Planning
| Time |
Event |
(+)
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07:30 - 09:00
|
Registration - Registration |
|
|
09:00 - 09:15
|
Welcome - C. CHASSOT, director of research, INSA |
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09:15 - 09:45
|
Session 1. AIRBUS Research and perspectives for aircraft control actuation |
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09:45 - 10:15
|
Session 1. Electro-hydraulic system architectures for more electric aircraft - Comparison of central and zonal power packages |
|
|
10:15 - 10:45
|
Session 1. Spoiler and flap rotary EM actuation (REMA) implementation on a recently certified business jet |
|
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10:45 - 11:15
|
Coffee break and poster display |
|
|
11:15 - 11:45
|
Session 2. Pseudo direct drive electrical machine for primary flight control surface actuation |
|
|
11:45 - 12:15
|
Session 2. A model-based systems engineering approach for efficient flight control system architecture variants modelling in conceptual design |
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|
12:15 - 12:45
|
Session 2. State and development of actuation system and component in China |
|
|
12:45 - 14:00
|
Lunch |
|
|
14:00 - 14:30
|
Session 3. Reliability of the electronics for actuation? |
|
|
14:30 - 15:00
|
Session 3. Linear EMA HM using oil detection |
|
|
15:00 - 15:30
|
Session 3. First practical evaluation of a complete Fail-safe and 100% fault-tolerant inverter for critical load in aerospace application |
|
|
15:30 - 16:00
|
Coffee break and poster display |
|
|
16:00 - 16:30
|
Session 4. Electromechanical actuation for landing gear application: A case study on end-stroke impact in case of high speed free-fall emergency extension |
|
|
16:30 - 17:00
|
Session 4. Physical modeling and bond graph combined approach to guide failure analysis in an aircraft hydraulic brake system |
|
|
17:00 - 17:30
|
Session 4. Overview of Integrated Self-Powered Brake System for aircrafts |
|
| Time |
Event |
(+)
|
|
07:30 - 08:30
|
Registration - Registration |
|
|
08:30 - 09:00
|
Session 5. Virtual testing of aircraft hydraulic systems |
|
|
09:00 - 09:30
|
Session 5. Automated measurement of backlash and stiffness in electro-mechanical flight control actuation |
|
|
09:30 - 10:00
|
Session 5. Methodologies and test-rig configurations for the experimental improvement of aerospace flight control actuation systems |
|
|
10:00 - 10:30
|
Session 5. Flight control system architecture comprehensive evaluation based on electrical actuators for more electric aircraft |
|
|
10:30 - 11:00
|
Coffee break and poster display |
|
|
11:00 - 11:30
|
Session 6. EMADEF: a fully comprehensive analytical tool for the initial design of electro-mechanical servo-actuators for primary flight controls |
|
|
11:30 - 12:00
|
Session 6. Optimization of primary flight control actuation system using parametric sizing models of actuators, power electronics and structural analysis |
|
|
12:00 - 12:30
|
Session 6. Power cycling reliability and thermal performances of SiC power modules |
|
|
12:30 - 14:00
|
Lunch |
|
|
14:00 - 14:30
|
Session 7. Challenges of ball screw lifetime calculation in primary flight control applications |
|
|
14:30 - 15:00
|
Session 7. High fidelity model for efficiency calculation of ball screws for flight control actuators |
|
|
15:00 - 15:30
|
Session 7. A novel industry-oriented EMA model for ball screw optimised design including motor torque response and friction |
|
|
15:30 - 16:00
|
Coffee break and poster display |
|
|
16:00 - 16:30
|
Session 8. Development of an innovative piezo actuated flow servovalve with additive manufacturing body |
|
|
16:30 - 17:00
|
Session 8. The hydraulic infinite linear actuator applied to a high lift system |
|
|
17:00 - 17:30
|
Session 8. Implications of the use of flux-switching motors for aerospace actuation systems |
|
|
18:30 - 20:00
|
Private visit of Toulouse Museum - Private visit of Toulouse Museum |
|
|
20:00 - 23:00
|
Aperitive and banquet |
|
| Time |
Event |
(+)
|
|
08:30 - 09:00
|
Session 9. Fault-tolerant control system of the directional runway dynamics of small aircrafts with hydraulic differential brakes |
|
|
09:00 - 09:30
|
Session 9. Aircraft control using actuator current |
|
|
09:30 - 10:00
|
Session 9. Research on the operating modes and force fighting of hybrid actuation system based on EHA/SHA |
|
|
10:00 - 10:30
|
Session 9. Identifying enhancement potentials of actuation systems using a criticality index |
|
|
10:30 - 11:00
|
Coffee break |
|
|
11:00 - 11:30
|
Session 10. Highly responsive micro-EMA with regenerative recovery |
|
|
11:30 - 12:00
|
Session 10. Active/active aileron EMA system with optimised power supply architecture |
|
|
12:00 - 12:30
|
Session 10. Design considerations and test of the flight control actuators for a demonstrator for an unmanned freight transportation aircraft |
|
|
12:30 - 12:45
|
Conference closure - J-C. Maré |
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|
14:00 - 17:30
|
Tutorial. Introduction to optimization of actuation systems with opensource tools. Special registration required. Location: INSA - M. Budinger |
|
|
14:00 - 17:30
|
Tutorial. Virtual prototyping of mechanical transmission of aerospace actuators. Special registration required. Location: INSA - J-C. Maré |
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