| People | Locations | Statistics |
|---|---|---|
| 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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Santarelli, Massimo
in Cooperation with on an Cooperation-Score of 37%
Topics
- engine
- propulsion
- contaminant
- safety
- weight
- passenger
- vehicle occupant
- temperature
- gas
- warehousing
- fuel cell
- electrification
- motor
- passenger aircraft
- hydrogen
- aviation
- greenhouse gas
- hydrogen storage
- kerosene
- mobility concept
- low density
- industry
- road
- highway traffic
- carbon
- oxide
- biomass
- synthetic
- carbon dioxide
- modernization
- electrolysis
- synthetic fuel
- ship
- simulation
- feeding stuff
- sulfur
- fuel
- purification
- experiment
- engineering
- catalyst
- economic capital
- operating costs
- alarm system
- anode
- chlorine
- capital costs
- tar
- aircraft
- data
- reliability
- estimate
- power train
- electric power supply
- design
- control system
- sensor
- dynamic model
- calibration
- parametric analysis
- sensitivity analysis
- sensitivity
- uncertainty
- hydrogen fuel
- temperature sensor
- city
- noise
- flight
- behavior
- validation
- market
- flight test
- proton
- ultralight aircraft
- modeling
- cooling
- assessment
- density
- heat exchanger
- voltage
- cooling system
- committee
- aeronautics
- oxygen
- fluid
- fluid dynamic
- sport
- propeller
- low temperature
- polymer
- fuel cell vehicle
- evaporation
- conduction
- electrolyte
- gas turbine
- jet propelled aircraft
- regional jet
- electric power
- exhaust gas
- plant
- definition
- airplane
- hydrocarbon
- commuter
- re-procurement
- feasibility analysis
- laceration
- electrical system
- air compressor
- commuter aircraft
- show 80 more
Publications (12/12 displayed)
- 2023Potential and technical challenges of on-board hydrogen storage technologies coupled with fuel cell systems for aircraft electrificationcitations
- 2018Making synthetic fuels for the road transportation sector via solid oxide electrolysis and catalytic upgrade using recovered carbon dioxide and residual biomasscitations
- 2017Reporting Degradation from Different Fuel Contaminants in Ni-anode SOFCscitations
- 2015Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft applicationcitations
- 2015Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraftcitations
- 2012Air cooling of a Two-Seater fuel Cell-Powered aircraft: Dynamic modeling and comparison with experimental datacitations
- 2012Air Cooling of a Two-Seater Fuel Cells Powered Aircraft: Dynamic Modelling and Comparisons with Experiemtal Datacitations
- 2011Sensitivity analysis of temperature uncertainty in an aircraft PEM fuel cellcitations
- 2011Hybrid solid oxide fuel cell and micro gas turbine for regional jetscitations
- 2009Analysis of solid oxide fuel cell systems for more-electric aircraftcitations
- 2009Fuel Cells in Aeronautics: Analysis of Solid Oxide Fuel Cell Systems for More-Electric Aircraftscitations
- 2008SOFC-based systems as APU for different aircraft typologies: Feasibility analysis and problems
Places of action
article
Air Cooling of a Two-Seater Fuel Cells Powered Aircraft: Dynamic Modelling and Comparisons with Experiemtal Data
Abstract
The application of fuel cell (FC) technology to aircraft propulsion and/or energy supply is becoming of great interest for undoubted advantages in terms of pollution emissions and noise reduction. A better understanding of problems related to fuel cells applied to aeronautics is sought by the European Commission (EC) funded project Environmentally Friendly Inter-City Aircraft Powered by Fuel Cells (ENFICA-FC). The main objective of the ENFICA-FC project was to develop and validate the use of a fuel cell–based power system for the propulsion of more-electric/all-electric aircraft. The fuel cell system was installed in the light sport aircraft Rapid 200, which was flight and performance tested. One of the key items under investigation is the simulation of the cooling system and the evaluation of fuel cell temperature. The polymer electrolyte membrane fuel cell (PEMFC) is considered to be the best candidate for the fuel cell vehicle because it has high power density, solid membrane electrolyte, and as it operates at low temperatures, it has a fast start-up. However, to generate a reliable and efficient power response and to prevent membrane degradation or damage with hydrogen and oxygen depletion, a sophisticated control technique becomes vitally important. In particular, as the ionic conduction of the polymeric membrane is a function of its degree of humidification, the stack temperature has to be carefully controlled to avoid phenomena of water evaporation, causing an increase of ohmic drop and a decrease of stack performances. The output voltage and hence the power of the fuel cell system is affected considerably by the change of the stack temperature. A simplified fluid-dynamic model has been developed and validated by computational fluid dynamics (CFD) analysis and it is used to compute the air flow to the fuel cell heat-exchanger inlet. Propeller effects are included referring to an optimal propeller specifically designed for the ENFICA-FC project. A mathematical model of the fuel cell system dynamics coupled ...
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