Abstract: A container end piece has: an inlet; an outlet; a closure device that is movable between a closed position and an open position; and a connection device for connecting the container end piece on to the tank end piece. The connecting device has: a clamping device that is movable between a spaced-apart position, in which the container end piece can be inserted around the tank end piece, and a clamped position, in which the clamping device co-operates with the tank end piece; and a control device that is actuable between a retracted position and an active position, in which the control device exerts a clamping force on the clamping device in its clamped position.

Abstract: Methods, systems, and computer readable media are disclosed for managing an aircraft's systems through a dedicated interface. One aspect of a method for implementing the subject matter described herein includes at least one interactive interface configured for managing an aircraft system, displaying at least one or more graphic object representing at least one or more system component, displaying at least one or more energy flow icon representing the direction of circulation of an energy flow, and interacting with the at least one or more system component through a user action on the at least one or more graphic object.

Abstract: Methods, systems, and computer readable media are disclosed for managing an aircraft's systems through a dedicated interface. One aspect of a method for implementing the subject matter described herein includes at least one global visualization interface for managing aircraft systems and including a hardware processor. The method also includes displaying at least one or more graphic object representing at least one or more aircraft system, displaying at least one or more energy flow icon representing the direction of circulation of an energy flow, and accessing a system management interface of at least one or more aircraft system through performing an user interaction with the graphic object.

Abstract: Methods, systems, and computer readable media are disclosed for troubleshooting and repairing an aircraft system failure during abnormal situations of an aircraft's operation. One aspect of a method for implementing the subject matter described herein includes at least one interactive interface configured for troubleshooting and repairing an aircraft system failure. The method also includes displaying at least one or more graphic object representing at least one or more aircraft system and configured for receiving interaction from a user, displaying at least one or more energy flow icon representing the direction of circulation of an energy flow, and displaying at least one or more macro action icon configured for performing an automated action sequence configured for troubleshooting and repairing the system failure.

Abstract: Methods, systems, and computer readable media are disclosed for managing an aircraft's systems through a dedicated interface. One aspect of a method for implementing the subject matter described herein includes at least one interactive interface configured for managing an aircraft system, displaying at least one or more graphic object representing at least one or more system component, displaying at least one or more energy flow icon representing the direction of circulation of an energy flow, and interacting with the at least one or more system component through a user action on the at least one or more graphic object.

Abstract: Methods, systems, and computer readable media are disclosed for troubleshooting and repairing an aircraft system failure during abnormal situations of an aircraft's operation. One aspect of a method for implementing the subject matter described herein includes at least one interactive interface configured for troubleshooting and repairing an aircraft system failure. The method also includes displaying at least one or more graphic object representing at least one or more aircraft system and configured for receiving interaction from a user, displaying at least one or more energy flow icon representing the direction of circulation of an energy flow, and displaying at least one or more macro action icon configured for performing an automated action sequence configured for troubleshooting and repairing the system failure.

Abstract: Methods, systems, and computer readable media are disclosed for managing an aircraft's systems through a dedicated interface. One aspect of a method for implementing the subject matter described herein includes at least one global visualization interface for managing aircraft systems and including a hardware processor. The method also includes displaying at least one or more graphic object representing at least one or more aircraft system, displaying at least one or more energy flow icon representing the direction of circulation of an energy flow, and accessing a system management interface of at least one or more aircraft system through performing an user interaction with the graphic object.