
STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR
STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR
15 Projects, page 1 of 3
Open Access Mandate for Publications assignment_turned_in Project2020 - 2024Partners:ARTUS SAS, ELEMENT SEVILLE, Selvita, P.W.METROL, CAERO +72 partnersARTUS SAS,ELEMENT SEVILLE,Selvita,P.W.METROL,CAERO,UPM,SIEC BADAWCZA LUKASIEWICZ-INSTYTUT LOTNICTWA,Airbus Operations Limited,INVENT,ECE,Tabor (Poland),University of Patras,CIRA,STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR,AIRBUS OPERATIONS SL,RAMAL,LEONARDO,Eurotech (Poland),TECHNI-MODUL ENGINEERING SA,FHG,Noesis Solutions (Belgium),FOKKER TECHNOLOGIES HOLDING BV,GE AVIATION SYSTEMS LTD,ISQ,AEROTEX UK LLP,LORTEK,ΕΑΒ,University of Sheffield,P.G.A. ELECTRONIC,University of Nottingham,ZL M&M,AIRBUS OPERATIONS,ONERA,GEVEN SPA,LEO-LTD,SISW,Łukasiewicz Research Network,University of Stuttgart,Dassault Aviation (France),Aernnova (Spain),CAPGEMINI ENGINEERING DEUTSCHLAND SAS & CO KG,SAAB,Airbus (Netherlands),ACUMEN DESIGN ASSOCIATES LIMITED,Imperial,SZEL-TECH,AIRBUS DEFENCE AND SPACE SA,ASCO Industries (Belgium),Royal NLR,POLITO,DEMA,Inasco (Greece),Airbus (India),Piaggio Aerospace (Italy),VUB,AKZO NOBEL CAR REFINISHES BV,INEGI,AIRBUS OPERATIONS GMBH,CORIOLIS COMPOSITES SAS,FADA-CATEC,FIDAMC,TECNALIA,AIRBUS HELICOPTERS DEUTSCHLAND GMBH,IAI,DLR,UNIBO,FUNDACION CENTRO DE TECNOLOGIAS AERONAUTICAS,University Federico II of Naples,BSC,Ferroperm Piezoceramics AS,DANOBAT,AM,EVEKTOR, spol. s.r.o.,AERTEC,MEGGITT AEROSPACE LIMITED,TU Delft,POLSKIE ZAKLADY LOTNICZEFunder: European Commission Project Code: 945521Overall Budget: 112,809,000 EURFunder Contribution: 79,628,800 EURThe Airframe ITD aims at re-thinking and developing the technologies as building blocks and the “solution space” on the level of the entire or holistic aircraft: pushing aerodynamics across new frontiers, combining and integrating new materials and structural techniques – and integrating innovative new controls and propulsion architectures with the airframe; and optimizing this against the challenges of weight, cost, life-cycle impact and durability.
more_vert Open Access Mandate for Publications assignment_turned_in Project2020 - 2023Partners:Royal NLR, FLG, SAFRAN ELECTRICAL & POWER, ESI (France), TriaGnoSys +54 partnersRoyal NLR,FLG,SAFRAN ELECTRICAL & POWER,ESI (France),TriaGnoSys,University of Bradford,Airbus (India),ZODIAC,FOKKER TECHNOLOGIES HOLDING BV,University of Nottingham,MICHELIN,DIEHL AVIATION GILCHING GMBH,Arkema (France),AIRBUS OPERATIONS,ALTYS Technologies,SAFRAN SA,Thalgo (France),CEA,DSPACE,SAFRAN AEROSYSTEMS SAS,CIRA,GOODRICH CONTROL SYSTEMS PRIVATE UNLIMITED COMPANY,Dassault Aviation (France),SELL GMBH,LIEBHERR-ELECTRONICS AND DRIVES GMBH,DIEHL AEROSPACE GMBH,TTTech Computertechnik (Austria),SIEC BADAWCZA LUKASIEWICZ-INSTYTUT LOTNICTWA,Airbus Operations Limited,LIEBHERR AEROSPACE TOULOUSE SAS,PRz,EVEKTOR, spol. s.r.o.,SEPC,HONEYWELL INTERNATIONAL SRO,ESI (Germany),GAS-UK,SAFRAN ELECTRONICS & DEFENSE,FREQUENTIS,ALES,ZODIAC SEATS FRANCE,SAAB,Piaggio Aerospace (Italy),NORD-MICRO GMBH & CO OHG,Tabor (Poland),Airbus (Netherlands),AIRTEL,UTRC,INTERTECHNIQUE,LLI,AIRSENSE ANALYTICS GMBH,Łukasiewicz Research Network,PEL,AIRBUS OPERATIONS GMBH,STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR,FAU,SAFRAN LANDING SYSTEMS,AIRBUS DEFENCE AND SPACE SA,SED-CS,ITIFunder: European Commission Project Code: 945535Overall Budget: 86,260,704 EURFunder Contribution: 62,623,700 EURThe Systems ITD will develop and build highly integrated, high TRL demonstrators in major areas such as power management, cockpit, wing, landing gear, to address the needs of future generation aircraft in terms of maturation, demonstration and Innovation. Integrated Cockpit Environment for New Functions & Operations - D1: Extended Cockpit - D24: Enhanced vision and awareness - D25: Integrated Modular Communications Innovative Cabin and Cargo technologies - D2: Equipment and