Aircraft cabin display unit

Measuring and testing – Navigation – Take-off and landing monitors

Patent

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Details

73182, 364443, G01C 2110

Patent

active

041633873

ABSTRACT:
A cabin display unit accepts information from a plurality of sources such as the petot static tube, a static air pressure source, a temperature source, cabin pressure source and the like and converts the data to corresponding electrical valves. The valves are multiplexed and converted to a digital value and applied to a micro-processor which calculates, from the data, the aircraft's true air speed, outside temperature, altitude, etc., and displays the calculated information on a cabin display unit.

REFERENCES:
patent: 3995144 (1976-11-01), Johnson et al.

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