Aernnova Engineering Solutions
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DESIGN DEPARTMENT- Leonardo Da Vinci, 13
Miñano - Alava
Spain
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Novel innovative competitive effective tilt rotor integrated project
NICE-TRIP Subjects :
Innovation, Technology Transfer, Information Processing, Information Systems, Telecommunications, Social Aspects, Standards, Electronics, Microelectronics, Aerospace Technology, Safety, Economic Aspects, Policies, Evaluation
Contract type :
Integrated Project
Participants :
VERTAIR BELGIQUE-BELGIË
VERTAIR
TECHNICAL DIRECTORATE Gulledelle 94 BELGIQUE-BELGIË
SAMTECH S.A. BELGIQUE-BELGIË
SAMTECH S.A.
R & D DEPARTMENT Rue des Chasseurs-Ardennais 8 BELGIQUE-BELGIË
N.A. AFGHANISTAN
N.A.
AFGHANISTAN
UNIVERSITY OF LIEGE, BELGIUM BELGIQUE-BELGIË
UNIVERSITY OF LIEGE, BELGIUM
AEROSPACE AND MECHANICAL ENGINEERING DEPARTMENT (LTAS) - WIND TUNNEL LABORATORY Place du 20 Aout, 7 BELGIQUE-BELGIË
AERNNOVA ENGINEERING SOLUTIONS ESPAÑA
AERNNOVA ENGINEERING SOLUTIONS
DESIGN DEPARTMENT- Leonardo Da Vinci, 13 ESPAÑA
CENTRE DE RECHERCHE EN AÉRONAUTIQUE, ASBL BELGIQUE-BELGIË
CENTRE DE RECHERCHE EN AÉRONAUTIQUE, ASBL
OPTIMISATION GROUP - CENAERO Bâtiment Mermoz 1, 2ème étage - Avenue Jean Mermoz 30 BELGIQUE-BELGIË
SENER INGENIERIA Y SISTEMAS ESPAÑA
SENER INGENIERIA Y SISTEMAS
STRUCTURE AND MECHANISMS DEPARTMENT Avenida Zugazarte 56 ESPAÑA
ZF LUFTFAHRTTECHNIK GMBH DEUTSCHLAND
ZF LUFTFAHRTTECHNIK GMBH
PRODUCTS/TRANSMISSION DESIGN, LX Flugplatzstrasse DEUTSCHLAND
CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA ITALIA
CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA
MANAGEMENT OF VTOL PROGRAMMES (PMAE) Via Maiorise s.n.c. ITALIA
FUNDACION CENTRO DE TECNOLOGIAS AERONAUTICAS ESPAÑA
FUNDACION CENTRO DE TECNOLOGIAS AERONAUTICAS
CTA MINANO C/ Juan De La Cierva, 1 ESPAÑA
DEUTSCHES FORSCHUNGSZENTRUM FÜR LUFT- UND RAUMFAHRT E.V. DEUTSCHLAND
DEUTSCHES FORSCHUNGSZENTRUM FÜR LUFT- UND RAUMFAHRT E.V.
INSTITUTE FOR FLIGHT RESEARCH Linder Höhe DEUTSCHLAND
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM NEDERLAND
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM
DIVISION AEROSPACE VEHICLES / DEPARTMENT HELICOPTERS AND AEROACOUSTICS PO Box 90502 Anthony Fokkerweg 2, 1059 CM NEDERLAND
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AÉROSPATIALES FRANCE
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AÉROSPATIALES
DELEGATE DIRECTOR FOR ROTORCRAFT PROGRAM (DCV/H) 29, avenue de la Division Leclerc FRANCE
CONSORZIO SICTA - SISTEMI INNOVATIVI PER IL CONTROLLO DEL TRAFFICO AEREO ITALIA
CONSORZIO SICTA - SISTEMI INNOVATIVI PER IL CONTROLLO DEL TRAFFICO AEREO
ENGINEERING DEPARTMENT Via Fulco Ruffo di Calabria c/o Aeroporto di Capodichino ITALIA
POLITECNICO DI MILANO ITALIA
POLITECNICO DI MILANO
DIPARTIMENTO DI INGEGNERIA AEROSPAZIALE Piazza Leonardo da Vinci, 32 ITALIA
THE UNIVERSITY OF LIVERPOOL UNITED KINGDOM
THE UNIVERSITY OF LIVERPOOL
DEPARTMENT OF ENGINEERING, FLIGHT SCIENCE AND TECHNOLOGY The Foundation Building, 765 Brownlow Hill UNITED KINGDOM
UNIVERSITAET STUTTGART DEUTSCHLAND
UNIVERSITAET STUTTGART
ABTEILUNG GANZHEITLICHE BILANZIERUNG, GABI Keplerstrasse 7 DEUTSCHLAND
POLITCHNIKA WARSZAWSKA (WARSAW UNIVERSITY OF TECHNOLOGY) POLSKA
POLITCHNIKA WARSZAWSKA (WARSAW UNIVERSITY OF TECHNOLOGY)
DEPARTMENT OF AUTOMATION AND AERONAUTICAL SYSTEMS, INSTITUTE OF AERONAUTICS AND APPLIED MECHANICS, FACULTY OF POWER AND AERONAUTICAL ENGINEERING Pl. Politechniki 1 POLSKA
LIEBHERR-AEROSPACE LINDENBERG GMBH DEUTSCHLAND
LIEBHERR-AEROSPACE LINDENBERG GMBH
Postfach 1363 Pfaenderstrasse 50-52 DEUTSCHLAND
RIGA SCIENTIFIC EXPERIMENTAL CENTRE "AVIATEST LNK" LATVIJA
RIGA SCIENTIFIC EXPERIMENTAL CENTRE "AVIATEST LNK"
Rezeknes Str. 1 LATVIJA
CASTILLA Y LEON AERONAUTICA S.A. ESPAÑA
CASTILLA Y LEON AERONAUTICA S.A.
