Abstract: A method and a device are disclosed for exchanging data between a technical management system of an aircraft and a mission management system of the aircraft, in order to permit one of the systems to determine the consequences of an event detected in the other of the systems. After at least one event has been detected in one of the technical management and mission management systems of the aircraft, at least one information item pertaining to the detected event is transmitted to the other of the technical management and mission management systems of the aircraft. The consequences of the event detected in the other of the technical management and mission management systems of the aircraft are then determined. The adaptation of at least one datum of the other of the technical management and mission management systems of the aircraft is evaluated in response to the determination.

Abstract: The invention has as its object in particular a method and a device for aiding in the diagnosis and in the decision on operation of an aircraft comprising means for detection of failures relating to the pieces of equipment thereof. After having received (400) at least one alert linked to the detection of at least one failure relating to at least one piece of equipment of the said aircraft, the said at least one alert comprising at least one indication relating to the said at least one failure, and at least one information item relating to the next mission of the said aircraft, a database comprising a minimum equipment list and operating conditions and/or limitations associated with the operation thereof is accessed.

Abstract: Disclosed is a display system for an aircraft cockpit. The display system includes a plurality of display devices, each of which comprises at least one viewing screen configured to display a display format, and a cursor management unit linked to each display device and configured for moving a cursor over sensitive objects on the viewing screens of the display devices.

Abstract: A device for control of a plurality of support subsystems in an aircraft includes a filtering unit that determines at least one command associated with at least one support subsystem of the plurality of support subsystems according to at least one context parameter. The device also includes a display unit that displays at least one representation of the at least one determined command. The at least one representation of the at least one determined command includes an indication relating to a state of the at least one support subsystem controlled by the at least one determined command. The device further includes a selection unit that selects the at least one representation. In addition, the device includes an activation unit that transmits the at least one determined command to the at least one support subsystem in response to an activation of the at least one selected representation.

Abstract: The object of the invention is in particular a method and a device for aiding in the control of systems installed on board an aircraft comprising at least one display device capable of displaying configuration parameters of the said aircraft and at least one associated acquisition device. After the state of the said aircraft has been determined (900), a plurality of elements to be displayed on the said at least one display device is selected (905), according to the said state of the said aircraft, in a predetermined set of elements comprising at least one parameter for configuration of the avionics, at least one parameter for configuration of support subsystems and at least one activatable representation of least one command of support subsystems of the said aircraft. The said plurality of elements is displayed on the said display device.

Abstract: The object of the invention is in particular a method and a device for aiding in the control of systems installed on board an aircraft comprising at least one display device capable of displaying configuration parameters of the said aircraft and at least one associated acquisition device. After the state of the said aircraft has been determined (900), a plurality of elements to be displayed on the said at least one display device is selected (905), according to the said state of the said aircraft, in a predetermined set of elements comprising at least one parameter for configuration of the avionics, at least one parameter for configuration of support subsystems and at least one activatable representation of least one command of support subsystems of the said aircraft. The said plurality of elements is displayed on the said display device.

Abstract: The object of the invention is in particular a method and a device for exchanging data between a technical management system of an aircraft and a mission management system of the said aircraft, in order to permit one of the said systems to determine the consequences of an event detected in the other of the said systems. After at least one event has been detected (300) in one of the said technical management and mission management systems of the said aircraft, at least one information item pertaining to the said detected event is transmitted (320) to the other of the said technical management and mission management systems of the said aircraft. The consequences of the said event detected in the said other of the said technical management and mission management systems of the said aircraft are then determined (330). The adaptation of at least one datum of the said other of the said technical management and mission management systems of the said aircraft is evaluated in response to the said determination step.

Abstract: The object of the invention is in particular a device for control of a plurality of support subsystems in an aircraft. This device comprises filtering means capable of determining at least one command associated with at least one support subsystem of the said plurality of support subsystems according to at least one context parameter, and means for displaying at least one representation (405, 410) of the said at least one determined command. The device additionally comprises selecting means capable of selecting the said at least one representation and activating means capable of transmitting the said at least one command to the said at least one support subsystem in response to the activation of the said at least one selected representation.

Abstract: The invention has as its object in particular a method and a device for aiding in the diagnosis and in the decision on operation of an aircraft comprising means for detection of failures relating to the pieces of equipment thereof. After having received (400) at least one alert linked to the detection of at least one failure relating to at least one piece of equipment of the said aircraft, the said at least one alert comprising at least one indication relating to the said at least one failure, and at least one information item relating to the next mission of the said aircraft, a database comprising a minimum equipment list and operating conditions and/or limitations associated with the operation thereof is accessed.

Abstract: The display system (1) comprises means for determining the geographic position of a cursor (CU) on a screen (3A), means for transmitting this geographic position, and means for displaying on at least one other screen (3C) a characteristic symbol (S1) which is located in this geographic position.

Abstract: A device for aiding the visual spotting of a second aircraft in flight by the pilot of a first aircraft looking at the sky through the canopy may include an approximately vertical display device and a first device that displays on the display device a representation of the canopy. A communication device receives position information relating to the second aircraft from an outside source. Using the received position information, a second device displays on the display device a symbol representative of the second aircraft such that the position of the symbol in relation to the displayed representation of the canopy corresponds to the position of the second aircraft in relation to the aircraft's canopy as seen through the pilot's field of view.

Abstract: Device for aiding the visual spotting of an aircraft in flight from another aircraft, also in flight.

Abstract: The control device (1) comprises at least one first and one second control system (4, 5) which comprises control elements (A1 to A8, B1 to B6) actuable by an operator, so as to control the monitoring system (2). These first and second control systems (4, 5) are in interaction so that an actuation of a control element of one of the control systems (4, 5) automatically brings about an action on a control element of the other control system (5, 4) which is intended to control the same function (F1 to F6) in such a way as to bring it into a control state representative of the controlled state of this function (F1 to F6).

Abstract: The method provides for an information presentation (IF1) to be presented on a visual-display screen (5), the information representing at least one vertical plane along a theoretical flight trajectory of the aircraft, and which includes an axis system (8, 9), in which a y-axis (8) is graduated in altitude, and an x-axis (9) is graduated in distance from the position of the aircraft, a particular symbol (7) representing the aircraft, which is arranged on the y-axis (8) at a position representative of the altitude of said aircraft, and a first plot (T1) representing a theoretical flight trajectory of said aircraft in the vertical plane. Said information presentation (IF1) further includes at least one second plot (T2) corresponding to a safety altitude, and a third plot (T3) corresponding to a contour of the terrain (10) in the vertical plane.

Abstract: Device for controlling a system for monitoring the environment of an aircraft, in particular of a transport aircraft.