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13 projets européens trouvés

Recherche sur 125080 projets européens

 TERMINÉ 

JEt noise of high bypass RatiO eNgine: Installation, advanced Modelling and mitigatiOn (JERONIMO)

Date du début: 1 nov. 2012, Date de fin: 31 août 2017,

The central goal of JERONIMO is the understanding of the physical mechanisms of ultrahigh bypass ratio (UHBR) engines with a bypass ratio (BPR) larger than 12 and the related installed jet noise with potential jet-wing interaction. The aim is to reduce uncertainties in jet noise characterisation of this novel installation configuration by wind tunnel tests and predictions and being able to derive ...
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 13

 TERMINÉ 

Highly-accurate/reliable WT test demonstration of low-noise innovative MLG configuration (ARTIC)

Date du début: 1 juil. 2014, Date de fin: 31 déc. 2015,

The objective of the activity under this CfP is the test of a full-scale Main Landing Gear fuselage-mounted architecture sized for a high-wing regional aircraft configuration in a Wind Tunnel facility. This proposal considers a complete architecture including all necessary features from an aeroacoustic point of view including: gear struts, wheel pack, bay cavity and doors, fairings and portion of ...
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 3

 TERMINÉ 

Aviation Noise Research Network and Coordination (X-NOISE EV)

Date du début: 1 déc. 2010, Date de fin: 30 nov. 2015,

The X-NOISE EV Coordination Action, through its network structure and comprehensive workplan involving experts groups, scientific workshops, international cooperation seminars and a common information system, addresses the noise challenges faced by Aviation. To this end, it will more specifically:- Evaluate EU-funded projects results and assess their contribution to the state-of-the-art.- Formulat ...
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 28

 TERMINÉ 

Smart Intelligent Aircraft Structures (SARISTU)

Date du début: 1 sept. 2011, Date de fin: 31 août 2015,

The project proposal concerns the challenges posed by the physical integration of smart intelligentstructural concepts. It addresses aircraft weight and operational cost reductions as well as animprovement in the flight profile specific aerodynamic performance.This concerns material concepts enabling a conformal, controlled distortion of aerodynamicallyimportant surfaces, material concepts enablin ...
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 68

 TERMINÉ 

Future Aircraft design following the carrier-pod concept as an enabler for co-modal seamless transport, passenger safety and environmental sustainability (FANTASSY)

Date du début: 1 août 2012, Date de fin: 31 oct. 2014,

Aviation has dramatically transformed society over the past 100 years. Fast and efficient transportation has essentially been “shrinking the planet” and changing the landscape in terms of financial and societal conditions. The growth of air traffic over the past 50 years has been spectacular, and will continue in the future. This anticipated growth carries along challenges and opportunities in va ...
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 4

 TERMINÉ 

OPtimisation for low Environmental Noise impact AIRcraft (OPENAIR)

Date du début: 1 avr. 2009, Date de fin: 30 sept. 2014,

Reducing noise from aircraft operations perceived by airport neighbouring communities is a major challenge facing the aircraft manufacturing industry, social society and the air transport business. By adopting a whole aircraft approach based on the latest developments in active / adaptive technologies, flow control techniques and advances in computational aero-acoustics applied to the major causes ...
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 51

 TERMINÉ 

NOVEL AERONAUTICAL MULTIFUNCTIONAL COMPOSITE STRUCTURES WITH BULK ELECTRICAL CONDUCTIVITY AND SELF-SENSING CAPABILITIES (ELECTRICAL)

Date du début: 1 oct. 2010, Date de fin: 30 juin 2014,

"Aircraft structures appear to be strategic components to be manufactured in composite materials for reducing weight, although new questions regarding electrical conductivity have arisen such as static discharge, electrical bonding and grounding, interference shielding and current return through the structure.These functions can be met by the use of technologies based on nanocomposites, which inde ...
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 14

 TERMINÉ 

INNOVATIVE SMART COMPOSITE MOULDS FOR COST-EFFECTIVE MANUFACTURING OF PLASTIC AND COMPOSITE COMPONENTS (COEUS-TITAN)

Date du début: 1 mars 2011, Date de fin: 28 févr. 2014,

Currently, composite moulds are mainly used in open-mould manufacturing processes and in Light RTM (a low-pressure variation of RTM). The proposed project aims to extend the applicability of composite moulds into the more demanding regime of RTM production, as well as to extend the application of the open mould and light RTM techniques in the field of advanced resin systems, where elevated tempera ...
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 13

 TERMINÉ 

Simulation Based Solutions for Industrial Manufacture of Large Infusion Composite Parts (INFUCOMP)

Date du début: 1 oct. 2009, Date de fin: 30 sept. 2013,

"Today, advanced composites use either layers of plies impregnated with resin (pre-pregs) to form a laminate, or Liquid Composites Moulding (e.g. RTM) of dry textiles. Prepreg composites give superior mechanical properties due to toughened resins and high fibre content, but suffer from high material costs, limited shapeability, complex, expensive and time consuming manufacturing, and limited mater ...
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 15

 TERMINÉ 

Turboshaft Engine Exhaust Noise Identification (TEENI)

Date du début: 1 avr. 2008, Date de fin: 31 mars 2013,

"Helicopters can generate a large amount of external noise, as their traditional missions –rescue, medical, law enforcement– are very close to populated areas. As emphasised in ACARE SRA2, increasing rotorcraft missions in the public vicinity should not lead to increasing public disturbance. Turboshaft engine is known as a major contributor to exterior noise for take-off conditions. ACARE SRA2 ob ...
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 11

 TERMINÉ 

Industrialization of Manufacturing Technologies for Composite Profiles for Aerospace Applications (IMac-Pro)

Date du début: 1 juil. 2008, Date de fin: 31 déc. 2012,

Main aim of the project is the development of a complete, integrated process chain for the cost effective serial production of various aerospace CFRP stiffener profiles. The production is foreseen in the two steps: Preform manufacturing and infiltration / curing. The project will focus on complex profile geometries with variable cross sections, single or multiple curvature and integrated load int ...
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 20

 TERMINÉ 

INNOVATIVE REPAIR OF AEROSPACE STRUCTURES WITH CURING OPTIMIZATION AND LIFE CYCLE MONITORING ABILITIES (IAPETUS)

Date du début: 1 juin 2009, Date de fin: 31 déc. 2012,

"Bonded composite patches are ideal for aircraft structural repair as they offer enhanced specific properties, case-tailored performance and excellent corrosion resistance. Bonding further eliminates stress concentrations induced from mechanical fastening of metal sheets, seals the interface, and reduces the risk of fretting fatigue between the patch and the component. IAPETUS focuses on the use o ...
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 10

 TERMINÉ 

MULTIFUNCTIONAL LAYERS FOR SAFER AIRCRAFT COMPOSITES STRUCTURES (LAYSA)

Date du début: 1 sept. 2008, Date de fin: 31 déc. 2011,

"The use of composite materials in aeronautics industry has increased constantly over the last 35 years, due mainly to their high specific strength and stiffness combined with the possibility of designing complex geometry components that are more aerodynamically efficient than metals. But due to organic nature of polymeric matrix component, composite materials are electrically and thermally bad co ...
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 12