Airbus Operations Gmbh

Airbus Defence and Space Gmbh

Tape Weaving Sweden Ab

Swerea Sicomp Ab

Leif Asp

Peter Linde

Alexander Bismarck

Dan Zenkert

Fredrik Ohlsson

Nandan Khokar

Christian Metzner

Soraia Pimenta

Maciej Wysocki

Simon Leijonmarck

David Carlstedt

Tony Carlson

Göran Lindbergh

Guillaume Moreau

James M Glaser

Florence Rinn

Maria Kjell

Novel ultra-thin unidirectional pre-preg tapes are disclosed. They can be used to produce ultra-thin woven, bias, multiaxial, chopped-oriented etc. types of pre-pregs. These ultra-thin pre-pregs enable production of composite material products with well-controlled dimensional tolerances and smooth/even surfaces. Further, they render the production of composite material products relatively simpler, tidier, quicker, and economical. The obtained composite material products are relatively thinner, lighter, and mechanically higher-performing.

Ultra-thin pre-preg sheets and composite materials thereof

A battery cell includes an anode, a cathode, and a separator between the anode and the cathode, wherein at least one of the anode or the cathode includes at least a carbon fiber ply comprising carbon fibers, the carbon fiber ply having a thickness of less than 90 micrometers. Also disclosed are a battery and an aircraft including such battery cell, and a method for manufacturing such battery cell.

Battery cell comprising an ultra thin layer of carbon fibers

A fiber composite component includes an integrated structural health sensor arrangement, wherein the component includes a plurality of layers of fibers embedded in a matrix material, wherein the layers include at least two strain sensing fibers arranged parallel and at a distance to each other, wherein the strain sensing fibers are lithiated carbon fibers having piezoelectric characteristics.

Fiber composite component having an integrated structural health sensor arrangement

A structural component includes a composite laminate built up of a plurality of layers of carbon fibers, wherein the layers of carbon fibers are oriented in different directions, wherein the carbon fibers are surrounded by a conductive polymer resin, wherein the carbon fibers of at least one of the layers comprise an electrically insulating coating, and wherein at least one of the coated carbon fibers extend through its respective layer to form an electrical connection between ends of the layer spaced apart from one another.

Structural component with an electrical transmission device, method for providing a structural component with an electrical transmission device, electrical wiring system and aircraft component

Growing community of inventors

Moelndal, Sweden

Leif Asp