systems for Cabin & Cargo applications Innovative and Integrated Electrical Wing Architecture and Components - D3: Smart Integrated Wing Demonstrator - D4: Innovative Electrical Wing Demonstrator Innovative Technologies and Optimized Architecture for Landing Gears - D5: Advanced Landing Gears Systems - D6: Electrical Nose Landing Gear System - D7: Electrical Rotorcraft Landing Gear System - D17: Advanced Landing Gear Sensing & Monitoring System High Power Electrical Generation and Conversion Architecture - D8.1: Innovative Power Generation and Conversion for large A/C - D8.2: Innovative Power Generation and Conversion for small A/C Innovative Energy Management Systems Architectures - D9: Innovative Electrical and Control/Command Networks for distribution systems - D10: HVDC Electrical Power Network Demonstrator Innovative Technologies for Environmental Control System - D11: Next Generation EECS for Large A/C - D12: Next Generation EECS Demonstrator for Regional A/C - D13: Next Generation Cooling systems Demonstrators - D16: Thermal Management demonstration on AVANT test rig Ice protection demonstration - D14: Advanced Electro-thermal Wing Ice Protection Demonstrator - D15: Ice Detection System Small Air Transport (SAT) Innovative Systems Solutions - D18, D19, D21: More Electric Aircraft level 0 - D20: Low power de-ice for SAT - D22: Safe and Comfortable Cabin - D23: Affordable future avionic solution for small aircraft ECO Design T2: Production Lifecycle Optimisation Long-term Technologies T1: Power Electronics T3: Modelling and Simulation Tools for System Integration on Aircraft
more_vert assignment_turned_in Project2013 - 2018Partners:TAU, Coexpair (Belgium), ARA, AcQ Inducom, AIRBUS OPERATIONS GMBH +38 partnersTAU,Coexpair (Belgium),ARA,AcQ Inducom,AIRBUS OPERATIONS GMBH,Airbus Operations Limited,ASCO Industries (Belgium),INCAS,Royal NLR,KTH,University of Manchester,IAI,BAES,Sonaca (Belgium),AIRBUS OPERATIONS,CIRA,ONERA,SAFRAN LANDING SYSTEMS,FHG,L - UP SAS,WUT,FSUE,SLCA,INVENT,AED,VZLÚ,CERFACS,AIRBUSGROUP LIMITED,University of London,IBK-Innovation (Germany),AIRBUS OPERATIONS SL,City, University of London,EADS DEUTSCHLAND GMBH,Dassault Aviation (France),DLR,STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR,INCAS,TUHH,TURKISH AEROSPACE INDUSTRIES TAI,GKN Aerospace Services Limited,FOI,CFSE,AEDFunder: European Commission Project Code: 604013more_vert Open Access Mandate for Publications and Research data assignment_turned_in Project2020 - 2025Partners:UNIMORE, CENTRO SVILUPPO MATERIALI SPA, TNO, TU Delft, ESI (Germany) +28 partnersUNIMORE,CENTRO SVILUPPO MATERIALI SPA,TNO,TU Delft,ESI (Germany),K-LOOPS SRL,TALLERES JASO INDUSTRIAL SL,INNOVATIVE SECURITY SOLUTIONS SRL,AIMEN,V2I,ACA,CECIMO,University of Coimbra,FHG,University of Patras,TECNALIA,VDL BUS ROESELARE,KVE,CEA,DGH Robotics,STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR,Royal NLR,ESI (France),IPC,FOKKER TECHNOLOGIES HOLDING BV,BIBA,MV WERFTEN,TRANSITION TECHNOLOGIES PSC SPOLKA AKCYJNA,TTS TECHNOLOGY TRANSFER SYSTEMS SRL,FUNDINGBOX ACCELERATOR SP ZOO,ATOS SPAIN SA,IDESA,COMETA SPAFunder: European Commission Project Code: 958303Overall Budget: 20,125,800 EURFunder Contribution: 14,722,000 EURThe manufacturing of large-scale parts needs the implementation of a holistic data management and integrated automation methodology to achieve the desired levels of precision using modular and more flexible equipment. Large-part manufacturing is characterized by the high customization required (built-customer specific). Also, manufacturing of complex large-scale parts involves a variety of subassemblies that must be manufactured and assembled. This high degree of personalization implies a great effort in the design and the posterior verification after manufacturing, to achieve high precision. On the other hand, this customised product-centric design requires an optimisation of the resources of the workshop –i.e. workers, machines, devices— for