479.575 PEOPLE
| People | Locations | Statistics |
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| Ziakopoulos, Apostolos | Athens |
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| Vigliani, Alessandro | Turin |
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| Catani, Jacopo | Rome |
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| Statheros, Thomas | Stevenage |
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| Utriainen, Roni | Tampere |
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| Guglieri, Giorgio | Turin |
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| Martínez Sánchez, Joaquín |
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| Tobolar, Jakub |
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| Volodarets, M. |
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| Piwowar, Piotr |
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| Tennoy, Aud | Oslo |
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| Matos, Ana Rita |
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| Cicevic, Svetlana |
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| Sommer, Carsten | Kassel |
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| Liu, Meiqi |
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| Pirdavani, Ali | Hasselt |
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| Niklaß, Malte |
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| Lima, Pedro | Braga |
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| Turunen, Anu W. |
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| Antunes, Carlos Henggeler |
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| Krasnov, Oleg A. |
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| Lopes, Joao P. |
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| Turan, Osman |
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| Lučanin, Vojkan | Belgrade |
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| Tanaskovic, Jovan |
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Clare, Jon C.
University of Nottingham
in Cooperation with on an Cooperation-Score of 37%
Topics
- aircraft
- density
- generator
- propulsion
- variable
- implementation
- design
- bus
- voltage
- prototype
- electric power generation
- rectifier
- permanent magnet
- topology
- assessment
- performance evaluation
- electric power
- modernization
- actuating system
- actuator
- civil aircraft
- aileron
- landing gear
- landing
- protection
- rudder
- engine
- weight
- flight
- electric power supply
- capacitor
- motor
- airplane
- electric current
- hydrostatics
- show 5 more
Publications
- 20214-MW Class High-Power-Density Generator for Future Hybrid-Electric Aircraftcitations
- 2021Research and Realization of High-Power Medium-Voltage Active Rectifier Concepts for Future Hybrid-Electric Aircraft Generationcitations
- 2014DC side ripple cancellation in a cascaded multi-level topology for automotive applicationscitations
- 2014Power conversion for a novel AC/DC aircraft electrical distribution systemcitations
- 2013Performance evaluation of 3-phase buck-type PWM rectifiers with integratted and symmetrical Boost converter using SiC MOSFETS for aircraft applicationcitations
- 2013An overview of the more electrical aircraftcitations
- 2012Regeneration of energy onto an aircraft electrical power system from an electro-mechanical actuatorcitations
- 2011Power flow analysis in electro-mechanical actuators for civil aircraftcitations
- 2010Power flow analysis for a two-stage direct power converter for use in an aircraft aileron application
- 2009Aircraft Electrical Landing Gear Actuation Using Dual-output Power Converter with Mutual Power Circuit Componentscitations
- 2009Performance evaluation of two stagematrix converters for EMA in aircraft applicationscitations
- 2008Regeneration in aircraft electrical power systems?citations
- 2008Performance assessment of matrix converter and two stage matrix converter for EMA in aircraft applicationcitations
- 2006Matrix converter protection for more electric aircraft applicationscitations
- 2005A 20 KW matrix converter drive system for an Electro-Mechanical Aircraft (EMA) actuator
- 2004Dynamic performance of a matrix converter driven electro-mechanical actuator for an aircraft rudder
- 2004Power supply loss ride-through and device voltage drop compensation in a matrix converter permanent magnet motor drive for an aircraft actuatorcitations
- 2004An electro-hydrostatic aircraft actuator using a matrix converter permanent magnet motor drive
- 2003A matrix converter based permanent magnet motor drive for an aircraft actuation systemcitations
- 2003Matrix converter solution for aircraft starting
- 2003A Matrix Converter Based Permanent Magnet Motor Drive for an Electro-Hydrostatic Aircraft Actuatorcitations
Places of action
