
SAFRAN AEROSYSTEMS SAS
SAFRAN AEROSYSTEMS SAS
10 Projects, page 1 of 2
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 Open Access Mandate for Publications assignment_turned_in Project2015 - 2019Partners:Cranfield University, AIRBUS PROSKY, ENAV, EMBRAER PORTUGAL SA, KLM +31 partnersCranfield University,AIRBUS PROSKY,ENAV,EMBRAER PORTUGAL SA,KLM,Airbus (Netherlands),INCAS,STAC,CSEM,VZLÚ,FSUE,Lufthansa (Germany),AIRBUS DEFENCE AND SPACE SA,Thalgo (France),INCAS,CAA,Airbus (India),DLR,BAS,Deep Blue (Italy),Trinity College Dublin, Ireland,INTA,Institut Polytechnique de Bordeaux,SAFRAN AEROSYSTEMS SAS,FOI,CIRA,EUROCONTROL - EUROPEAN ORGANISATION FOR THE SAFETY OF AIR NAVIGATION,ONERA,TUM,LEONARDO,Alenia Aermacchi,LSE,CEiiA,Royal NLR,EMBRAER PORTUGAL COMPOSITOS,AIRBUS OPERATIONSFunder: European Commission Project Code: 640597Overall Budget: 16,270,300 EURFunder Contribution: 14,882,900 EURThe EC Flight Path 2050 vision aims to achieve the highest levels of safety to ensure that passengers and freight as well as the air transport system and its infrastructure are protected. However, trends in safety performance over the last decade indicate that the ACARE Vision 2020 safety goal of an 80% reduction of the accident rate is not being achieved. A stronger focus on safety is required. There is a need to start a Joint Research Programme (JRP) on Aviation Safety, aiming for Coordinated Safety Research as well as Safety Research Coordination. The proposed JRP Safety, established under coordination of EREA, is built on European safety priorities, around four main themes with each theme consisting of a small set of projects. Theme 1 (New solutions for today’s accidents) aims for breakthrough research with the purpose of enabling a direct, specific, significant risk reduction in the medium term. Theme 2 (Strengthening the capability to manage risk) conducts research on processes and technologies to enable the aviation system actors to achieve near-total control over the safety risk in the air transport system. Theme 3 (Building ultra-resilient systems and operators) conducts research on the improvement of Systems and the Human Operator with the specific aim to improve safety performance under unanticipated circumstances. Theme 4 (Building ultra-resilient vehicles), aims at reducing the effect of external hazards on the aerial vehicle integrity, as well as improving the safety of the cabin environment. To really connect and drive complementary Safety R&D (by EREA) to safety priorities as put forward in the EASA European Aviation Safety plan (EASp) and the EC ACARE Strategic Research and Innovation (RIA)Agenda, Safety Research Coordination activities are proposed. Focus on key priorities that impact the safety level most will significantly increase the leverage effect of the complementary safety Research and Innovation actions planned and performed by EREA.
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.
