Abstract: The enhanced flight vision system of an aircraft comprises an image acquisition system provided to acquire images of an outside environment of the aircraft, and a display system configured to allow information to be displayed on a display unit overlayed with the outside environment of the aircraft. The display system is configured to receive images produced by the image acquisition system and to display these images on the display unit. The image acquisition system is configured to associate ancillary information with at least a part of the images produced and the display system is configured to check the integrity of an image received from the image acquisition system, based on the ancillary information associated with that image; and in the absence of integrity, deactivate the display on the display unit of at least the image received from the image acquisition system.

Abstract: An enhanced flight vision system for an aircraft includes an image acquisition system configured to acquire images of the surroundings outside the aircraft and a display system configured to receive images produced by the image acquisition system and to display these images on a display in the cockpit of the aircraft. The display system is configured to acquire information about the flight path angle of the aircraft when approaching a runway, to calculate a difference between the flight path angle of the aircraft and a nominal angle and to deactivate the display of the images received from the image acquisition system on the display when the absolute value of the difference is greater than a first angular value.

Abstract: A desensitization device includes an acquisition module for acquiring the current flight parameters of the aircraft, a generation module for generating a first image depicting flight symbology including at least one reference zero pitch line, a generation module for generating a second image depicting topography of terrain overflown by the aircraft, a generation module for generating a third image including at least two portions separated by a separating line, a generation module configured to generate a fourth image by superposing the first image, the second image and the third image in that order, the first image being placed in the foreground, and a transmission module configured to transmit, to a user device, a signal that is representative of the fourth image.

Abstract: The enhanced flight vision system of an aircraft comprises an image acquisition system provided to acquire images of an outside environment of the aircraft, and a display system configured to allow information to be displayed on a display unit overlayed with the outside environment of the aircraft. The display system is configured to receive images produced by the image acquisition system and to display these images on the display unit. The image acquisition system is configured to associate ancillary information with at least a part of the images produced and the display system is configured to check the integrity of an image received from the image acquisition system, based on the ancillary information associated with that image; and in the absence of integrity, deactivate the display on the display unit of at least the image received from the image acquisition system.

Abstract: An enhanced flight vision system for an aircraft includes an image acquisition system configured to acquire images of the surroundings outside the aircraft and a display system configured to receive images produced by the image acquisition system and to display these images on a display in the cockpit of the aircraft. The display system is configured to acquire information about the flight path angle of the aircraft when approaching a runway, to calculate a difference between the flight path angle of the aircraft and a nominal angle and to deactivate the display of the images received from the image acquisition system on the display when the absolute value of the difference is greater than a first angular value.

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 desensitization device includes an acquisition module for acquiring the current flight parameters of the aircraft, a generation module for generating a first image depicting flight symbology including at least one reference zero pitch line, a generation module for generating a second image depicting topography of terrain overflown by the aircraft, a generation module for generating a third image including at least two portions separated by a separating line, a generation module configured to generate a fourth image by superposing the first image, the second image and the third image in that order, the first image being placed in the foreground, and a transmission module configured to transmit, to a user device, a signal that is representative of the fourth image.

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 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.