13 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Aerodynamic rigs for VHBR IP turbine (ORBIT)
Date du début: 1 janv. 2017, Date de fin: 31 déc. 2018,
The ORBIT project targets the environmental and competitiveness challenge of the European aeronautics sector, by addressing the topic of experimental validation rig testing to develop aerodynamic technologies for the multi-stage IP turbine of the Very High Bypass Ratio engine (VHBR).The advancement of multi-stage IP Turbine technologies, as an important contributor to the VHBR engine concept, will ...
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1
Participant partenaire
TERMINÉ
Engine Module Validators (ENOVAL)
Date du début: 1 oct. 2013, Date de fin: 30 sept. 2017,
The ENOVAL project will provide the next step of engine technologies to achieve and surpass the ACARE 2020 goals on the way towards Flightpath 2050. ENOVAL completes the European 7th Framework Programme (FP7) roadmap of Level 2 aero engine projects. ENOVAL will focus on the low pressure system of ultra-high by-pass ratio propulsion systems (12 < BPR < 20) in conjunction with ultra high overall pre ...
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37
Participants partenaires
TERMINÉ
Low Emissions Core-Engine Technologies (LEMCOTEC)
Date du début: 1 oct. 2011, Date de fin: 30 juin 2017,
The main objective of the LEMCOTEC project will be the improvement of core-engine thermal efficiency by increasing the overall pressure ratio (OPR) to up to 70 leading to a further reduction of CO2. Since NOx increases with OPR, combustion technologies have to be further developed, at the same time, to at least compensate for this effect. The project will attain and exceed the ACARE targets for 20 ...
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39
Participants partenaires
TERMINÉ
Engine Breakthrough Components and Subsystems (E-BREAK)
Date du début: 1 oct. 2012, Date de fin: 31 mars 2017,
Future aero engines will need to be more efficient and contribute to the reduction on environmental impact of air transportation. They must reach some standards of performance by reducing emissions and creating some savings on operation costs.EIMG consortium has launched since several years some initiatives to develop future engines in the frame of the European Committee research programmes.Within ...
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48
Participants partenaires
TERMINÉ
WING STRUCTURAL TEST DEVELOPMENT METHOD (WISDOM)
Date du début: 14 janv. 2013, Date de fin: 13 déc. 2016,
The proposal approach innovative solutions for the design and manufacturing of the test rig and the definition of the method and prformance for the structural testing of two different kinds of configuration for the outer wings within a Smart Fixed Wing Aircraft.The WISDOM proposal, understand that the test philosophy is to demonstrate that major components tests can be performed on flight test air ...
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3
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TERMINÉ
Global in flight health monitoring platform for composite aerostructures based on advanced VIBRATION based methods (VIBRATION)
Date du début: 1 mai 2013, Date de fin: 31 oct. 2016,
"In order to reduce the sensor number, one has to be based on signals carrying information about the “global” structure state. The structure’s vibrational behavior is definitely a global characteristic. The idea is thus the development of a vibration based, in flight, SHM platform, which can be applied in aircraft structures in practice.The main practical problem for the application of vibration b ...
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7
Participants partenaires
TERMINÉ
Development of Electric Smart Actuator for gas turbine engines (E-SEMA)
Date du début: 1 avr. 2012, Date de fin: 31 oct. 2014,
"The E-SEMA project will design, manufacture and test an innovative concept of light, reliable and smart electrical actuator for an inlet guide vane or stator vane application of gas turbine engines that will be capable of interfacing and connecting to the engine control unit in a plug-and-play manner. This innovative concept of smart electrical actuator will be based on a multi-disciplinary appro ...
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6
Participants partenaires
TERMINÉ
Development and Optimization of THz NDT on Aeronautics Composite Multi-layered Structure (DOTNAC)
Date du début: 1 sept. 2010, Date de fin: 31 août 2013,
"Modern aircraft structures have to comply with severe requirements: they have to be light as well as safe. These requirements lead to an increased use of composite materials in the aircraft industry. However, new materials also require new techniques in order to inspect aircraft components during production in a non-destructive way.The primary goal of the DOTNAC project is to develop a safe, con ...
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10
Participants partenaires
TERMINÉ
Development of high power density electrical actuators (HP-SMART EMA)
Date du début: 1 janv. 2010, Date de fin: 30 juin 2013,
"The HP-SMART-EMA project will develop and test an innovative concept of extremely light, reliable and smart electrical actuator for control systems of turbine engines that will be capable of interfacing and connecting to the engine / turbine control unit in a plug-and-play manner. This innovative concept of smart electrical actuators will be based on a multi-disciplinary approach that will consid ...
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6
Participants partenaires
TERMINÉ
Flutter-Free Turbomachinery Blades (FUTURE)
Date du début: 1 juil. 2008, Date de fin: 30 juin 2013,
"FUTURE brings together European and international well reputed centres-of-excellence in order to reach major scientific & technical objectives in striving towards flutter-free turbomachine blades. By advancing the state-of-the-art in flutter prediction capabilities and design rules, the FUTURE project will lead to benefits in terms of decreased development cost, reduced weight and fuel consumptio ...
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26
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TERMINÉ
Full-field Advanced Non Destructive Technique for On-line Thermo-Mechanical Measurements on Aeronautical Structures (FANTOM)
Date du début: 1 déc. 2008, Date de fin: 31 mai 2012,
"The increasing use of composites, sandwich and lightweight structures and parts in new airplanes leads to a need of adapted Non Destructive Testing techniques for such new materials. Various NDT techniques are currently used for flaw detection or mechanical characterization during the development of aerostructures. There is a constant need for improved inspection methods; with increased reliabili ...
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6
Participants partenaires
TERMINÉ
valiDation of Radical Engine Architecture systeMs (DREAM)
Date du début: 1 févr. 2008, Date de fin: 31 janv. 2012,
"Since the publication of the ACARE goals, the commercial and political pressure to reduce CO2 has increased considerably. DREAM is the response of the aero-engine community to this pressure. The first major DREAM objective is to design, integrate and validate new engine concepts based on open rotor contra-rotating architectures to reduce fuel consumption and CO2 emissions 7% beyond the ACARE 2020 ...
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46
Participants partenaires
TERMINÉ
AIRCRAFT INTEGRATED STRUCTURAL HEALTH ASSESSMENT II (AISHA II)
Date du début: 1 mai 2008, Date de fin: 31 oct. 2011,
"The safe use of complex engineering structures such as aircrafts can only be guaranteed when efficient means of damage assessment are in place. Whereas the design of civil structures is nowadays based on a damage tolerance approach and time based inspection cycles, it is envisaged that the large cost associated with this approach can be drastically reduced by switching to a condition based mainte ...
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