Aircraft flight instrument display system

Communications: electrical – Land vehicle alarms or indicators – Internal alarm or indicator responsive to a condition of the...

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340 27NA, 340724, 340734, 340747, 340750, G06K 1520

Patent

active

041491483

ABSTRACT:
Apparatus for providing an integrated display of flight instrument parameters on the screen of a single cathode ray tube is presented. The synthetically generated symbology is equivalent to that typically provided by ten conventional electromechanical instruments including an attitude-director indicator, horizontal situation indicator, pressure altimeter, radio altimeter, vertical speed indicator, radio magnetic indicator, Mach airspeed indicator, autopilot-flight director mode annunciator, load factor indicator and true air-speed indicator.

REFERENCES:
patent: 3396377 (1968-08-01), Strout
patent: 3668622 (1972-06-01), Gannett et al.
patent: 3899662 (1975-08-01), Kreeger et al.

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