R&D DEPARTMENT Pol. Industrial de Bayas C/Oron P.4 ESPAÑA
EUROCOPTER DEUTSCHLAND GMBH DEUTSCHLAND
EUROCOPTER DEUTSCHLAND GMBH
RESEARCH PROGRAMMES (OTRM/O) Postfach 81663 Willy-Messerschmitt-Str., Tor 1 DEUTSCHLAND
Samtech Belgium
Samtech
PO Box 8 Boulevard Frere Orban 25 4000 Belgium
PAULSTRA SNC France
PAULSTRA SNC
PAULSTRA-VIBRACHOC RUE MARIUS AUFAN, 61 France
EUROCOPTER DEUTSCHLAND Germany
EUROCOPTER DEUTSCHLAND
AERODYNAMICS AND FLIGHT MECHANICS Postfach Willy Messerschmitt Str. 1 Germany
Liebherr Aerospace Lindenberg Germany
Liebherr Aerospace Lindenberg
Pfänderstrasse 50-52 D- Germany
ZF LUFTFAHRTTECHNIK Germany
ZF LUFTFAHRTTECHNIK
RESEARCH AND DEVELOPMENT LE Flugplatzstrasse Germany
AERNNOVA ENGINEERING SOLUTIONS Spain
AERNNOVA ENGINEERING SOLUTIONS
DESIGN DEPARTMENT- Leonardo Da Vinci, 13 Spain
CASTILLA Y LEON AERONAUTICA Spain
CASTILLA Y LEON AERONAUTICA
R&D DEPARTMENT Pol. Industrial de Bayas C/Oron P.4 Spain
SENER Inginieria y Sistemas Spain
SENER Inginieria y Sistemas
Av Zugazarte 56 Spain
AGUSTA Italy
AGUSTA
Via G. Augusta, 520 Italy
MECAER MECCANICA AERONAUTICA Italy
MECAER MECCANICA AERONAUTICA
TECNICAL DEPARTEMENT Via per Arona, 46 Italy
SECONDO MONA Italy
SECONDO MONA
TECHNOLOGY RESEARCH DEPARTMENT Via Carlo Del Prete 1 Italy
SELEX GALILEO Italy
SELEX GALILEO
GA ENGINEERING IMPIANTI E UTILITIES Via Albert Einstein 35 Italy
SISTEMI DINAMICI Italy
SISTEMI DINAMICI
Via Livornese 1019 Italy
WESTLAND HELICOPTERS United Kingdom
WESTLAND HELICOPTERS
ROTOR AERODYNAMICS, ROTOR SYSTEMS Lysander Road United Kingdom
This proposal has been prepared in the framework of a research and development roadmap defined by the European rotorcraft community that aims to develop a civil tilt-rotor aircraft. A key target of the road map is a flying demonstrator in the 2010 decade. NICETRIP specifically addresses the acquisition of new knowledge and technology validation concerning tilt-rotor.The main project objectives are:- To validate the European civil tilt-rotor concept based on the ERICA architecture;- To validate critical technologies and systems through the development, integration and testing of components of a tilt-rotor aircraft on full-scale dedicated rigs;- To acquire new knowledge on tilt-rotor through the development and testing of several wind tunnel models, including a large-scale full-span powered model;- To investigate and evaluate the introduction of tilt-rotors in the European Air Traffic Management System;- To assess the sustainability of the tilt-rotor product with respect to social and environmental issue s and to define the path towards a future tilt-rotor flying demonstrator.Project NICETRIP is fully relevant to the strategic objective 1.3.2.1: - Integration of technologies towards the future tilt-rotor aircraft, of the work programme of call 3 of the Thematic Priority Aeronautics and Space. The organisation and resources proposed to achieve the project objectives include a 54-month work plan made of 7 work packages and a consortium of 31 participants, fully representing the span of needed capabilities.
Source :
cordis
Cost Effective Small AiRcraft
CESAR Subjects :
Standards, Information Processing, Information Systems, Social Aspects, Electronics, Microelectronics, Evaluation, Safety, Economic Aspects, Innovation, Technology Transfer, Aerospace Technology, Policies, Telecommunications
Contract type :
Integrated Project
Participants :
VYZKUMNY A ZKUSEBNI LETECKY USTAV, A.S. CESKA REPUBLIKA
VYZKUMNY A ZKUSEBNI LETECKY USTAV, A.S.
INTERNATIONAL COOPERATION / VZLU Beranovych 130 CESKA REPUBLIKA
C.I.R.A. - CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA ITALIA
C.I.R.A. - CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA
MODELLING AND DESIGN METHODS CAPUA (CE) ITALIA
VR GROUP, A.S. CESKA REPUBLIKA
VR GROUP, A.S.
VR GROUP, A.S., OFFICE BRNO Touzimská 583 CESKA REPUBLIKA
PRVNI BRNENSKA STROJIRNA VELKA BITES, A.S. CESKA REPUBLIKA
PRVNI BRNENSKA STROJIRNA VELKA BITES, A.S.
