Heidelberger Druckmaschinen Ag

Airbus Operations Gmbh

Airbus Deutschland Gmbh

Airbus Operations (s.a.s.)

Airbus (sas)

Airbus Corporation

Eckart Frankenberger

Peter Hachmann

G&uuml;nter Stephan

Karl-Heinz Helmst&auml;dter

Michael Gieser

Christian Hieb

Ruben Schmitt

Christian G&ouml;rbing

Holger Frauen

Peter Thoma

Hans-Peter Hiltwein

Uwe Fischer

Werner Weber

Christian Görbing

Eike Klemkow

Ludwig Becker

Heinz-Detlef Naeve

Peter Konstanzer

Dirk Gross

Andrew Booth

Oliver Kraatz

Horst Zapp

Matthias Meussen

Gerhard Muller

Thorsten Bergemann

A system for positioning vehicle components relative to each other on a floor to prepare an assembly. A plurality of carriers receive a vehicle component. A plurality of positioning tables have a lower portions which can be fixed to the floor and a upper portions which receive a carrier. A location device having at least one base and mobile units moveable relative to the base. At some of the positioning tables moves the respective upper portion along at least two movement axes relative to the respective lower portion to position a carrier located thereon. A transport device guides the carriers from an external position to a positioning table and to place them on the upper portion. The location device determines the positions of the respective mobile units relative to the at least one base. A position control unit controls a movement of the upper portions to a predetermined target position.

System and method for positioning vehicle components for assembly

A method for producing an aircraft fuselage for simplifying and accelerating the production of the aircraft fuselage. The method includes providing a fuselage structure which surrounds an interior space and has an inner side facing the interior space, providing an insulating panel for insulating the fuselage structure, wherein the insulating panel has an inner surface and an outer surface, providing a film which is provided with electric strip conductors, fastening the film to the inner surface of the insulating panel, and attaching the insulating panel to the inner side of the fuselage structure.

Method for producing an aircraft fuselage

A process of joining a wing to an aircraft fuselage comprising the steps of: mapping the wing root of the wing, mapping the center-wing-box (CWB) of the aircraft fuselage, determining the position to provide the hole pattern on the CWB, providing the holes on the CWB, and attaching the wing root to the CWB. Primary and secondary templates with corresponding hole patterns may be used in combination with targets and laser trackers to implement the process. The hole pattern of the wing root can therefore be duplicated on the CWB at a position such that when the wings are joined to the fuselage, the aircraft will have optimum flight performance and dynamic symmetry. A predictive fit is thus provided, based on virtual representation and analysis, and advantageously permits the hole pattern to be provided without requiring the CWB and wing root to be brought together.

Process of joining a wing to an aircraft fuselage

A signal-initiation device for initiating control signals in an aircraft fuselage, an aircraft fuselage including a signal-initiation device of such a type, an aircraft including such a fuselage, and the use of a signal-initiation device of such a type. The signal-initiation device for initiating control signals in an aircraft fuselage comprises a switching area configured to generate at least one control signal for controlling at least one orifice shutter present in the aircraft fuselage; and an initiating component connected to the switching area, configured to introduce the at least one control signal into the aircraft fuselage.

Signal initiation for aircraft doors

A method for installing an electric system into an aircraft fuselage. The object to provide a method for simply and quickly installing an electric system into an aircraft fuselage, wherein the electric system is as little heavy and space consuming as possible, and wherein a wide range of customized alternatives of the electric system is possible, is achieved by the steps of providing a fuselage element extending along an aircraft longitudinal axis and including an outer skin and an interior surface, providing a foil sheet of an electrically insulating substrate material, attaching said foil sheet on the inner side of said fuselage element, applying particles of electrically conductive material onto the inner surface of said attached foil sheet opposite the outer skin in a predetermined pattern, such that the accumulated particles of electrically conductive material form electric conductor elements along said inner surface of said foil sheet.

Method for installing an electric system into an aircraft fuselage

A method for producing an aircraft structure component is disclosed the component having an outer skin provided with electric conductor elements. The method includes providing an aircraft structure component having an outer skin, applying particles of electrically conductive material onto the outer surface of the outer skin of said aircraft structure component in a predetermined pattern, such that the accumulated particles of electrically conductive material form electric conductor elements along the outer surface of the outer skin, and applying particles of electrically insulating material onto the outer surface of the outer skin of said aircraft structure component in a predetermined pattern, such that the accumulated particles of electrically isolating material form an insulating layer for the electric conductor elements.