more_vert Open Access Mandate for Publications and Research data assignment_turned_in Project2023 - 2026Partners:TU Delft, KhAI, GE AEROSPACE POLAND SPOLKA Z OGRANICZONA ODPOWIEDZIALNOSCIA, ONERA, ARIANEGROUP SAS +23 partnersTU Delft,KhAI,GE AEROSPACE POLAND SPOLKA Z OGRANICZONA ODPOWIEDZIALNOSCIA,ONERA,ARIANEGROUP SAS,SAFRAN ELECTRONICS & DEFENSE,SAFRAN AERO BOOSTERS,SENIOR AEROSPACE ERMETO SAS,FACT,ILT TECNOLOGIE S.R.L.,OMB SALERI SPA,TECHNOFAN,DLR,GENERAL ELECTRIC DEUTSCHLAND HOLDING GMBH,AIRBUS OPERATIONS,SAFRAN AEROSYSTEMS SAS,SOGECLAIR AEROSPACE SAS,University of Florence,SAFRAN AIRCRAFT ENGINES,SAFRAN FILTRATION SYSTEMS,SAFRAN ELECTRICAL & POWER,GE AVIO SRL,PFW,CETIM,SIEMENS PLM,CONS. SVILUPPO DELLE AREE GEOTERMICHE,Ergon Research SRL,GE MARMARA TECHNOLOGY CENTER MUHENDISLIK HIZMETLERI LIMITED SIRKETIFunder: European Commission Project Code: 101102019Overall Budget: 110,588,000 EURFunder Contribution: 80,495,200 EURThe HYDEA project, which stands for “HYdrogen DEmonstrator for Aviation”, proposes a robust technology maturation plan to develop an H2C (Hydrogen Combustion) propulsion system compatible with an Entry Into Service of a zero-CO2 low-emission aircraft in 2035, consistently with the expected timeframe of the European Green Deal and CA SRIA objectives. The project aims to address fundamental questions related to the use of hydrogen as an aviation fuel, concentrating on the development and testing in relevant conditions of an H2 combustor and H2 fuel system, also including emission studies and further technologies which will serve as an outlook to future engines, i.e. NOx optimization studies, potential contrails emissions and investigating integration aspects between engine and aircraft. HYDEA results will be core for the ZEROe technology exploration project, launched by Airbus in 2020. The revolutionary technologies in scope call for an early engagement and dialogue with EASA (European Union Aviation Safety Agency) within HYDEA, starting from phase 1.
more_vert Open Access Mandate for Publications and Research data assignment_turned_in Project2023 - 2025Partners:UTRC, SAFRAN ELECTRICAL COMPONENTS, Wrocław University of Science and Technology, ALES, UGR +29 partnersUTRC,SAFRAN ELECTRICAL COMPONENTS,Wrocław University of Science and Technology,ALES,UGR,AIT,TUL,DIEHL AEROSPACE GMBH,Thalgo (France),SAFRAN AEROSYSTEMS SAS,UNISA,DRAKA,FHG,Carlos III University of Madrid,SEPC,University of Bayreuth,SAFRAN ELECTRICAL & POWER,AERTEC,UNIVERSITY OF NOTTINGHAM ITALY,LEONARDO,Royal NLR,FOKKER ELMO BV,Ilmenau University of Technology,University of Campania "Luigi Vanvitelli",HS ELEKTRONIK SYSTEME GMBH,AER,TEMAI,UPM,IRT ANTOINE DE SAINT EXUPERY,TECNALIA,AAU,GMVIS SKYSOFT,AIRBUS DEFENCE AND SPACE SA,SAFRAN SAFunder: European Commission Project Code: 101101961Overall Budget: 45,158,000 EURFunder Contribution: 34,210,300 EURAviation needs to meet the ambitious targets of the European Green Deal. This means a step change is needed towards hybrid electric regional aircraft to significantly reduce the fuel burn. This can only be accomplished with power distribution networks that can safely handle the high power and high voltage levels, ultimately up to several Megawatt. The HECATE project will address the associated challenges of system weight and power density, high voltage challenges with lightning, arcing and electromagnetic interference as well as optimized thermal management, in addition to digitizing the design process with digital twins. This will lead to transformative technology bricks, which are holistically optimized at system integration architecture level. The HECATE project will demonstrate a >500 kW architecture in a copper bird at TRL5. This will provide a clearer understanding of high voltage challenges and how to mitigate them, with a scalability roadmap towards CAJU Phase 2 flight demonstration and exploitation in a 2035 new built Hybrid Electric Regional aircraft. Also, environmental impact and LCA will be assessed. For optimal alignment and ensuring certifiability, HECATE will establish relationships with other Clean Aviation projects (e.g. HER-01 for MW propulsion, HER-02 for thermal, TRA-01 for architecture, TRA-02 for certification) and authorities and standards groups (e.g. EASA, EUROCAE). As a set of key enabling technologies that are well integrated, HECATE will contribute to the Clean Aviation SRIA and its expected impacts, and fully fulfill the call's expected outcomes. The 37-member consortium mobilizes key EU based industries throughout the entire existing supply chain: from aircraft OEMs to system integrators, to system and subsystems suppliers, 5 of which are SMEs. 17 RTOs, complement and reinforce the industries, which also ensures knowledge gained is embedded in future research and education programs. HECATE requests 34 210 348€ of grant.
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