PROJECTS AND DEVELOPMENT DEPARTMENT AIRCRAFT TECHNIQUE DIVISION Vlkovska 279 CESKA REPUBLIKA
BRNO UNIVERSITY OF TECHNOLOGY CESKA REPUBLIKA
BRNO UNIVERSITY OF TECHNOLOGY
FACULTY OF MECHANICAL ENGINEERING, INSTITUTE OF AEROSPACE ENGINEERIG Antoninska 548/1 CESKA REPUBLIKA
INSTYTUT LOTNICTWA - INSTITUTE OF AVIATION POLSKA
INSTYTUT LOTNICTWA - INSTITUTE OF AVIATION
AERODYNAMIC DEPARTMENT AIRCRAFT DESIGN DEPARTMENT n/a Al. Krakowska 110/114 POLSKA
THE UNIVERSITY OF MANCHESTER UNITED KINGDOM
THE UNIVERSITY OF MANCHESTER
SCHOOL OF ELECTRICAL AND ELECTRONIC ENGINEERING Oxford Road UNITED KINGDOM
AIT- AUSTRIAN INSTITUTE OF TECHNOLOGY GMBH ÖSTERREICH
AIT- AUSTRIAN INSTITUTE OF TECHNOLOGY GMBH
ADVANCED MATERIALS AND AEROSPACE TECHNOLOGIES - AMAT Donau-City-Strasse 1 ÖSTERREICH
EADS DEUTSCHLAND GMBH DEUTSCHLAND
EADS DEUTSCHLAND GMBH
CORPORATE RESEARCH CENTRE GERMANY DEPARTMENT SC/IRT/LG-PM Willy-Messerschmitt-Straße DEUTSCHLAND
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM NEDERLAND
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM
AEROSPACE VEHICLES DIVISION / STRUCTURES TECHNOLOGY DEPARTMENT AEROSPACE VEHICLES DIVISION / STRUCTURES TECHNOLOGY DEPARTMENT PO Box 90502 Anthony Fokkerweg 2, 1059 CM NEDERLAND
SWEDISH DEFENCE RESEARCH AGENCY SVERIGE
SWEDISH DEFENCE RESEARCH AGENCY
DEPARTMENT OF COMPUTATIONAL PHYSICS Gullfossgatan 6 SVERIGE
SVENSKA ROTOR MASKINER AB SVERIGE
SVENSKA ROTOR MASKINER AB
SVENSKA ROTOR MASKINER Box 15 085 Box 15 085 SVERIGE
INSTITUTUL NATIONAL DE CERCETARI AEROSPATIALE "ELIE CARAFOLI" ROMANIA
INSTITUTUL NATIONAL DE CERCETARI AEROSPATIALE "ELIE CARAFOLI"
INCAS - SUBSONIC WIND TUNNEL PO Box 77538 Iuliu Maniu 220 ROMANIA
JIHOSTROJ A.S. CESKA REPUBLIKA
JIHOSTROJ A.S.
R&D DEPARTMENT OF AERO TECHNOLOGY DIVISION Budejovicka 148 CESKA REPUBLIKA
CENTRE DE RECHERCHE EN AÉRONAUTIQUE, ASBL BELGIQUE-BELGIË
CENTRE DE RECHERCHE EN AÉRONAUTIQUE, ASBL
OPTIMISATION GROUP - CENAERO Bâtiment Mermoz 1, 2ème étage - Avenue Jean Mermoz 30 BELGIQUE-BELGIË
DEUTSCHES ZENTRUM FÜR LUFT- UND RAUMFAHRT E.V. DEUTSCHLAND
DEUTSCHES ZENTRUM FÜR LUFT- UND RAUMFAHRT E.V.
INSTITUT FÜR AERODYNAMIK UND STRÖMUNGSTECHNIK Linder Hoehe DEUTSCHLAND
SPEEL PRAHA, LTD. CESKA REPUBLIKA
SPEEL PRAHA, LTD.
SPEEL'S R&D DEPARTMENT Beranovych 130 CESKA REPUBLIKA
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AÉROSPATIALES' FRANCE
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AÉROSPATIALES'
APPLIED AERODYNAMICS DEPARTMENT (DAAP) BP 72 29, avenue de la Division Leclerc FRANCE
UNIVERSITY OF PATRAS HELLAS
UNIVERSITY OF PATRAS
LABORATORY FOR MANUFACTURING SYSTEMS AND AUTOMATION-DEPARTMENT OF MECHANICAL ENGINEERING AND AERONAUTICS Patras University Campus HELLAS
TECHNISCHE UNIVERSITÄT MÜNCHEN DEUTSCHLAND
TECHNISCHE UNIVERSITÄT MÜNCHEN
INSTITUTE FOR ENERGY SYSTEMS Arcisstr. 21 DEUTSCHLAND
SWEREA SICOMP AB SVERIGE
SWEREA SICOMP AB
SICOMP AB PO Box 271 Fibervägen 2 SVERIGE
RHEINISCH-WESTFÄLISCHE TECHNISCHE HOCHSCHULE AACHEN (RWTH) DEUTSCHLAND
RHEINISCH-WESTFÄLISCHE TECHNISCHE HOCHSCHULE AACHEN (RWTH)
CHAIR OF FLIGHT DYNAMICS AND INSTITUTE OF AEROSPACE ENGINEERING Templergraben 55 DEUTSCHLAND
MESIT PRISTROJE SPOL. S R.O. CESKA REPUBLIKA
MESIT PRISTROJE SPOL. S R.O.
TECHNICAL DEPARTMENT OF MESIT PRISTROJE SPOL. S R.O. Sokolovska 573 CESKA REPUBLIKA
JIHLAVAN, A.S. CESKA REPUBLIKA
JIHLAVAN, A.S.
DESIGN AND TESTING DEPARTMENT Znojemská 64 CESKA REPUBLIKA
AERNNOVA ENGINEERING SOLUTIONS, S.A. ESPAÑA
AERNNOVA ENGINEERING SOLUTIONS, S.A.
R&D DEPARTMENT P.T.Alava C/ Leonardo Da Vinci, 13 ESPAÑA
UNIS, A.S. CESKA REPUBLIKA
UNIS, A.S.
