7 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Gust Load Alleviation techniques assessment on wind tUnnel MOdel of advanced Regional aircraft (GLAMOUR)
Date du début: 1 févr. 2014, Date de fin: 30 sept. 2016,
The aim of Gust Load Alleviation techcniques assessment on wind tUnnel MOdel of advanced Regional aircraft (GLAMOUR) proposal is a technological optimisation and experimental validation through an aero-servo-elastic innovative WT model of gust load alleviation control systems for advanced Green Regional Aircraft. The expected benefits of such technologies are mainly the mitigation of gust load res ...
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5
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TERMINÉ
Experimental Acoustic Subsonic wind tunnel Investigation of the advanced geared turbofan Regional aircraft integrating HLD innovative low-noise design (EASIER)
Date du début: 1 juin 2014, Date de fin: 31 oct. 2015,
EASIER adresses the CfP JTI_CS_2013-2-GRA-05-008 and proposes a way to perform acoustic tests on a WT-model which was designed and manufactured in a previous CfP.The current project is proposed by a small consortium combining the necessary competence for this project:- IBK is a small company coordinating the project and performing design work in the project. IBK is also leading the consortium buil ...
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4
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TERMINÉ
LOw Subsonic Investigationof a largecomplete Turboprop Aircraft (LOSITA)
Date du début: 1 oct. 2013, Date de fin: 30 sept. 2015,
The project tackles the design, manufacturing and testing of an advanced turob-prop 90-seat regional aircraft complete powered model. The model will be tested in a Wind-Tunnel with the aim of evaluation the performance of the high-.lift devices in different configurations.Major work-packages therefore are the design and manufacturing of the model, the design and manufacturing of a engine demonstra ...
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4
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TERMINÉ
WindTunnel Tests on an Innovative regional A/C for Noise assessment (WITTINESS)
Date du début: 1 oct. 2014, Date de fin: 30 sept. 2015,
WITTINESS adresses the acoustic measurement campaign of previously (in a different CfP) designed WT-model, equipped with engine-demonstrators. In order to tackle this project a consortium including a company experienced in design, structural mechanics and aerodynamics, a SME, a manufacturer and a university with a strong focus on acoustic measurements propose an approach to use the previously desi ...
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4
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TERMINÉ
Experimental Subsonic Investigation of a Complete Aircraft Propulsion system Installation and Architecture power plant optimization (ESICAPIA)
Date du début: 1 juin 2013, Date de fin: 31 mai 2015,
The proposed project tackles a CfP from the JTI-GRA ITD. Is focuses on the experimental optimization of a regional aircraft configuration and a subsequent optimization of take-off/ landing configuration. The regional aircraft has a wing designed for natural laminar flow, fuselage-mounted engines and a T-tail. Open configurational questions that are addressed tackle wing-tip devices and their perfo ...
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5
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TERMINÉ
Active Flow Control Technique on Trailing Edge Shroud for Improved High Lift Configurations (ATTESI)
Date du début: 1 juin 2011, Date de fin: 28 févr. 2014,
"The subject of the proposed project ATTESI is the design and evaluation of flow control techniques to improve the separation behavior on a drooped spoiler configuration.The proposed project comprehends numerical evaluation and optimization of the spoiler droop together with different flow control approaches applied upstream of the kink (the effect of the droop) and at the trailing edge of the spo ...
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4
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TERMINÉ
Structural design of a counter-rotating open rotor (DECROR)
Date du début: 1 janv. 2010, Date de fin: 30 juin 2011,
"In this project two fe-models for counter-rotating open rotors made from composites are needed. Before generating these models a structural design is necessary. IBK is a SME with a long tradition in both structural mechanics and aerodynamics. Consequently our customers come from areas where both parts of our knowledge are needed, which is among the aviation industry the turbine industry. IBK can ...
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