Airbus Defence and Space Gmbh

Airbus Operations Gmbh

Christopher Buchmann

Christian Weimer

Jonas Gruenewald

Christoph Meier

Alois Friedberger

Thomas Kruse

Thomas Körwien

Henning Becker

Richard Hesse

Andreas Meyer-Giesow

Jonas GRÜNEWALD

A method for determining a distance between components has the steps of providing a first conductive section in or on the first component in a region directed toward the second component, providing a second conductive section in or on the second component in a region directed toward the first conductive section, feeding a first voltage pulse into a first connection of the first conductive section, capturing a reflection voltage pulse in response to the first voltage pulse at the first connection, determining an impedance profile along the first conductive section by evaluating the reflection voltage pulse, and determining a distance between the components along the first conductive section by calculating a corresponding local distance, associated with the determined impedance profile, between the first conductive section and the second conductive section.

Method for determining a distance between two components to be joined

A measurement arrangement for measuring process and structure parameters of a fiber composite material along a measuring path includes a fiber material, a matrix material which surrounds the fiber material at least in regions, and an electrical sensor element that includes at least two signal transmission lines twisted together and aligned along the measuring path in and/or at the fiber material such that the signal transmission lines are surrounded at least in portions by the matrix material, wherein the electrical sensor element is configured to measure the process and structure parameters on the basis of the behavior of electromagnetic signals that are fed into the signal transmission lines.

Measurement arrangement for measuring process and structure parameters of a fiber composite material along a measuring path

A fiber composite laminate having one or more fiber layers, comprising a first laminate region and a second laminate region. In the first laminate region, the fiber layers of the fiber composite laminate are impregnated with a thermoplastic elastomer material. In the second laminate region, fiber layers of a first lamina of the fiber composite laminate are impregnated with the thermoplastic elastomer matrix, and fiber layers of at least one second lamina of the fiber composite laminate that is positioned on top of the first lamina are impregnated with a thermosetting polymer matrix.

Fiber composite laminate and method for producing a fiber composite laminate

A method for producing a fiber composite laminate, including the steps of applying pressure and/or heat to a first preform, which has one or more dry fiber layers and a thermoplastic elastomer, such that the thermoplastic portion of the thermoplastic elastomer completely impregnates the dry fiber layers of the first preform in at least one first region and only partially impregnates the dry fiber layers in at least one second region and, in a thermosetting polymer matrix, impregnating and curing the fiber layers of the second region of the first preform that are still dry and have not been impregnated with the thermoplastic portion of the thermoplastic elastomer.

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Munich, Germany

Christopher Buchmann