Aircraft propulsion control system

Details Aircraft propulsion control system Aircraft propulsion control system

1990-09-11

1992-08-11

Casaregola, Louis J.

Power plants

Reaction motor

Condition responsive thrust varying means

60 3924, F02C 900

Patent

active

051368412

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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Banbury, "Boeing 757/767 Flight Management Computer System", Proceedings of The IEEE 1980 National Aerospace and Electronics Conference 1980, pp. 177-179.

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