Flight indicator with testing means for a helicopter

Specialized metallurgical processes – compositions for use therei – Processes – Free metal or alloy reductant contains magnesium

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36455101, G01C 2100

Patent

active

059084855

ABSTRACT:
A flight indicator for an aircraft, intended to give the power margin available on at least one engine of the aircraft. The indicator includes sensors (2, 3, 4) capable of delivering data relating to various monitored parameters of the engine, means (5) of processing the data coming from the sensors (2, 3, 4), and display (6) showing the processed data relating to that parameter among the monitored engine parameters, whose current value is closest to the limiting value for the parameter. The indicator includes a testing device (12) for testing the analytical consistency between at least one of the parameters and at least one other of the parameters.

REFERENCES:
patent: 4763285 (1988-08-01), Moore et al.
patent: 4780838 (1988-10-01), Adelson
patent: 4787053 (1988-11-01), Moore et al.
patent: 5079946 (1992-01-01), Motamedi et al.
patent: 5257190 (1993-10-01), Crane
patent: 5608627 (1997-03-01), Lecomte et al.

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