Abstract: According to an exemplary embodiment of the present invention, a diagnosis system for detecting a state of emergency during assembly of a fuselage (101) of an airplane is provided, which is adapted for detecting an emergency event and outputting information relating to the actual position of the emergency event. This may provide for a fast error identification during airplane assembly.

Abstract: A method for the mounting and alignment of a component supported in a supporting device at a plurality of support points in a desired orientation, wherein an elastic deformation of at least one deformation zone of the supporting device is registered, and from a certain deviation from a desired value of the at least one deformation zone is traversed orthogonally relative to at least one support point. Also a supporting device for purposes of executing such a method, which has at least one elastically deformable deformation zone, a measurement device for purposes of registering and evaluating the at least one elastic deformation, and at least one actuator for purposes of traversing the support points orthogonally relative to one another.

Abstract: The invention relates to a vibrating rivet tool for pressing and fixing rivets in component holes in component of aircraft. The vibrating rivet tool comprises a rivet receptacle and a drive unit for producing a high static pressing force. According to the invention, the static pressing force is superimposed by a mechanical vibration, of which the amplitude acts substantially in the direction of a longitudinal axis of the rivet. As a result, the force necessary to press and fix the rivet in a component hole is reduced in such a way that the overall size and mass of the vibrating rivet tool according to the invention are smaller/lower in comparison with conventional rivet tools. Due to the small overall size and low weight, the vibrating rivet tool can more easily be integrated in automated riveting processes.

Abstract: A positioning system is provided for mounting a wing of an aircraft to a fuselage of the aircraft. The positioning system includes, but is not limited to a programmable mounting unit that can perform a final adjustment and alignment of the wing with respect to the fuselage without user interaction.

Abstract: A positioning system is provided for mounting a wing of an aircraft to a fuselage of the aircraft. The positioning system includes, but is not limited to a programmable mounting unit that can perform a final adjustment and alignment of the wing with respect to the fuselage without user interaction.

Abstract: According to an exemplary embodiment of the present invention, a diagnosis system for detecting a state of emergency during assembly of a fuselage (101) of an airplane is provided, which is adapted for detecting an emergency event and outputting information relating to the actual position of the emergency event. This may provide for a fast error identification during airplane assembly.

Abstract: The invention relates to a vibrating rivet tool for pressing and fixing rivets in component holes in component of aircraft. The vibrating rivet tool comprises a rivet receptacle and a drive unit for producing a high static pressing force. According to the invention, the static pressing force is superimposed by a mechanical vibration, of which the amplitude acts substantially in the direction of a longitudinal axis of the rivet. As a result, the force necessary to press and fix the rivet in a component hole is reduced in such a way that the overall size and mass of the vibrating rivet tool according to the invention are smaller/lower in comparison with conventional rivet tools. Due to the small overall size and low weight, the vibrating rivet tool can more easily be integrated in automated riveting processes.

Abstract: The invention relates to a flexible assembly for performing work on large surfaces. The invention comprises a mobile assembly which supports a working head and which is equipped with movement systems (1) comprising a fixing system (2) and a traction system which act in an independent or synchronised manner, such that the assembly can move in steps across the application surface.

Abstract: A system element for the transporting and positioning of a tool on a surface of a workpiece, includes at least one suction device that generates a suction stream, and a transport device that is arranged around the suction device, and includes: at least two rollers that are rotatably supported on the suction device, connection elements that interconnect respective end regions of various rollers, and the rollers and the connection elements are elastically deformable, and when there is a suction stream, the system element substantially conforms with the surface of the workpiece.

Abstract: A system element for the transporting and positioning of a tool on a surface of a workpiece, includes at least one suction device that generates a suction stream, and a transport device that is arranged around the suction device, and includes: at least two rollers that are rotatably supported on the suction device, connection elements that interconnect respective end regions of various rollers, and the rollers and the connection elements are elastically deformable, and when there is a suction stream, the system element substantially conforms with the surface of the workpiece.