Patents by Inventor Dan ZENKERT

Dan ZENKERT has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 11075384
    Abstract: 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.
    Type: Grant
    Filed: November 20, 2018
    Date of Patent: July 27, 2021
    Assignees: Airbus Defence and Space GmbH, Airbus Operations GmbH
    Inventors: Peter Linde, Leif Asp, Dan Zenkert, Maciej Wysocki, Fredrik Ohlsson, Christian Metzner
  • Patent number: 10875661
    Abstract: 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.
    Type: Grant
    Filed: December 10, 2019
    Date of Patent: December 29, 2020
    Inventors: Peter Linde, Leif Asp, Dan Zenkert, Göran Lindbergh
  • Publication number: 20200235402
    Abstract: 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.
    Type: Application
    Filed: November 20, 2018
    Publication date: July 23, 2020
    Inventors: Peter LINDE, Leif ASP, Dan ZENKERT, Maciej WYSOCKI, Fredrik OHLSSON, Christian METZNER
  • Publication number: 20200198800
    Abstract: 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.
    Type: Application
    Filed: December 10, 2019
    Publication date: June 25, 2020
    Applicant: Airbus Operations GmbH
    Inventors: Peter Linde, Leif Asp, Dan Zenkert, Göran Lindbergh
  • Publication number: 20200200696
    Abstract: A fiber composite component having an integrated structural health sensor arrangement includes a plurality of layers of fibers embedded in a matrix material, at least two rupture sensing fibers arranged on or in at least one of the layers, wherein the rupture sensing fibers are carbon fibers having an electrically insulating coating, and two electrical connection devices, each being accessible from an outer delimiting surface or an outer edge of the component, wherein the electrical connection devices are connected to different ends of the rupture sensing fibers.
    Type: Application
    Filed: December 11, 2019
    Publication date: June 25, 2020
    Applicant: Airbus Operations GmbH
    Inventors: Peter Linde, Leif Asp, Dan Zenkert
  • Publication number: 20190181452
    Abstract: 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.
    Type: Application
    Filed: November 20, 2018
    Publication date: June 13, 2019
    Inventors: Peter LINDE, Leif ASP, Dan ZENKERT, Maciej WYSOCKI, Fredrik OHLSSON, Christian METZNER
  • Patent number: 10286997
    Abstract: 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.
    Type: Grant
    Filed: July 7, 2017
    Date of Patent: May 14, 2019
    Assignee: Airbus Operations GmbH
    Inventors: Peter Linde, Leif Asp, Dan Zenkert
  • Publication number: 20180015705
    Abstract: A structural component includes a composite laminate built up of layers of carbon fibers, wherein the layers of carbon fibers are oriented in different directions and wherein the carbon fibers are surrounded by a conductive polymer resin. The carbon fibers of at least one of the layers include 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. With an ion-transmissive insulation coating the carbon fibers form anodes such that, together with a metal layer provided with the composite laminate forming an cathode, the structural is enabled to additionally form an integrated composite power source.
    Type: Application
    Filed: July 17, 2017
    Publication date: January 18, 2018
    Inventors: Peter LINDE, Leif ASP, Dan ZENKERT
  • Publication number: 20180015995
    Abstract: A structural component includes a composite laminate built up of a plurality of layers of carbon fibres, wherein the layers of carbon fibres are oriented in different directions, wherein the carbon fibres are surrounded by a conductive polymer resin, wherein the carbon fibres of at least one of the layers comprise an electrically insulating coating, and wherein at least one of the coated carbon fibres extend through its respective layer to form an electrical connection between ends of the layer spaced apart from one another.
    Type: Application
    Filed: July 7, 2017
    Publication date: January 18, 2018
    Applicant: Airbus Operations GmbH
    Inventors: Peter Linde, Leif Asp, Dan Zenkert