Aircraft braking control
AssigneeMeggitt Aerospace Limited
InventorMichael Clothier
Life of this patent
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AssigneeMeggitt Aerospace Limited
InventorMichael Clothier
Estimating the term…
An aircraft braking control system for an aircraft braking system that comprises at least one first side braking unit (30L) for braking a respective wheel (22L) positioned on a first side of a longitudinal axis of an aircraft and at least one second side braking unit (30R) for braking a respective wheel (22R) positioned on a second side of said longitudinal axis, said braking control system comprising a brake control unit (40) operable to process respective measurements of performance of the braking units (30L, 30R) and according to the process results to provide command signals for controlling respective braking forces applied by said first and second braking units (30L, 30R) to reduce any difference between a first side braking force applied on the first side of the longitudinal axis by said at least one first side braking unit (30L) and a second side braking force applied on said second side by said at least one second side braking unit (30R).
1-50. (canceled)
Apparatus for controlling an aircraft braking system that comprises at least one first side braking means for braking a wheel positioned on a first side of a longitudinal axis of an aircraft and at least one second side braking means for braking a wheel positioned on a second side of the longitudinal axis, said apparatus comprising control means for processing respective indications of braking effect of the braking means and in response to the result of said processing issuing control signals for controlling braking forces applied by the braking means, said indications of braking effect being determined based on wheel speed of the respective wheel and an aircraft speed value obtained without reference to wheel speed, each indication of braking effect comprising a brake slip ratio calculated using the equation:
A method of controlling brakes on an aircraft having at least one first side braking unit for braking a respective wheel positioned on a first side of a longitudinal axis of an aircraft and at least one second side braking unit for braking a respective wheel positioned on a second side of the longitudinal axis, said method comprising processing respective measurements of performance of the braking units which are calculated using a wheel rotational speed for the respective wheel and an indication of aircraft speed obtained without reference to the wheel speed, the respective measurements of performance are a slip ratio being calculated using the equation:
Dependencies are inferred from the claim text.