Howgozit airspeed indicator system

G - Physics – 01 – C

Patent

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Details

G01C 21/12 (2006.01) G01D 7/00 (2006.01) G01D 7/02 (2006.01) G01P 1/12 (2006.01)

Patent

CA 2202409

An aircraft instrument system that informs the pilot of whether, during the takeoff roll, the aircraft's acceleration rate is sufficient to ensure that Vl speed will be achieved at the expected time ( and, thus, distance ) ,and, if not, how far in distance the aircraft is lagging behind the required acceleration schedule.

Instrument de bord qui indique au pilote si, pendant la course au décollage, le taux d'accélération de l'aéronef est assez élevé pour permettre que la vitesse V1 soit atteinte au moment (et donc, à la distance) prévu et, sinon, de quelle distance l'aéronef est-il à court pour respecter l'accélération nécessaire.

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