Témata

• Spring-in prediction capability for large integral wing structure [SAT]
• Development and application of an innovative methodology devoted for high temperature characterization of high efficient composite structures
• MEMS sensors, wireless and innovative measurement systems for validation of HVDC system Structure integration and for new SHMS architectures
• Development of a multipurpose test rig and validation of an innovative rotorcraft vertical tail
• Model Manufacturing and Wind Tunnel Testing of High Lift System for SAT Aircraft
• Cost analysis software platform for evaluating innovative manufacturing technology for SMART fuselage
• Calibrating Ultrasonic Sensors for atmospheric corrosion.
• Material modelling platform for generation of thermoplastic material allowable
• Design Against Distortion: Part distortion prediction, design for minimized distortion, additive manufactured polymer aerospace parts
• Smart Active Inceptors System definition for Tilt Rotor application
• Tilt Rotor Whirl Flutter experimental investigation and assessment
• Innovative mould for thermoplastic skin of the lower fuselage demonstrator
• Design, manufacture and deliver a high performance, low cost, low weight Nacelle Structure for Next Generation TiltRotor (NGCTR) - Technology Demonstrator (TD)
• High performance gas expansion system for halon-free cargo hold fire suppression system.
• Innovative tooling, end-effector development and industrialisation for welding of thermoplastic components
• Automated data collection and semi-supervised processing framework for deep learning
• Audio Communication Manager for Disruptive Cockpit demonstrator
• Safe emergency trajectory generator
• Aircraft Design Optimisation providing optimum performance towards limiting aviation’s contribution towards Global Warming
• Research for the development of Particulate Matter (PM) regulations and guidelines
• Advanced High Bypass Ratio Low-Speed Composite Fan Design and Validation
• Measurement of rotor vibration using tip-timing for high speed booster and evaluation of associated uncertainties
• Turbulence modeling of heat exchangers and roughness impact
• Ground vortex characterization method applicable for engine testing
• Additive manufacturing boundary limits assessment for Eco Design process optimization [ECO]
• Fan inlet advanced distortion simulator
• Innovative low noise fan stator technologies for 2030+ powerplants
• BLI configurations of classical tube and wing aircraft architecture - Wind tunnel tests insight into propulsor inlet distortion and power saving
• Rear End Structural Test Program – Component & Subcomponent tests
• Rear End Aerodynamic and Aeroelastic Studies
• Fatigue life prediction on Inco 718 part subject to service induced damages
• Rear End Structural Test Program - Low level tests
• Development of System pipework and Tooling for Sub-Assembly, Final-Assembly of the HLFC-wing Prototype
• Shielding/High-lift composite thermoplastic flap manufacturing, tool design and manufacturing & process definition
• UHBR Installed Advanced Nacelle Optimisation and Evaluation Close Coupled to Wing
• Insulation Monitoring for IT Grounded (Isolation Terra) Aerospace Electrical Systems
• Innovative Nacelle cowl opening system
• Non-Intrusive Flow Field Measurement within a UHBR Intake
• Assessment of arc tracking hazards in high voltage aerospace systems
• Camera-based smart sensing system for cabin readiness
• Software engine for multi-criteria decision support in civil aircraft flight management
• Machine learning to detect Cyber intrusion and anomalies
• Multi-Material Thermoplastic high pressure Nitrogen Tanks for Aircrafts
• Complex cores for CFRP primary structural products manufactured with high pressure RTM
• Additive Manufacturing Magnetic Motor
• Aircraft wing architecture optimal assembly
• Flexible and Automated Manufacturing of wound components for high reliability
• Virtual Testing Based Certification
• Demonstration and test of low-loss, high reliability, high speed, bearing-relief generators
• Alternative energy sources and novel propulsion technologies
• Environmental regulations and policies
• Overall Air Transport System Vehicle Scenarios
• Anticontamination Coatings and Cleaning Solutions for Laminar Wings
• Biphasic Heat Transport Integration for Efficient Heat Exchange within Composite materials Nacelle
• Conceptual Design of a 19-passenger Commuter Aircraft with near zero emissions