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Materiales catalizadores de bajo coste para pilas de combustible
El coste total de las pilas de combustible depende principalmente de la cantidad de catalizadores de platino. Un equipo de científicos financiado por la Unión Europea desarrolló materiales nuevos para disminuir la concentración de platino en las pilas de combustible, mejorando su rentabilidad para vehículos eléctricos.
Programme: FP7-JTI
Record Number: 169638
Last updated on: 2017-03-14
Available languages: DE, EN, ES, FR, IT, PL
GNSS-based ATM for Rotorcraft to Decrease Emissions and Noise
ID: 255886
Anfangsdatum: 2009-12-31, Enddatum: 2015-12-30
The GARDEN project - GNSS-based ATM for Rotorcraft to Decrease Emissions and Noise - will support the definition of new flight profiles for rotorcraft to reduce the noise footprint and the gas emissions. Concrete milestones will be implemented to address various types of oper...
Programme: FP7-JTI
Record Number: 98042
Last updated on: 2016-06-06
SONACA Contribution to an Electro-thermal Wing Ice Protection System
ID: 255780
Anfangsdatum: 2010-01-01, Enddatum: 2015-12-31
"The objective of this proposal is to support Liebherr Aerospace in building up an A320 slat equipped with an electro-thermal solution for wing ice protection system. First step will be to define the top level requirements to be mutually agreed with Liebherr and Airbus. This ...
Programme: FP7-JTI
Record Number: 98051
Last updated on: 2015-03-10
LORD Engine Mounting System for the SAGE2 Open-Rotor demonstrator
ID: 338539
Anfangsdatum: 2013-09-01, Enddatum: 2016-12-31
This response to the SAGE-02 call details the proposed approach to an engine mounting system for the open-rotor demonstrator. The goal of the program is to define the requirements of the mounting system, design and develop the system so that it meets the requirements and can ...
Programme: FP7-JTI
Record Number: 185393
Last updated on: 2016-12-19
Advanced Methods for the Prediction of Lean-burn Combustor Unsteady Phenomena
ID: 641453
Anfangsdatum: 2014-12-01, Enddatum: 2016-11-30
The development of lean-burn gas turbine combustors, which will lead to a reduction of emissions from aviation, relies upon resolving significant problems associated with this new technology, namely the emergence of combustion-induced pressure oscillations that can damage the...
Programme: FP7-JTI
Record Number: 192605
Last updated on: 2016-03-10
FAST impact cross-analysis methodology for Composite leading edge Structures
ID: 632420
Anfangsdatum: 2014-11-01, Enddatum: 2016-10-31
"ACS will develop an integrated numerical and test approach for composite wing leading edge hailstone impact application with electrical ice protection system. We propose finite element free fast impact models satisfying the governing equations of impact mechanics coupled wit...
Programme: FP7-JTI
Record Number: 192458
Last updated on: 2015-03-12
Humidity Optimisation Tool
[PROJEKT] HOT - Humidity Optimisation Tool
ID: 632508
Anfangsdatum: 2014-12-01, Enddatum: 2016-11-30
"Humidity Optimisation Tool: Outside humidity treatment is a main contributor to aircraft ECS (environmental control system) power requirements. To reduce this power it is needed to know exactly the not to exceed outlet humidity at the pack outlet. Liquid water at Low Pressur...
Programme: FP7-JTI
Record Number: 192561
Last updated on: 2015-03-12
PySimulator and Modelica Based Collaborative System Design Simulation Analysis Environment for Energy System Applications
ID: 632413
Anfangsdatum: 2014-10-01, Enddatum: 2016-09-30
The PyModSimA project develops new open-source vendor-independent collaborative system design and modeling & simulation tools. This will enable more efficient development processes involving aircraft, engine, and equipment manufacturers, e.g. for application in Green Operatio...
Programme: FP7-JTI
Record Number: 192500
Last updated on: 2016-03-31
Optimizing power density of aircraft inverter by optimized topology and PWM-pattern
ID: 640714
Anfangsdatum: 2014-10-01, Enddatum: 2016-11-30
The project is aimed at an increase of power density (kW per kg) of a three-phase inverter for aerospace application (power range 10 … 50 kW) of at least 10% with a concomitant compliance with RTCA DO-160, chapter 21 CMC limits. The increase in power density will be achieved ...
Programme: FP7-JTI
Record Number: 192277
Last updated on: 2016-03-31
technology development and fabrication of HIgh TEmperature high frequency CApacitors for power switch integration
ID: 641553
Anfangsdatum: 2014-12-01, Enddatum: 2016-11-30
Automotive, aerospace, and energy production industries can greatly benefit from the development of semiconductor based electronics operating at temperature higher than 150 °C. Wide bandgap semiconductors like SiC and GaN are key enablers as these allow electronics to functio...
Programme: FP7-JTI
Record Number: 193065
Last updated on: 2017-03-27
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List retrieved on: 2017-04-23
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