Aircraft propulsion control system

Power plants – Reaction motor – Interrelated reaction motors

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Details

60233, 60 3915, 60 3924, F02C 928

Patent

active

050441558

ABSTRACT:
Integration of engine functions and data communications between an aircraft propulsion module and an airframe is enabled by the use of fiber optic links which multiplex information and control functions without risk of an electrical failure in one portion of the aircraft electronics system propagating to other portions of the aircraft electronic systems.

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