Control device and method for an aircraft
AssigneeAirbus Operations GmbH
InventorsAshley Bidmead, Mark Johnson
Life of this patent
Estimating the term…
Abstract
A control device for an aircraft is disclosed including a push-button switch that is configured to be held in a depressed position by a pilot during taxiing of the aircraft. The push-button switch is configured to return automatically to a released position if it is not held in the depressed position by the pilot. The control device is configured to output a command for braking to a braking system of the aircraft, if the push-button switch moves to the released position during taxiing of the aircraft and does not return to the depressed position within a set time. The button may be provided on a tiller. A method of detecting on-board pilot incapacitation during an aircraft taxi phase is also disclosed.
Claims17
A control device for an aircraft, the aircraft including a braking system, the control device comprising:
- a manually operable push-button switch movable from a released position to a depressed position,
- the push-button switch being configured to return to the released position if it is not manually held in the depressed position,
- the push-button switch being configured to be held by a pilot in the depressed position during a taxi phase of the aircraft,
- the control device being arranged, in response to the push-button switch moving to the released position during the taxi phase, to output a signal which causes a braking command to be issued, after a set time has passed without the push-button switch being returned to the depressed position.
An aircraft, comprising:
- a control system,
- a braking system,
- a steering tiller, and
- a sensor located on the steering tiller for detecting whether or not the steering tiller is being gripped,
- the control system being arranged to receive a signal from the sensor indicating whether the steering tiller is being gripped during an aircraft taxi phase, and to output a command for braking to the braking system in response, in the event that the steering tiller is not being gripped for a set time period.
A method of modifying an existing aircraft to make it more suited to single-pilot operations, the aircraft having a sensor on a steering tiller with a primary function, the method comprising:
- adapting the sensor to have a secondary function specific to single pilot operations;
- adding a secondary indicator to the sensor to indicate the functionality of the sensor to flight crew;
- and
- installing software on a system of the aircraft such that when installed the system of the aircraft detects the state of the sensor allowing the sensor to perform the secondary function during taxiing and single pilot operations.
A method of detecting on-board pilot incapacitation during an aircraft taxi phase, comprising:
- a switch automatically moving to a released position if it is not held in a depressed position by the on-board pilot;
- detecting that the switch has moved from the depressed position;
- waiting for a specified time period, before one of
- (a) the switch returning to the depressed position before the end of the time period;
- or
- (b) as a consequence of the switch not being in the depressed position throughout the time period, the method further comprises outputting a command to a braking system of the aircraft for braking.
Dependencies are inferred from the claim text.