Standby instrument for aircraft

Details Standby instrument for aircraft Standby instrument for aircraft

G - Physics

01

C

G01C 23/00 (2006.01) G01P 13/00 (2006.01)

Patent

CA 2693145

The invention relates to a standby instrument for the piloting of aircraft allowing a pilot to restore a display similar to that of a head-up display in the event that the latter should fail. According to the invention, the standby instrument comprises means for determining and displaying a speed vector (11) of the aircraft only with the aid of means usually present in a standby instrument, namely means for measuring static and total pressures of the airstream surrounding the aircraft and means for inertial measurement.

L'invention concerne un instrument de secours pour le pilotage d'aéronefs permettant à un pilote de retrouver un affichage semblable à celui d'un affichage tête haute en cas de panne de celui-ci. Selon l'invention, l'instrument de secours comporte des moyens pour déterminer et afficher un vecteur vitesse (11) de l'aéronef uniquement à l'aide des moyens généralement présents dans un instrument de secours, à savoir des moyens de mesure des pressions statique et totale du flux d'air entourant l'aéronef ainsi que de moyens de mesure inertielle.

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