Process and device for braking an aircraft by seeking an optimal

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303 93, G06F 1550

Patent

active

044046332

ABSTRACT:
The present invention relates to a process and device for braking an aircraft taxiing on the ground after landing and comprising a plurality of braked wheels, by seeking a maximum coefficient of adherence between said braked wheels and the ground on which they roll, wherein said braking is subdivided into a plurality of successive braking periods and each of these periods is itself divided into a first phase during which a reference sliding value is imposed on each braked wheel and the optimal sliding value of the period is determined, and into a second phase during which said optimal sliding value is imposed on all said braked wheels. The invention is applicable to the automatic braking of aircraft.

REFERENCES:
patent: 3382012 (1968-05-01), Lucien
patent: 3394967 (1968-07-01), Lucien
patent: 3702714 (1972-11-01), Branson
patent: 4180223 (1979-12-01), Amberg
patent: 4367529 (1983-01-01), Masclet et al.

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