| People | Locations | Statistics |
|---|---|---|
| Ziakopoulos, Apostolos | Athens |
|
| Vigliani, Alessandro | Turin |
|
| Catani, Jacopo | Rome |
|
| Statheros, Thomas | Stevenage |
|
| Utriainen, Roni | Tampere |
|
| Guglieri, Giorgio | Turin |
|
| Martínez Sánchez, Joaquín |
| |
| Tobolar, Jakub |
| |
| Volodarets, M. |
| |
| Piwowar, Piotr |
| |
| Tennoy, Aud | Oslo |
|
| Matos, Ana Rita |
| |
| Cicevic, Svetlana |
| |
| Sommer, Carsten | Kassel |
|
| Liu, Meiqi |
| |
| Pirdavani, Ali | Hasselt |
|
| Niklaß, Malte |
| |
| Lima, Pedro | Braga |
|
| Turunen, Anu W. |
| |
| Antunes, Carlos Henggeler |
| |
| Krasnov, Oleg A. |
| |
| Lopes, Joao P. |
| |
| Turan, Osman |
| |
| Lučanin, Vojkan | Belgrade |
|
| Tanaskovic, Jovan |
|
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
Sensitivity analysis of stack power uncertainty in a PEMFC-based powertrain for aircraft application
Abstract
Experimental data concerning the reliability of fuel cell systems (FCS) in aviation are still unavailable to technical community, while assessing reliability of a component or a whole system represents a fundamental aspect that allows a new technology to be introduced in a high safety system such as an aircraft. The main aim of this paper is to show a method to estimate the reliability of an aircraft power system based on a hydrogen fuel cell, mainly for design purposes. The method is based on a high-order adaptive response surface technique, coupled with a dynamic model of the aircraft power system, and it is applied to the failure event represented by an incorrect power supply due to the failure of sensors of the control system of the powertrain. The most important advantage of the proposed method is the low computational effort it requires. The result is a ranking of the most critical sensors to be considered in the design phase of the power system and demonstrate that accurate temperature sensors and sensor calibration are of dramatic importance for the control of the stack power, in case of powertrain based on PEM fuel cell systems.
Topics
Search in FID move catalog