AIRPLANE AND HELICOPTER INTEGRATED STANDBY EQUIPMENT SYSTEM Russian patent published in 2008 - IPC G01C21/00 

Abstract RU 2337315 C2

FIELD: aviation.

SUBSTANCE: airplane and helicopter (below - aircraft) integrated standby equipment system designed as independent assembly contains liquid-crystal display, total and static pressure probes pipeline connected to onboard total and static pressure probes, electronic calculators of total and static pressure, spatial orientation module with off-line inertial sensors calculating aircraft spatial position (pitch angle, list angle), electronic calculator of indicated airspeed, barometric height, vertical speed and number M, satellite navigator and onboard navigation system "БИНС" data receivers, onboard magnetic probe data receivers, radio facilities data receivers and braking temperature receiver, engine control system data receivers, spatial position and course calculators considering correction under satellite navigation system and "БИНС" data, course calculators with correction under magnetic probe and radio facilities data, and electronic signal converter to required shape and displaying on liquid-crystal display and onboard systems.

EFFECT: higher accuracy of calculated flight-navigating parameters, higher data volume on liquid-crystal display.

6 cl, 1 dwg

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RU 2 337 315 C2

Authors

Kozhevnikov Viktor Ivanovich

Kozitsin Vladimir Kuz'Mich

Makarov Nikolaj Nikolaevich

Novoselov Oleg Nikolaevich

Dates

2008-10-27Published

2006-04-03Filed