Method and controller for an aircraft
AssigneeAirbus Operations GmbH
InventorsAndrew BILL, Michael ORFORD, Sukhpreet BLACK, Rodrigo JIMENEZ
Life of this patent
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Abstract
A computer-implemented method comprising determining, based on a first signal indicative of a pressure in a tire of a wheel of an aircraft and a second signal indicative of a deformation of the tire, a determined load on the wheel, and causing an action to be performed based on the determined load on the wheel. Also a system for an aircraft, the system comprising a monitoring system configured to detect pressure and deformation of a tire of a wheel of the aircraft, and a controller configured to determine, on the basis of the pressure and deformation detected by the monitoring system, load on the wheel.
Claims23
A computer-implemented method comprising:
- determining, based on a first signal indicative of a pressure in a tire of a wheel of an aircraft and a second signal indicative of a deformation of the tire, a determined load on the wheel, and
- causing an action to be performed based on the determined load on the wheel.
A system for an aircraft, the system comprising:
- a monitoring system configured to detect a pressure and a deformation of a tire of a wheel of the aircraft, and
- a controller configured to determine, based on the pressure and the deformation detected by the monitoring system, load on the wheel,
- wherein the system is configured to cause an action to be performed based on the load on the wheel determined by the controller.
Dependencies are inferred from the claim text.