more source
Triboelectric Nanogenerators Promote Self-Powered Sensing and Intelligent Monitoring. [PDF]
Cui Y, Yang T, Luo H, Zheng Y.
europepmc +1 more source
A new type of aircraft icing detection system. [PDF]
Renno NO +12 more
europepmc +1 more source
Application of Hybrid-Electric Propulsion to ‘Large-Cabin’ Business Aircraft
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

