US 12,214,867 B2
Aircraft brake control system
Alexander Hayes, Bristol (GB); Ashley Bidmead, Bristol (GB); Thierry Storme, Bristol (GB); Robert Coombe, Bristol (GB); Mark Johnson, Bristol (GB); and Andrew Hebborn, Bristol (GB)
Assigned to AIRBUS OPERATIONS LIMITED, Bristol (GB)
Filed by AIRBUS OPERATIONS LIMITED, Bristol (GB)
Filed on Feb. 10, 2022, as Appl. No. 17/650,558.
Claims priority of application No. 2101916 (GB), filed on Feb. 11, 2021.
Prior Publication US 2022/0266992 A1, Aug. 25, 2022
Int. Cl. B64C 25/00 (2006.01); B60T 8/17 (2006.01); B60T 8/172 (2006.01); B64C 25/46 (2006.01); B64D 47/08 (2006.01)
CPC B64C 25/46 (2013.01) [B60T 8/1703 (2013.01); B60T 8/172 (2013.01); B64D 47/08 (2013.01)] 21 Claims
OG exemplary drawing
 
1. An aircraft brake control system for controlling anti-skid braking of at least first and second wheels in a wheel set of an aircraft, the system comprising a control assembly having:
wheel speed inputs including:
an input of an indication of the wheel speed of one or more wheels, and
determining a threshold value at which the one or more wheels is unlikely to skid, and
an anti-skid output for maintaining the one or more wheels within the threshold value, wherein the control assembly also has one or more inputs providing an indication of whether or not a wheel of the wheel set has skidded, and wherein the output is a selective output configured to indicate:
a wheel speed other than the lowest wheel speed, if a wheel skid is not indicated, and
the lowest wheel speed, if a wheel skid is indicated.