MECHATRONIC SYSTEM DEPARTMENT Jundrovska 33 CESKA REPUBLIKA
UNIVERSITÉ DE LIEGE BELGIQUE-BELGIË
UNIVERSITÉ DE LIEGE
FACULTY OF APPLIED SCIENCES DEPARTMENT OF AEROSPACE AND MECHANICAL ENGINEERING TURBOMACHINERY GROUP Place du XX Aout, 7 BELGIQUE-BELGIË
POLSKIE ZAKLADY LOTNICZE SP. Z O.O. POLSKA
POLSKIE ZAKLADY LOTNICZE SP. Z O.O.
DESIGN ORGANISATION PRODUCTION ORGANISATION Wojska Polskiego 3 POLSKA
HELLENIC AEROSPACE INDUSTRY S.A. HELLAS
HELLENIC AEROSPACE INDUSTRY S.A.
RESEARCH & PRODUCT DESIGN HELLENIC AEROSPACE INDUSTRY, PO BOX 23, 32009 SCHIMATARI, GREECE HELLAS
EVEKTOR SPOL. S R.O. CESKA REPUBLIKA
EVEKTOR SPOL. S R.O.
EVEKTOR Letecka 1008 CESKA REPUBLIKA
AERO VODOCHODY A.S. CESKA REPUBLIKA
AERO VODOCHODY A.S.
DTTO U Letiste 374, Dolinek CESKA REPUBLIKA
SE "IVCHENKO PROGRESS" Ukraine
SE "IVCHENKO PROGRESS"
SCIENTIFIC-RESEARCH DEPARTMENT 2, Ivanova Street Ukraine
AERO VODOCHODY Czech Republic
AERO VODOCHODY
DTTO U Letiste 374, Dolinek Czech Republic
EVEKTOR SPOL Czech Republic
EVEKTOR SPOL
EVEKTOR Letecka 1008 Czech Republic
JIHLAVAN Czech Republic
JIHLAVAN
DESIGN AND TESTING DEPARTMENT Znojemská 64 Czech Republic
JIHOSTROJ Czech Republic
JIHOSTROJ
R&D DEPARTMENT OF AERO TECHNOLOGY DIVISION Budejovicka 148 Czech Republic
MESIT PRISTROJE SPOL Czech Republic
MESIT PRISTROJE SPOL
TECHNICAL DEPARTMENT OF MESIT PRISTROJE SPOL. S R.O. Sokolovska 573 Czech Republic
PRVNI BRNENSKA STROJIRNA VELKA BITES Czech Republic
PRVNI BRNENSKA STROJIRNA VELKA BITES
AIRCRAFT TECHNIQUE DIVISION Vlkovska 279 Czech Republic
SPEEL PRAHA Czech Republic
SPEEL PRAHA
SPEEL'S R&D DEPARTMENT Beranovych 130 Czech Republic
UNIS Czech Republic
UNIS
MECHATRONIC SYSTEM DEPARTMENT Jundrovska 33 Czech Republic
VR GROUP Czech Republic
VR GROUP
VR GROUP, A.S., OFFICE BRNO Touzimská 583 Czech Republic
POLSKIE ZAKLADY LOTNICZE SP Z OO Poland
POLSKIE ZAKLADY LOTNICZE SP Z OO
DESIGN ORGANISATION PRODUCTION ORGANISATION Wojska Polskiego 3 Poland
Eurocopter France France
Eurocopter France
RESEARCH PROGRAMME Aeroport International Marseille France
Liebherr Aerospace Toulouse France
Liebherr Aerospace Toulouse
Engineering and Programs Department Avenue des Etats Unis 31016 France
SOCATAS France
SOCATAS
GENERAL AIRCRAFT DIVISION Aéroport Tarbes Lourdes Pyrénées France
TECHNOFAN France
TECHNOFAN
RESEARCH & DEVELOPMENT BP 30053 10 place Marcel Dassault France
HELLENIC AEROSPACE INDUSTRY Greece
HELLENIC AEROSPACE INDUSTRY
ENGINEERING DEPARTMENT ELECTRONICS BUSINESS UNIT TANAGRA Greece
EADS DEUTSCHLAND Germany
EADS DEUTSCHLAND
Postfach Willy-Messerschmitt-Strasse Germany
SVENSKA ROTOR MASKINER Sweden
SVENSKA ROTOR MASKINER
SVENSKA ROTOR MASKINER Box 15 085 Box 15 085 Sweden
AERNNOVA ENGINEERING SOLUTIONS Spain
AERNNOVA ENGINEERING SOLUTIONS
DESIGN DEPARTMENT- Leonardo Da Vinci, 13 Spain
PIAGGIO AERO INDUSTRIES Italy
PIAGGIO AERO INDUSTRIES
PIAGGIO HIGH TECHNOLOGY - FLIGHT TECHNOLOGY Viale Castro Pretorio 116 Italy
MATERIALS ENGINEERING RESEARCH LABORATORY United Kingdom
MATERIALS ENGINEERING RESEARCH LABORATORY
MATERIALS ENGINEERING RESEARCH LABORATORY 89/91 Tamworth Road United Kingdom
TURBOMECA France
TURBOMECA
France
CESAR focuses on small-size commercial aircraft providing manufacturers with an enhanced ability needed to become fully competitive in the world market. The objective is to build up a new development concept for this aircraft category and to improve selected technologies enabling a significant reduction of the time-to-market and lowering the overall development, operation and maintenance costs, while considering safety, passenger comfort and environmental impact. The project consists of five RTD areas sufficiently covering the complexity of the aircraft design process, namely aerodynamic and structural design, propulsion integration, aircraft system optimisation and design integration aspects. In particular CESAR aims at enhancing aerodynamic and structural design tools and structural evaluation methods. RTD work comprises development, validation and integration of design tools and methodologies to provide suitable environment for virtual aircraft simulation. Enhancement of design processes, knowledge management and collaboration tools is an essential part of the project. Another important part of the project is technological development for aircraft subparts and systems. The CESAR aspires to provide technologies and knowledge for advanced wing, competitive and environmentally acceptable propulsion unit and new technologies for selected aircraft systems to reduce aircraft operating costs and improve safety. The activities also include the integration of the latest technologies already applied to large commercial aircraft and their modified economical use within the category of small-size commercial aircraft, e.g. cost effective actuation, complex power-plant control system, competitive technologies for air systems, structural health monitoring and on condition maintenance systems. Validation is carried out on two levels: a) on the task level (hardware platforms), b) on the project level (two baseline a/c configurations for assessment and trade offs).
