Method of managing brake system architecture for an airplane...

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Indication or control of braking – acceleration – or deceleration

Reexamination Certificate

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C701S078000, C188S156000, C303S009620

Reexamination Certificate

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06954692

ABSTRACT:
The invention relates to a method of managing a braking system architecture for an airplane fitted with brakes having electromechanical actuators, in which some of the actuators are connected to a battery assembly of the airplane and other actuators are not connected to the battery assembly of the airplane, which method comprises a step of controlling at least one of the actuators that is not connected to the battery assembly to cause it to exert a force equal to a unit holding force, which force is determined independently of any braking demand from the pilot. The invention also provides an architecture specially adapted to implement the method.

REFERENCES:
patent: 5961190 (1999-10-01), Brandmeier et al.
patent: 6081081 (2000-06-01), Maisch
patent: 6138801 (2000-10-01), Shirai et al.
patent: 6142026 (2000-11-01), Ohashi et al.
patent: 6219033 (2001-04-01), Rosenberg et al.
patent: 6402259 (2002-06-01), Corio et al.
patent: 2001/0045771 (2001-11-01), Corio et al.

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