Abstract: The control device of a communication system of an aircraft having a predefined number of communication channels comprises a processing unit and one or more sets of buttons each associated with a communication channel. The number of sets of buttons is less than the predefined number of communication channels of the communication system. The device comprises a set of call buttons comprising at least one transmission button, and a display area on a display screen, this display area being associated with the set of call buttons. The processing unit is configured to display an indication in the display area associated with the set of call buttons when the communication system receives a call on a channel with which no set of buttons is associated and to select this channel for transmission following an action of a user on the transmission button of the set of call buttons.

Abstract: A method and device for displaying a symbology for assisting the piloting of an aircraft during a landing phase. The display device allows a crew to anticipate or avoid emission of a runway overrun warning, able to be emitted by a piloting assistance unit. The display device includes a display unit to display a symbology, a module for determining characteristics of the runway and an end of runway margin, a module for determining a run distance necessary for the aircraft to attain a run speed, when the piloting assistance unit operates in a first mode, a transmission module configured for transmitting a set of signals making it possible for the display unit to display a symbol representative of the run distance, at least one symbols representative of the characteristics of the runway and a symbol representative of the end of runway margin.

Abstract: The control device of a communication system of an aircraft having a predefined number of communication channels comprises a processing unit and sets of buttons each associated with a communication channel and comprising a button for setting sound volume, a reception button and a transmission button. The number of sets of buttons is at least equal to two and less than the predefined number of communication channels of the communication system. The device comprises display areas on a display screen, a display area being associated with each set of buttons and provided to display at least the name of the communication channel associated with the set of buttons. The processing unit is configured to configure the association between each of the sets of buttons and the communication channel associated with this set of buttons according to actions of a user on at least one interactive element of the device.

Abstract: A method and device for displaying a symbology for assisting the piloting of an aircraft during a landing phase. The display device allows a crew to anticipate or avoid emission of a runway overrun warning, able to be emitted by a piloting assistance unit. The display device includes a display unit to display a symbology, a module for determining characteristics of the runway and an end of runway margin, a module for determining a run distance necessary for the aircraft to attain a run speed, when the piloting assistance unit operates in a first mode, a transmission module configured for transmitting a set of signals making it possible for the display unit to display a symbol representative of the run distance, at least one symbols representative of the characteristics of the runway and a symbol representative of the end of runway margin.

Abstract: The control device of a communication system of an aircraft having a predefined number of communication channels comprises a processing unit and sets of buttons each associated with a communication channel and comprising a button for setting sound volume, a reception button and a transmission button. The number of sets of buttons is at least equal to two and less than the predefined number of communication channels of the communication system. The device comprises display areas on a display screen, a display area being associated with each set of buttons and provided to display at least the name of the communication channel associated with the set of buttons. The processing unit is configured to configure the association between each of the sets of buttons and the communication channel associated with this set of buttons according to actions of a user on at least one interactive element of the device.

Abstract: The control device of a communication system of an aircraft having a predefined number of communication channels comprises a processing unit and one or more sets of buttons each associated with a communication channel. The number of sets of buttons is less than the predefined number of communication channels of the communication system. The device comprises a set of call buttons comprising at least one transmission button, and a display area on a display screen, this display area being associated with the set of call buttons. The processing unit is configured to display an indication in the display area associated with the set of call buttons when the communication system receives a call on a channel with which no set of buttons is associated and to select this channel for transmission following an action of a user on the transmission button of the set of call buttons.

Abstract: A display system and method including screens in a cockpit of an aircraft. A control unit is configured to command the display according to a normal display mode, wherein the control unit is configured so as to command the display such that subsequent to the occurrence of an event on board the aircraft leading to the display of an interactive element in an interaction window, the control unit commands the display of the interaction window on one of the screens of the screens at least while an action by an operator is required on the interactive element, and a reconfigured display mode, wherein the control unit is configured to command the display, on a second screen including a signaling area, of a display window that is normally displayed on a first screen in the normal display mode, and to command the display of an indicator in the signaling area if the interaction window is not displayed on a screen of the screens when an action by an operator is required on the interactive element.

Abstract: An aircraft comprising a landing gear, having at least one wheel rotatably driven by an electric motor, and a motor control system. The control system comprises a control panel, presenting a first control configured to deliver a torque or power value to the motor along a direction of forward travel of the aircraft and second control configured to deliver a taxiing speed value along a direction of reverse travel, a control unit connected to the control panel and to the electric motor, presenting a first arrangement configured to control, in torque or power, the motor according to the value delivered by the first control, and a second arrangement configured to control, in speed, the motor according to the taxiing speed value delivered by the second control, and a speed sensor configured to measure the taxiing speed of the aircraft, and to transmit this speed information to the control unit.

Abstract: A method for verifying coherence of takeoff parameters of an aircraft from an airport with an available runway length at a moment of takeoff comprises a step of identifying a takeoff runway and a step of validating takeoff parameters with a view to authorizing takeoff of the aircraft if the takeoff distance is shorter than the remaining runway length associated with the identified takeoff runway.

Abstract: A method for verifying the coherence of the takeoff parameters of an aircraft from an airport with an available runway length at the moment of takeoff comprises a step (E20) of identifying a takeoff runway and a step (E30) of validating the takeoff parameters with a view to authorizing takeoff of the aircraft if the takeoff distance is shorter than the remaining runway length associated with the identified takeoff runway. Use to make takeoff of an aircraft from an airport safe.