Source :
cordis
Improved material exploitation at safe design of composite airframe structures by accurate simulation of collapse
COCOMAT Subjects :
Aerospace Technology
Contract type :
Specific Targeted Research Project
Participants :
DEUTSCHES ZENTRUM FÜR LUFT UND RAUMFAHRT E.V. DEUTSCHLAND
DEUTSCHES ZENTRUM FÜR LUFT UND RAUMFAHRT E.V.
INSTITUTE OF STRUCTURAL MECHANICS Linder Höhe DEUTSCHLAND
TECHNION - ISRAEL INSTITUTE OF TECHNOLOGY ISRAEL
TECHNION - ISRAEL INSTITUTE OF TECHNOLOGY
FACULTY OF AEROSPACE ENGINEERING Technion City ISRAEL
RHEINISCH-WESTFAELISCHE TECHNISCHE HOCHSCHULE AACHEN DEUTSCHLAND
RHEINISCH-WESTFAELISCHE TECHNISCHE HOCHSCHULE AACHEN
INSTITUT FUER LEICHTBAU Templergraben 55 DEUTSCHLAND
SMR SA SCHWEIZ/SUISSE/SVIZZERA
SMR SA
SMR SA PO Box 4014 Rue Dufour 109b SCHWEIZ/SUISSE/SVIZZERA
SAMTECH S.A. BELGIQUE-BELGIË
SAMTECH S.A.
R & D DEPARTMENT Rue des Chasseurs-Ardennais 8 BELGIQUE-BELGIË
RIGA TECHNICAL UNIVERSITY LATVIJA
RIGA TECHNICAL UNIVERSITY
INSTITUTE OF MATERIALS AND STRUCTURES Kalku iela 1 LATVIJA
POLITECNICO DI MILANO ITALIA
POLITECNICO DI MILANO
DIPARTIMENTO DI INGEGNERIA AEROSPAZIALE Piazza Leonardo da Vinci, 32 ITALIA
AGUSTA S.P.A. ITALIA
AGUSTA S.P.A.
STRUCTURE, CONTROLS AND UNDERCARRIAGE DESIGN GROUP OF HELICOPTER SYSTEM DESIGN DEPT. Via G. Agusta, 520 ITALIA
SWEDISH DEFENCE RESEARCH AGENCY SVERIGE
SWEDISH DEFENCE RESEARCH AGENCY
AERONAUTICS DIVISION, FFA SVERIGE
AERNNOVA ENGINEERING SOLUTIONS SA ESPAÑA
AERNNOVA ENGINEERING SOLUTIONS SA
OFICINA DE VITORIA Parque Tecnologico de Alava C/Leonardo da Vinci, 13 ESPAÑA
HELLENIC AEROSPACE INDUSTRY S.A. HELLAS
HELLENIC AEROSPACE INDUSTRY S.A.
RESEARCH & DEVELOPMENT DEPARTMENT HELLENIC AEROSPACE INDUSTRY, PO Box 23 HELLAS
WYTWORNIA SPRZETU KOMUNIKACYJNEGO PZL-SWIDNIK S.A. POLSKA
WYTWORNIA SPRZETU KOMUNIKACYJNEGO PZL-SWIDNIK S.A.
RESEARCH AND DEVELOPMENT CENTRE Al. Lotnikow Polskich 1 POLSKA
ADVANCED COMPOSITE STRUCTURES LIMITED AUSTRALIA
ADVANCED COMPOSITE STRUCTURES LIMITED
COOPERATIVE RESEARCH CENTRE FOR ADVENCED COMPOSITE STRUCTURES LIMITED 506 Lorimer Street AUSTRALIA
INSTITUT FUER BAUSTATIK, UNIVERSITAET KARLSRUHE DEUTSCHLAND
INSTITUT FUER BAUSTATIK, UNIVERSITAET KARLSRUHE
INSTITUT FÜR BAUSTATIK, UNIVERSITAET KARLSRUHE Postfach 6980 Kaiserstrasse 12 DEUTSCHLAND
Samtech Belgium
Samtech
PO Box 8 Boulevard Frere Orban 25 4000 Belgium
HELLENIC AEROSPACE INDUSTRY Greece
HELLENIC AEROSPACE INDUSTRY
ENGINEERING DEPARTMENT ELECTRONICS BUSINESS UNIT TANAGRA Greece
ISRAEL AIRCRAFT INDUSTRIES Israel
ISRAEL AIRCRAFT INDUSTRIES
ENGINEERING DIVISION PRELIMINARY DESIGN DEPARTMENT Ben Gurion International Airport Israel
SMR Switzerland
SMR
SMR SA PO Box Rue Dufour 109b Switzerland
AERNNOVA ENGINEERING SOLUTIONS Spain
AERNNOVA ENGINEERING SOLUTIONS
DESIGN DEPARTMENT- Leonardo Da Vinci, 13 Spain
European aircraft industry demands for reduced development and operating costs, by 20% and 50% in the short and long term, respectively. COCOMAT contributes to this aim by reducing structural weight at safe design; it exploits considerable reserves in primary fibre composite fuselage structures by accurate and reliable simulation of collapse. Collapse is specified by that point of the load-displacement-curve where a sharp decrease occurs thus limiting the load carrying capacity. Right now collapse of aircraft structures cannot be simulated with sufficient reliability, leading to over-conservative designs.More reliable determination requires knowledge of degradation due to static as well as low cycle loading in the post-buckling range. Improved slow and fast simulation tools as well as design guidelines for stiffened panels are needed which take skin stringer separation and material degradation into account. Reliable fast tools reducing design and analysis time by an order of magnitude, will allow for an economic design process, whereas very accurate but necessarily slow tools are required for the final certification. The project will deliver both types of tools, ready for industrial application. Industry brings in experience with design and manufacture of real shells; research contributes knowledge on testing and on development of simulation tools. Design guidelines are defined in common, and the developed tools are validated by industry.The results comprise a substantially extended data base on material properties and on collapse of undamaged and pre-damaged statically and low cyclically loaded structures, degradation models, improved slow and fast computation tools as well as design guidelines. The knowledge, the experience, the results and especially the fast tools of the running FP 5 project POSICOSS form an excellent basis for COCOMAT and allow to start work at a very high level. Urgent industrial need is manifested by involvement of eight companies.
