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ONERA , ZL M&M , STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR , AIRBUS OPERATIONS , UoN , FOKKER TECHNOLOGIES HOLDING BV , AIRBUS OPERATIONS SL , INVENT , AEROTEX UK LLP , POLSKIE ZAKLADY LOTNICZE , Royal NLR , ECE , AIRBUS DEFENCE AND SPACE GMBH , P.G.A. ELECTRONIC , ARTUS SAS , Aernnova (Spain) , AIRBUS OPERATIONS GMBH , UPM , SISW , Tabor (Poland) , ...
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ONERA , ZL M&M , STORK FOKKER AESP FOKKER STRUCTURES FOKKER AEROSTR , AIRBUS OPERATIONS , UoN , FOKKER TECHNOLOGIES HOLDING BV , AIRBUS OPERATIONS SL , INVENT , AEROTEX UK LLP , POLSKIE ZAKLADY LOTNICZE , Royal NLR , ECE , AIRBUS DEFENCE AND SPACE GMBH , P.G.A. ELECTRONIC , ARTUS SAS , Aernnova (Spain) , AIRBUS OPERATIONS GMBH , UPM , SISW , Tabor (Poland) , INEGI , Imperial , EVEKTOR, spol. s.r.o. , ELEMENT SEVILLE , Inasco (Greece) , AIRBUS DEFENCE AND SPACE SA , FUNDACION CENTRO DE TECNOLOGIAS AERONAUTICAS , TECNALIA , AIRBUS HELICOPTERS DEUTSCHLAND GMBH , IAI , CORIOLIS COMPOSITES SAS , ISQ , Eurotech (Poland) , TECHNI-MODUL ENGINEERING SA , Piaggio Aerospace (Italy) , DEMA , Ferroperm Piezoceramics AS , P.W.METROL , Airbus Operations Limited , AM , CAERO , VUB , University Federico II of Naples , TU Delft , ASCO Industries (Belgium) , University of Patras , FADA-CATEC , BSC , RAMAL , POLITO , HAI , GEVEN SPA , GE AVIATION SYSTEMS LTD , SAAB , UEL , Selvita , UNIBO , DLR , CAPGEMINI ENGINEERING DEUTSCHLAND SAS & CO KG , DANOBAT , Noesis Solutions (Belgium) , ACUMEN DESIGN ASSOCIATES LIMITED , LEO-LTD , ALTRAN TECHNOLOGIES , CT INGENIEROS AAI , AKZO NOBEL CAR REFINISHES BV , AERTEC , FHG , University of Sheffield , University of Stuttgart , LORTEK , FIDAMC , CIRA , Dassault Aviation (France) , MEGGITT AEROSPACE LIMITED , Airbus (India) , LEONARDO , SZEL-TECH
The 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.
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