Navigabilité des aéronefs

Aicraft Systems

Objectives

To study the various types of systems (e.g. hydraulic system) which exist on an aircraft, in consideration of the concepts of safety, by providing multiple networks.

Educational content

Air systems - General :

Air production.

Air conditioning (thermal budgets, temperature control, forthcoming changes, weight and balance).

Cabin pressurisation.

Ventilation of electronic systems.

General distribution (cockpit, cabin, baggage compartments and bays; problems concerning comfort, humidity, filtration, ozone, etc.).

Anti-icing - Presentation of control / indication and parameters in the cockpit.

Hydraulic systems :

Performance objectives, safety and maintenance (with their consequences on the choice of general architecture).

Resulting general architecture.

Design of a system.

Integration tests on a global test bed.

Presentation of control / indication and parameters in the cockpit.

Accessories, fluids used.

Forthcoming changes.

Landing gear systems :

Retraction / extension systems.

Nose-wheel steering.

Braking system.

Pilot presentation.

Electrical systems :

Performance and safety objectives (with effects on the choice of general architecture - redundancy and segregation).

Resulting architecture.

Presentation in the cockpit - Equipment and accessories.

Fuel systems :

System functions.

Tanks (design and problems).

The different systems.

Gauging system.

Pilot presentation.

Fuel specifications.

Installation of equipment and accessories. Equipment and accessories.

Visits :

Visit of the Centre d'Essais Aéronautique de Toulouse.

Visit of Liebherr Aerospace Toulouse.

For information only  : 27 hours

Participates

Engineers and executives.
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