Source :
cordis
Aircraft Reliability Through Intelligent Materials Application
ARTIMA Subjects :
Safety, Aerospace Technology, Social Aspects, Standards, Economic Aspects, Innovation, Technology Transfer, Electronics, Microelectronics, Evaluation, Telecommunications, Policies, Information Processing, Information Systems
Contract type :
Specific Targeted Research Project
Participants :
AERNNOVA ENGINEERING SOLUTIONS S.A. ESPAÑA
AERNNOVA ENGINEERING SOLUTIONS S.A.
R&D DEPARTMENT C/Leonardo Da Vinci, 13-Parque Tecnologico De Alava ESPAÑA
EADS DEUTSCHLAND GMBH DEUTSCHLAND
EADS DEUTSCHLAND GMBH
CORPORATE RESEARCH CENTER GERMANY, DEPT. MICROSYSTEMS & ELECTRONICS (LG-ME) WILLY-MESSERSCHMITT-STRASSE DEUTSCHLAND
THE SWEDISH DEFENCE RESEARCH AGENCY SVERIGE
THE SWEDISH DEFENCE RESEARCH AGENCY
AERONAUTICS DIVISION, FFA SE-172 90 SVERIGE
ADAPTIVE MATERIALS TECHNOLOGY - ADAPTAMAT LTD. SUOMI/FINLAND
ADAPTIVE MATERIALS TECHNOLOGY - ADAPTAMAT LTD.
ADAPTAMAT LTD. YRITYSPIHA 5 SUOMI/FINLAND
ADAPTIVE MATERIALS TECHNOLOGY ADAPTAMAT Finland
ADAPTIVE MATERIALS TECHNOLOGY ADAPTAMAT
ADAPTAMAT LTD. YRITYSPIHA 5 Finland
EADS DEUTSCHLAND Germany
EADS DEUTSCHLAND
Postfach Willy-Messerschmitt-Strasse Germany
AERNNOVA ENGINEERING SOLUTIONS Spain
AERNNOVA ENGINEERING SOLUTIONS
DESIGN DEPARTMENT- Leonardo Da Vinci, 13 Spain
The objective of the proposed research is to achieve a leap improvement in aircraft reliability through the application of smart materials. There exists an acute need to develop the capability to monitor aircraft structural health in real-time, in a reliable manner. Real-time structural health monitoring will not only improve the overall safety but will also made it possible to replace Corrective or Preventive maintenance modes with much more efficient Predictive or Proactive maintenance procedures- thus reducing the associated cost. Similarly, vibrations and noise levels are still to high in certain aircraft. Systems based on smart materials defined as solid-state actuators activated by external fields, e.g., electric or magnetic, can address all these factors. Smart materials have already reached a sufficient level of maturity to benefit from their unique characteristics not only in laboratory but also in an industrial environment. No moving parts, the ease of integration with metallic and composite structures and the capability to provide distributed actuation are among their most important characteristics. This project will take advantage on an extensive body of knowledge accumulated during nearly two decades of development of smart materials and their applications. The proposed project will give a final push to produce realistic industrial solutions for real-time structural health monitoring and aircraft vibrations reduction. The most promising methods will be tested on large-scale specimens, such as a portion of a commuter aircraft fuselage. Project goals will be achieved by a network consisting of several production companies, research institutes and universities. The know-how developed as a part of this project is ideal to stimulate creation and development of small, high-tech enterprises.
Source :
cordis
Integration of technologies in support of a passenger and environmentally friendly helicopter (FRIENDCOPTER)
FRIENDCOPTER Subjects :
Policies, Standards, Economic Aspects, Safety, Information Processing, Information Systems, Telecommunications, Electronics, Microelectronics, Social Aspects, Innovation, Technology Transfer, Aerospace Technology, Evaluation
Contract type :
Integrated Project
Participants :
VERTAIR EEIG, C/O AECMA BELGIQUE-BELGIË
VERTAIR EEIG, C/O AECMA
VERTAIR MANAGEMENT BOARD C/O AECMA Gulledelle 94 BELGIQUE-BELGIË
CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA ITALIA
CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA
PMAE - PROGRAM MANAGEMENT AREA HELICOPTERS & VTOL PROGRAMMES Via Maiorise s.n.c. ITALIA
LEUVEN MEASUREMENT SYSTEMS INTERNATIONAL N.V. BELGIQUE-BELGIË
LEUVEN MEASUREMENT SYSTEMS INTERNATIONAL N.V.
