Aircraft takeoff acceleration indicator system

Details Aircraft takeoff acceleration indicator system Aircraft takeoff acceleration indicator system

G - Physics

01

C

G01C 23/00 (2006.01) B64D 43/02 (2006.01)

Patent

CA 2253899

An aircraft instrument system that informs the pilot of whether, during the takeoff roll, the aircraft's acceleration rate is sufficient to ensure that V1 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.

L'invention concerne un système d'instrument aéronautique informant le pilote si la vitesse d'accélération de l'aéronef durant le roulement au décollage est suffisante pour atteindre la vitesse V1 au moment voulu (et donc sur la distance voulue), et si tel n'est pas le cas, de la distance correspondant au retard de l'aéronef sur le programme d'accélération requis.

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