Control system for the nacelle of a turboreactor

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

Reexamination Certificate

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Details

C060S226200

Reexamination Certificate

active

07954759

ABSTRACT:
The invention relates to an electrical control system for the nacelle of a turboreactor, comprising a plurality of electromechanical maneuvering elements for a plurality of actuating devices embodied as auxiliary parts of the turboreactor. The invention is characterized in that the control system comprises an electronic control box comprising a plurality of control inlets to be connected to control elements, and a plurality of outlets connected to electromechanical maneuvering of the auxiliary actuating devices. The control box can translate each instruction received into an operating sequence for at least one corresponding electromechanical maneuvering element. The invention also relates to a nacelle and an aircraft provided with one such control system.

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