Abstract: The aeroplane includes at least a fuselage, two wings, a rear tail unit including a horizontal tail provided with two tail ends, and at least two engines arranged on the fuselage on either side of a vertical plane of symmetry of the aeroplane. The aeroplane has a longitudinal axis. The engines are mounted so as to be able to be displaced, at least in flight, on the fuselage, substantially parallel to the longitudinal axis, and the tail ends are mounted so as to be able to be pivoted, at least in flight, relative to the horizontal tail. The aeroplane thus has a configuration that changes in flight.

Abstract: A device for maneuvering ground support equipment on an airport stand. Included in the device are a moving apparatus having a system for coupling with the ground support equipment, configured for maneuvering the ground support equipment according to a predetermined trajectory; and a remote control configured for remotely controlling the movements of the moving apparatus according to the predetermined trajectory. The device also relates to an item of ground support equipment on an airport stand which includes a connecting plate configured for being coupled to a moving apparatus of the device.

Abstract: A cargo compartment configured to be installed in an aircraft and to accommodate a plurality of cargo receiving devices is provided. The cargo compartment surrounds a compartment interior space, and includes a floor structure arrangement having a floor surface facing the compartment interior space and configured to support cargo receiving devices loaded into the cargo compartment. The cargo compartment includes two opposite side walls extending laterally of the floor structure arrangement away from the floor surface, and the side walls include an entrance opening for access to the compartment interior space. The floor structure arrangement also includes an air cushion device having a plurality of cushion nozzles distributed in the floor surface, and the cushion nozzles are configured to blow air up from the floor surface in a direction perpendicular to the floor surface.

Abstract: A device for maneuvering and immobilizing an aircraft on the ground. Included in the device is a moving apparatus and a remote control configured for remotely controlling the moving apparatus. The device allows a coupling of a single remote control with several moving apparatuses and/or of one moving apparatus with several remote controls. Also, the device allows an operator equipped with a remote control to remotely control several pushback maneuvers by successively using several moving apparatuses or several operators each equipped with a remote control to successively control the same moving apparatus.

Abstract: A device for maneuvering ground support equipment on an airport stand. Included in the device are a moving apparatus having a system for coupling with the ground support equipment, configured for maneuvering the ground support equipment according to a predetermined trajectory; and a remote control configured for remotely controlling the movements of the moving apparatus according to the predetermined trajectory. The device also relates to an item of ground support equipment on an airport stand which includes a connecting plate configured for being coupled to a moving apparatus of the device.

Abstract: A system for loading and unloading a cargo compartment of a vehicle, such as an aircraft, with a cargo receiving device is provided. The system includes a cargo receiving device including a base structure arrangement having a horizontal lower contact surface, and a locking mechanism configured to engage one or more corresponding holding members provided in a cargo compartment of a vehicle. The system also includes a transport device including a horizontal upper contact surface configured to be disposed in abutting contact to said lower contact surface, a drive unit configured to initiate horizontal movement of the transport device, a lift unit configured to initiate vertical movement of the upper contact surface, and an actuating unit configured to actuate the locking mechanism of the cargo receiving device.

Abstract: A system for loading and unloading a cargo compartment of a vehicle, such as an aircraft, with a cargo receiving device is provided. The system includes a cargo receiving device including a base structure arrangement having a horizontal lower contact surface, and a locking mechanism configured to engage one or more corresponding holding members provided in a cargo compartment of a vehicle. The system also includes a transport device including a horizontal upper contact surface configured to be disposed in abutting contact to said lower contact surface, a drive unit configured to initiate horizontal movement of the transport device, a lift unit configured to initiate vertical movement of the upper contact surface, and an actuating unit configured to actuate the locking mechanism of the cargo receiving device.

Abstract: A cargo compartment configured to be installed in an aircraft and to accommodate a plurality of cargo receiving devices is provided. The cargo compartment surrounds a compartment interior space, and includes a floor structure arrangement having a floor surface facing the compartment interior space and configured to support cargo receiving devices loaded into the cargo compartment. The cargo compartment includes two opposite side walls extending laterally of the floor structure arrangement away from the floor surface, and the side walls include an entrance opening for access to the compartment interior space. The floor structure arrangement also includes an air cushion device having a plurality of cushion nozzles distributed in the floor surface, and the cushion nozzles are configured to blow air up from the floor surface in a direction perpendicular to the floor surface.