Method for producing an aircraft structure component having an outer skin provided with electric conductor elements

A method for producing an aircraft structure component is disclosed the component having an outer skin provided with a smooth outer surface. The method includes providing an aircraft structure component having an outer skin including at least one recess, detecting the location of said at least one recess by a recess detecting device, and filling said at least one recess at the detected location with particles of a filling material, said particles of filling material being applied into said at least one recess by an ink jet printing device.

Method for producing an aircraft structure component having an outer skin provided with a smooth outer surface

Method and arrangement for supplying essentially hollow bodies with equipment wherein the hollow bodies each have a transverse dimension and a longitudinal dimension being larger than the transverse dimension. The bodies have at least one opening for accessing their interior from outside along their longitudinal dimension. The hollow bodies are arranged essentially side-by-side along the longitudinal dimension and they are moved along their transverse dimension in a clocked fashion. An arrangement comprises a plurality of conveyor means for moving hollow bodies, wherein the conveyor means are arranged such that the hollow bodies are arranged side-by-side along their longitudinal dimension and moved along their transverse dimension in a clocked fashion.

Method and arrangement for supplying essentially hollow bodies with equipment

A painting device for painting a curved surface () of an object (), with a paint material ejection device (), with a guide device () and with a control device. The paint material ejection device () is designed for ejecting paint material. By means of the guide device () the paint material ejection device () can be mechanically guided along a curved surface of an object. By means of the control device the paint material ejection device () and the guide device () can be controlled in such a way that by means of guiding the paint material ejection device () along a predefinable path and by means of predefinable ejection of paint from the paint material ejection device () along the predefinable path a curved surface () of an object () to be painted can be painted.

Painting device, painting arrangement, method for painting a curved surface of an object, and use of an inkjet device for painting an aircraft

The invention relates to a method for producing at least one fuselage cell of an aircraft with the following steps: at least partial production of surface protection and thermal insulation in the region of the at least one shell part, at least partial introduction of technical outfitting systems----, in particular of electrical and hydraulic lines, air-conditioning lines, electrical and hydraulic appliances, sanitary and catering equipment or the like, into the at least one shell part and/or the at least one floor grid, and assembly of the at least one shell part and of the at least one floor gridinto the at least one fuselage section

Method for producing a fuselage cell of an aircraft

An aerodynamic body with a plurality of nozzles for throttling a fluid flow to be removed by suction through the nozzles in a self-regulated fashion is disclosed. The aerodynamic body according to one example, includes a plurality of throttling nozzles with a throttle section that is defined by an inlet and an outlet. In one example, the interior wall of the throttle section may be designed such that an effective flow cross section is reduced in a self-regulated fashion due to the creation of turbulences on the interior wall of the throttle section as the pressure differential between the inlet and the outlet of the throttle section increases.

Reduction of frictional losses in the region of boundary layers on surfaces, around which a fluid flows

Nowadays floor structures in the fuselage of airplanes, which floor structures comprise transverse floor girders, are usually connected to the frame on the right and left by means of rivets and are in turn supported vertically downward by the frame by way of Samer rods. According to one embodiment of the present invention a structural element for an aircraft is stated, comprising an active element and a passive element. In this way additional stiffening of the fuselage, a reduction in fuselage deformation, or active vibration dampening can be provided without additional weight.

Structure element for an aircraft

The clamping device is used to adjust at least one register element in a printing machine. The device has an upper clamping rail, to which the register element is fixed. The upper clamping rail can be moved in a guide and fixed in position in order to adjust the register element.

Device for adjusting at least one register element in a printing machine, and corresponding method

A method and an apparatus for reversing sheet material in a sheet-processing machine having at least two printing units, a reversing drum with a gripper system, and an impression cylinder that can be operated as a storage drum in perfecting mode and to which a further gripper system for one edge of the sheet material is assigned. In perfecting mode, one of the edges of the sheet material is gripped at an angular offset before the transfer centerline between the reversing drum and the storage drum, before the edge of the sheet material fixed to the storage drum is released.

Method and apparatus for reversing sheet material in sheet-processing machines

A supporting or guiding device for sheets in a sheet processing machine includes a supporting or guiding layer having a supporting or guiding surface formed with a plurality of outlet openings for applying a throttled air flow therethrough to a respective sheet. A covering plate is spaced away from the supporting or guiding surface, and at least two intermediate layers are formed with a plurality of openings and disposed between the supporting or guiding surface and the covering plate. The covering plate is connected via a plurality of inlet openings to at least one blast air source. A respective opening formed in one of the intermediate layers is connected to two respective openings formed in the other of the intermediate layers, and an opening formed in the other intermediate layer is connected to two respective openings formed in the one intermediate layer, between one of the respective inlet openings and one of the respective outlet openings associated therewith.

Growing community of inventors

Hamburg, Germany

Eckart Frankenberger