Results 101 to 110 of about 3,861 (237)

Turboelectric Distributed Propulsion System Modelling [PDF]

open access: yes, 2013
The Blended-Wing-Body is a conceptual aircraft design with rear-mounted, over wing engines. Turboelectric distributed propulsion system with boundary layer ingestion has been considered for this aircraft.
Liu, Chengyuan
core  

Interaction Between Vortex‐Induced Vibrations and Base Vibrations in Piezoelectric Harvesters

open access: yesInternational Journal of Mechanical System Dynamics, EarlyView.
ABSTRACT In the present era, powering sensors using green energy is a significant challenge. One promising solution for the power supply of small sensors relies on piezoelectric energy harvesters excited by vortex‐induced vibrations (VIVs) generated by wind.
Michele Tonan   +3 more
wiley   +1 more source

HASTECS: A typical MDO process for future Hybrid Electric aircrafts

open access: yes, 2021
International audienceIn the framework of hybrid and full electric design of future greener aircrafts, this paper focuses on the multidisciplinary design optimization (MDO) of the powertrain system for a series hybrid electric architecture.
Roboam, Xavier
core  

Preliminary weight sizing of light pure-electric and hybrid-electric aircraft

open access: yesTransportation Research Procedia, 2018
Abstract The lack of consolidated preliminary design techniques coping with the characteristics of most recent electric and hybrid-electric power plants is often an obstacle for aircraft manufacturers and for owners and operators as well, making the design process less straightforward and hampering comparisons with respect to more traditional designs.
Riboldi, Carlo E. D.   +2 more
openaire   +3 more sources

Uncertainty, Sensitivity, and Efficiency Analysis of a Hybrid Piezoelectric–Electromagnetic Energy Harvester

open access: yesInternational Journal of Mechanical System Dynamics, EarlyView.
ABSTRACT Digitalization and emerging technologies are increasing the demand for wireless sensing and the Internet of Things (IoT), which provide opportunities for autonomous sources of electricity in the form of energy harvesting systems. This paper focuses on the challenges in hybrid piezoelectric‐electromagnetic kinetic energy harvesting systems that
Petr Sosna, Damian Gaska, Zdeněk Hadaš
wiley   +1 more source

Hybrid and electric propulsion system of aircrafts [PDF]

open access: yesAIP Conference Proceedings, 2021
V. G. Volchenko, A. N. Ser’yoznov
openaire   +1 more source

Fault Detection of Electric Motors via Symmetrized Dot Pattern‐Based Features

open access: yesInternational Journal of Mechanical System Dynamics, EarlyView.
ABSTRACT This study proposes a novel symmetrized dot pattern (SDP) approach using designed SDP‐based features, extracted from transformed vibration signals, for fault detection. These features describe the compactness, inclination, and shape of the “snowflake” diagram distributions.
Mario Spirto   +6 more
wiley   +1 more source

Microphysics and interactions of aerosols and fog on the northwest Atlantic Ocean

open access: yesQuarterly Journal of the Royal Meteorological Society, EarlyView.
In the Grand Banks, aerosol size distributions were bimodal, aerosol and fog droplet concentrations were low, and fogs were shorter (<12 hours). In contrast, near Sable Island, aerosol size distributions had a single broad mode that was likely influenced by continental emissions, corresponding with higher aerosol and droplet concentrations as well as ...
Gianina Giacosa   +11 more
wiley   +1 more source

Research on Climb Performance Optimization of Small Hybrid‑Electric Aircraft

open access: yesNanjing Hangkong Hangtian Daxue Xuebao
In order to analyze the influence of degree of hybridization and the number of electric motors on the climb performance of small hybrid‑electric aircraft and the selection of different performance parameters in the climb stage, according to the ...
CHU Shuanglei, YANG Jing, WEI Zhiqiang
doaj   +1 more source

Modeling and simulation enabled UAV electrical power system design

open access: yes, 2011
With the diversity of mission capability and the associated requirement for more advanced technologies, designing modern unmanned aerial vehicle (UAV) systems is an especially challenging task.
Rakhra, Puran   +11 more
core   +1 more source

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