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07:30 - 08:30
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Registration - Registration |
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08:30 - 09:00
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Session 5. Virtual testing of aircraft hydraulic systems |
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09:00 - 09:30
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Session 5. Automated measurement of backlash and stiffness in electro-mechanical flight control actuation |
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09:30 - 10:00
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Session 5. Methodologies and test-rig configurations for the experimental improvement of aerospace flight control actuation systems |
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10:00 - 10:30
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Session 5. Flight control system architecture comprehensive evaluation based on electrical actuators for more electric aircraft |
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10:30 - 11:00
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Coffee break and poster display |
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11:00 - 11:30
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Session 6. EMADEF: a fully comprehensive analytical tool for the initial design of electro-mechanical servo-actuators for primary flight controls |
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11:30 - 12:00
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Session 6. Optimization of primary flight control actuation system using parametric sizing models of actuators, power electronics and structural analysis |
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12:00 - 12:30
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Session 6. Power cycling reliability and thermal performances of SiC power modules |
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12:30 - 14:00
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Lunch |
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14:00 - 14:30
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Session 7. Challenges of ball screw lifetime calculation in primary flight control applications |
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14:30 - 15:00
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Session 7. High fidelity model for efficiency calculation of ball screws for flight control actuators |
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15:00 - 15:30
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Session 7. A novel industry-oriented EMA model for ball screw optimised design including motor torque response and friction |
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15:30 - 16:00
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Coffee break and poster display |
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16:00 - 16:30
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Session 8. Development of an innovative piezo actuated flow servovalve with additive manufacturing body |
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16:30 - 17:00
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Session 8. The hydraulic infinite linear actuator applied to a high lift system |
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17:00 - 17:30
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Session 8. Implications of the use of flux-switching motors for aerospace actuation systems |
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18:30 - 20:00
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Private visit of Toulouse Museum - Private visit of Toulouse Museum |
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20:00 - 23:00
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Aperitive and banquet |
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