a responsive, reconfigurable and modular production, targeting the execution of key labour-intensive tasks by preserving industry-specific workers’ knowledge and skills (worker-centric approach). PENELOPE proposes a novel methodology linking product-centric data management and production planning and scheduling in a closed-loop digital pipeline for ensuring an accurate and precise manufacturability from the initial product design. PENELOPE is built over five pillars for developing a common methodology and vision deployed in four industrial-driven pilot lines in strategic manufacturing sectors (Oil&Gas, Shipbuilding, Aeronautics and Bus&Coach) and with potential replicability to other sectors. Moreover, it will be set a pan-European network of Didactic Factories and showrooms, providing training and upskilling capabilities enabling the workforce transition towards Industry 4.0 and general-purpose testbeds for assisting in the industry adoption. PENELOPE envision to highly-increase EU manufacturing sector competitiveness by increasing production performance, quality and accuracy while ensuring workers’ safety and resource efficiency.
more_vert Open Access Mandate for Publications assignment_turned_in Project2020 - 2024Partners:Coventry University, BAES, AIRBUS OPERATIONS, Dassault Aviation (France), ERNEO +40 partnersCoventry University,BAES,AIRBUS OPERATIONS,Dassault Aviation (France),ERNEO,Thalgo (France),FHG,TU Delft,AIRBUS OPERATIONS SL,ONERA,GKN AEROSPACE SWEDEN AB,SAFRAN AIRCRAFT ENGINES,Airbus (India),AES,GMVIS SKYSOFT,FOKKER ELMO BV,LIEBHERR AEROSPACE TOULOUSE SAS,AIRBUS OPERATIONS GMBH,Airbus (Netherlands),KM,Safran Nacelles,AKIRA,LLI,SAFRAN POWER UNITS,HONEYWELL INTERNATIONAL SRO,Royal NLR,FOKKER TECHNOLOGIES HOLDING BV,STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR,AKIRA MECATURBINES,Airbus Operations Limited,GENERAL ELECTRIC DEUTSCHLAND HOLDING GMBH,SAFRAN AEROSYSTEMS SAS,Sonaca (Belgium),GE AVIO SRL,CIRA,DAC,FIDAMC,SAAB,INTERTECHNIQUE,BL,DLR,Aernnova (Spain),AIRBUS DEFENCE AND SPACE SA,AIRBUS DEFENCE AND SPACE GMBH,Rolls-Royce (United Kingdom)Funder: European Commission Project Code: 945583Overall Budget: 235,320,992 EURFunder Contribution: 173,872,992 EURMain objective for the Clean Sky 2 Large Passenger Aircraft Programme (LPA) is to further mature and validate key technologies such as advanced wings and empennages design, making use of hybrid laminar airflow wing developments, the integration of most advanced engines into the large passenger aicraft aircraft design as well as an all-new next generation fuselage cabin and cockpit-navigation. Dedicated demonstrators are dealing with Research on best opportunities to combine radical propulsion concepts, and the opportunities to use scalled flight testing for the maturation and validation of these concepts via scaled flight testing. Components of Hybrid electric propulsion concepts are developed and tested in a major ground based test rig. The LPA program is also contributing with a major workpackage to the E-Fan X program. The R&T activities in the LPA program is split in 21 so-called demonstrators. In the project period 2020 and 2021 a substantial number of hardware items ground and flight test items will be manufactured, assembled tested. For some large items like the Multifunctional Fuselage demonstrators or the HLFC wing ground demonstrator the detailed design and manufacturing of test items will be commenced. For the great majority of contributing technologies a Technology Readyness level (TRL) 3 or 4 will be accomplished or even exceeded. Based on data generated for each key technology contributing to the LPA program inputs will be provided to the CleanSky Technology Evaluator via the integration in agreed concept aircraft models in order to conduct the overall CS2 assessement. LPA is also contributing to conduct Eco Design Life Cycle assessements for selected LPA technologies.
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