RESEARCH & TECHNOLOGY DEVELOPMENT - TEST DIVISION Interleuvenlaan 68 BELGIQUE-BELGIË
AERNNOVA ENGINEERING SOLUTIONS, S.A ESPAÑA
AERNNOVA ENGINEERING SOLUTIONS, S.A
R&D DEPARTMENT PARQUE TECHNOLOGICO DE ALAVA, C/ LEONARDO DA VINCI, 13 ESPAÑA
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AÉROSPATIALES' FRANCE
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AÉROSPATIALES'
ONERA BP72 Avenue de la Division Leclerc n°29 FRANCE
CRANFILED UNIVERSITY UNITED KINGDOM
CRANFILED UNIVERSITY
DEPARTMENT OF AEROSPACE SCIENCES, SCHOOL OF ENGINEERING, FLUID MECH.& COMP. SC. GROUP UNITED KINGDOM
DEUTSCHES ZENTRUM FÜR LUFT - UND RAUMFAHRT E.V. DEUTSCHLAND
DEUTSCHES ZENTRUM FÜR LUFT - UND RAUMFAHRT E.V.
INSTITUTE OF AERODYNAMICS AND FLOW TECHNOLOGY INSTITUTE OF STRUCTURAL MECHANICS Linder Höhe DEUTSCHLAND
KUNGLIGA TEKNISKA HÖGSKOLAN SVERIGE
KUNGLIGA TEKNISKA HÖGSKOLAN
KTH AERONAUTICAL AND VEHICLE ENGINEERING/MWL Valhallavägen 79 SVERIGE
INGENIERIA DE SISTEMAS PARA LA DEFENSA DE ESPAÑA, S.A. ESPAÑA
INGENIERIA DE SISTEMAS PARA LA DEFENSA DE ESPAÑA, S.A.
TRANSPORT SYSTEM DIVISION Edison, 4 ESPAÑA
CARL VON OSSIETZKY UNIVERSITÄT OLDENBURG ( OLDENBURG UNIVERSITY) DEUTSCHLAND
CARL VON OSSIETZKY UNIVERSITÄT OLDENBURG ( OLDENBURG UNIVERSITY)
INSTITUTE OF PHYSICS -ACOUSTICS Carl-von-Ossietzky-Str. DEUTSCHLAND
WYTWORNIA SPRZETU KOMUNIKACYJNEGO "PZL - SWIDNIK" SA POLSKA
WYTWORNIA SPRZETU KOMUNIKACYJNEGO "PZL - SWIDNIK" SA
RESEARCH AND DEVELOPMENT CENTER al. Lotnikow Polskich 1 POLSKA
RIGA TECHNICAL UNIVERSITY LATVIJA
RIGA TECHNICAL UNIVERSITY
INSTITUTE OF MATERIALS AND STRUCTURES Kalku iela 1 LATVIJA
EUROCOPTER DEUTSCHLAND GMBH DEUTSCHLAND
EUROCOPTER DEUTSCHLAND GMBH
AERODYNAMICS DEUTSCHLAND
INGENIERA Y ECONOMIA DEL TRANSPORTE, S.A. ESPAÑA
INGENIERA Y ECONOMIA DEL TRANSPORTE, S.A.
AERONAUTICAL SYSTEMS Paseo Habana 138 ESPAÑA
DIPARTIMENTO DI INGEGNERIA MECCANICA E INDUSTRIALE - UNIVERSITÀ DEGLI STUDI ROMA TRE ITALIA
DIPARTIMENTO DI INGEGNERIA MECCANICA E INDUSTRIALE - UNIVERSITÀ DEGLI STUDI ROMA TRE
DIPARTIMENTO DI INGEGNERIA MECCANICA E INDUSTRIALE Via della Vasca Navale 79 ITALIA
FREE FIELD TECHNOLOGIES BELGIQUE-BELGIË
FREE FIELD TECHNOLOGIES
FREE FIELD TECHNOLOGIES SA 16 Place de l'Université' BELGIQUE-BELGIË
ZF LUFTFAHRTTECHNIK GMBH; HANDELSREGISTER HOFGEISMAR HRB 9101 DEUTSCHLAND
ZF LUFTFAHRTTECHNIK GMBH; HANDELSREGISTER HOFGEISMAR HRB 9101
RESEARCH AND DEVELOPMENT LE - PRODUCT DEPARTMENT LX, TESTING DEPARTMENT LB-V Flugplatzstrasse DEUTSCHLAND
ISTITUTO SUPERIOR TÉCNICO PORTUGAL
ISTITUTO SUPERIOR TÉCNICO
DEPARTAMENTO DE ENGENHARIA MECÂNICA (DEM) Av. Rovisco Pais PORTUGAL
ANOTEC CONSULTING, S.L. ESPAÑA
ANOTEC CONSULTING, S.L.
AEROACOUSTICS ROSALIA DE CASTRO 36 ESPAÑA
EADS DEUTSCHLAND GMBH CORPORATE RESEARCH CENTRE DEUTSCHLAND
EADS DEUTSCHLAND GMBH CORPORATE RESEARCH CENTRE
EADS INNOVATION WORKS GERMANY, DEPT.KEY PROJECT MANAGEMENT (IW-PM) Willy-Messerschmitt-Strasse DEUTSCHLAND
NOLIAC A/S DANMARK
NOLIAC A/S
R&D Hejreskovvej 18 DANMARK
VÝZKUMNÝ A ZKUSEBNI LETECKÝ ÙSTAV, A.S. CESKA REPUBLIKA
VÝZKUMNÝ A ZKUSEBNI LETECKÝ ÙSTAV, A.S.
