Method for managing the wheel steering control of an aircraft

Aeronautics and astronautics – Aircraft propulsion and steering on land or water

Reexamination Certificate

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Details

C244S051000, C244S099200, C244S10000R, C244S10300W, C244S183000, C244S184000

Reexamination Certificate

active

07731122

ABSTRACT:
The invention relates to a method for managing a steering control of an aircraft landing gear provided with at least one wheel steerable by the steering control, comprising the following steps:monitoring one or several taxi parameter(s) (51, 54, 64, 59, 61) of the aircraft to determine whether said aircraft enters a towing situation,setting the steering control in a free steering mode of the steerable wheel, if the aircraft enters the towing situation;activating the steering control so that the steerable wheel has an angular controlled steering by the steering control if the aircraft leaves said towing situation.

REFERENCES:
patent: 2919933 (1960-01-01), Olson
patent: 4007890 (1977-02-01), Bremer et al.
patent: 4113041 (1978-09-01), Birkeholm
patent: 4923253 (1990-05-01), Pollner et al.
patent: 4991862 (1991-02-01), Tsao et al.
patent: 5219033 (1993-06-01), Pollner et al.
patent: 5381987 (1995-01-01), Carns
patent: 5513821 (1996-05-01), Ralph
patent: 6305484 (2001-10-01), Leblanc
patent: 6928363 (2005-08-01), Sankrithi
patent: 1 342 645 (2003-09-01), None
patent: 837 891 (1960-06-01), None

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