Abstract: A device for painting a curved outer surface of an aircraft includes a paint applicator having a plurality of spray painting heads each assigned to one of a plurality of different base color supply units containing one of polyurethane aircraft paint and ink. The device further includes a spatially adjustable positioning device configured to move the paint applicator relative to the curved outer surface and at least one sensor device configured to determine a three-dimensional geometry of the curved outer surface. The device also includes a control unit configured to coordinate a movement of the positioning device with a paint output of the paint applicator, wherein the control unit is configured to alternately activate each of the plurality of spray painting heads so as to produce a picture motif so as to derive a two-dimensional driving geometry based on the three-dimensional geometry.

Abstract: A device for painting a curved outer surface of an aircraft includes a paint applicator having a plurality of spray painting heads each assigned to one of a plurality of different base color supply units containing one of polyurethane aircraft paint and ink. The device further includes a spatially adjustable positioning device configured to move the paint applicator relative to the curved outer surface and at least one sensor device configured to determine a three-dimensional geometry of the curved outer surface. The device also includes a control unit configured to coordinate a movement of the positioning device with a paint output of the paint applicator, wherein the control unit is configured to alternately activate each of the plurality of spray painting heads so as to produce a picture motif so as to derive a two-dimensional driving geometry based on the three-dimensional geometry.

Abstract: A method for accelerated drying of at least one polymer which is located at least partially on a component, in particular at least a layer of paint and/or a sealing agent which is applied to an aircraft component in particular with a different material composition, involving the following steps of: a) at least partially applying the at least one polymer, in particular an epoxy resin and/or polyurethane-based layer of paint and/or a sealing agent, to an upper side of the component, and b) at least partially drying the polymer by means of electromagnetic radiation with a wavelength range of between 0.28 ?m and 4.0 ?m. Accelerated drying of the polymer, in particular the paint layer thereby becomes possible from an upper side of the component to an upper side of the paint layer.

Abstract: A method for final assembly of at least two aircraft includes assembling the at least two aircraft in a transverse direction on a carousel, the at least two aircraft disposed side-by-side, and rotating the carousel on a vertical rotation axis 360°.

Abstract: A device for pretreating an exterior surface of an aircraft coated with an aircraft-specific base material so as to prepare the surface for a final painting with aircraft paint includes a pretreating tool. The pretreating tool has a laser head configured to activate the aircraft-specific base material using a laser. The device also includes a support construction including a robot device and a control unit configured to control and move the laser head over the surface using the robot device.

Abstract: A method for plasma treatment and painting of a surface, the surface including a plurality of different materials includes blasting the surface with a carbon dioxide snow so as to activate the surface to improve an adhesive strength; and treating the surface with a plasma treatment using at least one plasma nozzle following the blasting step, the treating including guiding the at least one plasma nozzle at a distance of not more than 15 mm from the surface at a feed rate of not more than 50 m/min.

Abstract: The invention relates to a device for applying information onto a surface of an aircraft, wherein the information is applicable in variable locations and is modifiable. The device can include a pad unit having at least one pad, at least one hand grip, a press-on mechanism, a hand lever, at least one support, and a housing. By applying varying printing patterns to the pads, any combination of characters can be stamped on. Moreover, the device configured as a hand-held tool can be operated by a user in variable locations. The printing process is effected by operating the hand lever, causing the pads to be brought into contact with the surface, and the information or, as the case may be, the technical coding to be applied onto said surface.

Abstract: A device for positional fixation of a first fuselage section to be joined onto a second one in a butt-join region, the first fuselage section being planked with a first skin and the second fuselage section being planked with a second skin. The fuselage sections are temporary connectable by at least one clamping element in the butt-join region for carrying out a joining process. The clamping elements are each formed with a holder and a counter holder, wherein for example the holders are positioned exteriorly on the second skin while the counter holders are positioned interiorly on an interior side of the first skin opposite in the butt-join region. Each holder comprises at least one magnet for temporarily fixing the fuselage sections to one another and preventing intrusion of bore chips in-between the skins and/or, as the case may be, a butt-join strap by use of the magnetic force of attraction toward the counter holder.

Abstract: A method for final assembly of at least two aircraft includes assembling the at least two aircraft in a transverse direction on a carousel, the at least two aircraft disposed side-by-side, and rotating the carousel on a vertical rotation axis 360°.

Abstract: A device for pretreating an exterior surface of an aircraft coated with an aircraft-specific base material so as to prepare the surface for a final painting with aircraft paint includes a pretreating tool. The pretreating tool has a laser head configured to activate the aircraft-specific base material using a laser. The device also includes a support construction including a robot device and a control unit configured to control and move the laser head over the surface using the robot device.

Abstract: A processing device for coating a surface of a rudder unit of an aircraft includes a plurality of spatially delimited work stations, wherein each of the plurality of work stations are disposed in succession and are configured to produce an assembly line-like coating process, wherein the plurality of work stations. The work stations include a pretreating station configured to activate the surface so as to form an activated surface; a painting station disposed downstream of the pretreating station and configured to paint the activated surface with at least one layer of paint having a first color so as to form a painted surface and configured to dry the painted surface immediately after the painting; and a decorating station.

Abstract: A device for painting a curved outer surface of an aircraft includes a paint applicator having a plurality of spray painting heads each assigned to one of a plurality of different base color supply units containing one of polyurethane aircraft paint and ink. The device further includes a spatially adjustable positioning device configured to move the paint applicator relative to the curved outer surface and at least one sensor device configured to determine a three-dimensional geometry of the curved outer surface. The device also includes a control unit configured to coordinate a movement of the positioning device with a paint output of the paint applicator, wherein the control unit is configured to alternately activate each of the plurality of spray painting heads so as to produce a picture motif so as to derive a two-dimensional driving geometry based on the three-dimensional geometry.

Abstract: A method for plasma treatment and painting of a surface, the surface including a plurality of different materials includes blasting the surface with a carbon dioxide snow so as to activate the surface to improve an adhesive strength; and treating the surface with a plasma treatment using at least one plasma nozzle following the blasting step, the treating including guiding the at least one plasma nozzle at a distance of not more than 15 mm from the surface at a feed rate of not more than 50 m/min.

Abstract: The invention relates to a method for accelerated drying of at least one polymer which is located at least partially on a component, in particular at least a layer of paint and/or a sealing agent which is applied to an aircraft component in particular with a different material composition, involving the following steps of: a) at least partially applying the at least one polymer, in particular an epoxy resin and/or polyurethane-based layer of paint and/or a sealing agent, to an upper side of the component, and b) at least partially drying the polymer by means of electromagnetic radiation with a wavelength range of between 0.28 ?m and 4.0 ?m. Accelerated drying of the polymer, in particular the paint layer thereby becomes possible from an upper side of the component to an upper side of the paint layer, whereby high surface-quality of the painting can be achieved with processing times which are nonetheless short.

Abstract: The invention relates to a device for applying information onto a surface of an aircraft, wherein the information is applicable in variable locations and is modifiable, comprising the following features: a) a pad unit comprising at least one pad which is made of a silicone-free rubber having a shore hardness suitable for the operating conditions of the device and which is hollow on the inside, at least in part; b) at least one hand grip; c) a press-on mechanism for the pad unit; d) at least one support which rests against the surface; and e) a housing; wherein a printing pattern is formed on the at least one pad with a polyurethane lacquer containing at least two components. By applying varying printing patterns to the pads, any combination of characters can be stamped on. Moreover, the device configured as a hand-held tool can be operated by a user in variable locations. The pads are wetted fully automatically in a wetting station.