HIGH-SPEED AERODYNAMICS DEPARTMENT Beranových 130 CESKA REPUBLIKA
UNIVERSITY OF PATRAS HELLAS
UNIVERSITY OF PATRAS
DEPT. OF MECHANICAL AND AERONAUTICAL ENGINEERING University of Patras, Research Committee HELLAS
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM (NATIONAL AEROSPACE LABORATORY) NEDERLAND
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM (NATIONAL AEROSPACE LABORATORY)
HELICOPTER DEPARTMENT (VH) PO Box 90502 Anthony Fokkerweg 2 NEDERLAND
FORM TECH GMBH DEUTSCHLAND
FORM TECH GMBH
FORMTECH GMBH Mittelwendung 35 DEUTSCHLAND
POLITECNICO DI MILANO ITALIA
POLITECNICO DI MILANO
DIPARTIMENTO DI INGEGNERIA AEROSPAZIALE (AEROSPACE DEPT. ENGINEERING) Piazza Leonardo da Vinci, 32 ITALIA
FREE FIELD TECHNOLOGIES Belgium
FREE FIELD TECHNOLOGIES
Belgium
LEUVEN MEASUREMENTS AND SYSTEMS INTERNATIONAL Belgium
LEUVEN MEASUREMENTS AND SYSTEMS INTERNATIONAL
CAE RESEARCH DEPARTMENT Interleuvenlaan 68, Researchpark Haasrode Z1 Belgium
VERTAIR EEIG, C/O AECMA Belgium
VERTAIR EEIG, C/O AECMA
VERTAIR MANAGEMENT BOARD C/O AECMA Gulledelle 94 Belgium
NOLIAC Denmark
NOLIAC
Denmark
WYTWORNIA SPRZETU KOMUNIKACYJNEGO "PZL-SWIDNIK" Poland
WYTWORNIA SPRZETU KOMUNIKACYJNEGO "PZL-SWIDNIK"
RESEARCH & DEVELOPMENT CENTRE Al. Lotnikow Polskich 1 Poland
AIRCELLE France
AIRCELLE
ENGINEERING DEPARTMENT B.P. 91 Route du Pont VIII France
DAHER LHOTELLIER AEROTECHNOLOGIES France
DAHER LHOTELLIER AEROTECHNOLOGIES
TECHNICAL DEPARTMENT 23 route de Tours France
Eurocopter France France
Eurocopter France
RESEARCH PROGRAMME Aeroport International Marseille France
PAULSTRA SNC France
PAULSTRA SNC
PAULSTRA-VIBRACHOC RUE MARIUS AUFAN, 61 France
EADS DEUTSCHLAND CORPORATE RESEARCH CENTRE Germany
EADS DEUTSCHLAND CORPORATE RESEARCH CENTRE
CORPORATE RESEARCH CENTRE GERMANY Willy-Messerschmitt-Straße Germany
EUROCOPTER DEUTSCHLAND Germany
EUROCOPTER DEUTSCHLAND
AERODYNAMICS AND FLIGHT MECHANICS Postfach Willy Messerschmitt Str. 1 Germany
FORM TECH Germany
FORM TECH
FORMTECH GMBH Mittelwendung 35 Germany
ZF LUFTFAHRTTECHNIK HANDELSREGISTER HOFGEISMAR HRB 9101 Germany
ZF LUFTFAHRTTECHNIK HANDELSREGISTER HOFGEISMAR HRB 9101
RESEARCH AND DEVELOPMENT LE - PRODUCT DEPARTMENT LX, TESTING DEPARTMENT LB-V Flugplatzstrasse Germany
INSTITUTO DE SOLDADURA E QUALIDADE ASSOCIACAO Portugal
INSTITUTO DE SOLDADURA E QUALIDADE ASSOCIACAO
Apartado 012 Av. Professor Doutor Cavaco Silva n° 33, Talaide, Taguspark Portugal
AERNNOVA ENGINEERING SOLUTIONS Spain
AERNNOVA ENGINEERING SOLUTIONS
DESIGN DEPARTMENT- Leonardo Da Vinci, 13 Spain
ANOTEC CONSULTING Spain
ANOTEC CONSULTING
AEROACOUSTICS ROSALIA DE CASTRO 36 Spain
AGUSTA Italy
AGUSTA
Via G. Augusta, 520 Italy
WESTLAND HELICOPTERS United Kingdom
WESTLAND HELICOPTERS
ROTOR AERODYNAMICS, ROTOR SYSTEMS Lysander Road United Kingdom
TURBOMECA France
TURBOMECA
France
Today's helicopters need to be improved further with respect to environmental and public acceptance. Helicopters generate external noise, cabin noise and vibration due to the complex nature of their dynamic systems and suffer from NOx emission; like other transport systems. It is therefore very essential that the new generation rotorcraft adress these issues to improve the situation, to make them environmentally friendly and acceptable to the general public The modern society needs this indispensable system due to its ability to fly medical, rescue and law enforcement missions. These missions require flight profiles close to populated areas. Hence, a number of enhancements appears mandatory. In detail, the following goals are envisaged: - External noise levels 10 db below the current ICAO/JAA rules especially during approach, - A reduction of fuel consumption up to 20 % for high speed flights. - Cabin noise levels below 70 dBA similar to airliner cabins for normal cruise flight, - Cabin vibrations below 0,05 g corresponding to jet smooth ride comfort for the same flight regime. Because of the large and fast rotating rotor, the non-symmetric rotor flow, the close vicinity of main gearbox and passenger position and the specific requests of engine performance, the targets mentioned above are highly challenging. In order to comply with the research objectives, an extreme high tech initiative is required, enabling however European aeronautic industry to hold their own against international competitors. In order to do so, short and long term objectives are planned targeting the following technology topics: - Short Term objectives: Noise Abatement Flight Procedures, Cabin Noise Reduction Engine Noise Reduction - Long Term Objectives Active Blade Control The activities envisaged in Friendcopter are to provide a number of key deliverables. All of these will have undergone intense efficiency testing, mostly by flight tests. In det#'
Source :
cordis
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