System for aiding control of the deceleration of an aircraft...

Aeronautics and astronautics – Retarding and restraining devices – Wheel brake arrangement

Reexamination Certificate

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Details

C244S183000, C701S015000, C340S959000

Reexamination Certificate

active

07014146

ABSTRACT:
The system (1) includes braking means (2) for braking the aircraft, a braking unit (3) controlling the braking means (2) on the basis of deceleration orders, a computing unit (5) for computing deceleration orders, which determines a plurality of distance/speed pairs relating to the movement of the aircraft over a landing runway, each of said pairs indicating the speed of movement at the associated distance defined relative to the runway threshold of the landing runway, and an interface element (7) that includes means (14) displaying on a screen (15) a representation (16) of the landing runway, showing the exits, and indications illustrating the distance/speed pairs, aiding an operator in choosing one of the exits, and means (17) enabling an operator to select the chosen exit.

REFERENCES:
patent: 4122522 (1978-10-01), Smith
patent: 4454582 (1984-06-01), Cleary et al.
patent: 5375058 (1994-12-01), Bass
patent: 5499025 (1996-03-01), Middleton et al.
patent: 5519618 (1996-05-01), Kastner et al.
patent: 5539642 (1996-07-01), Wiel
patent: 5968106 (1999-10-01), DeVlieg et al.
patent: 2004/0026992 (2004-02-01), Villaume
patent: 4009668 (1991-10-01), None
patent: 4304562 (1994-08-01), None
patent: 2817979 (2002-06-01), None
Preliminary Search Report dated Mar. 11, 2003 with English translation.
“System Predicts Critical Runway Performance Parameters,” NTIS Tech Notes, US Department of Commerce, Springfield, VA, US, p. 292, XP000227031, ISSN: 0889-8464.

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