Patents by Inventor Christian Zuber

Christian Zuber 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).

  • Publication number: 20240384769
    Abstract: An apparatus for detecting the clamping forces between a brake body (1) and a brake rotor (2) of a disc brake or drum brake comprises a multi-layer measuring film (3) that can be inserted between the brake body (1) and the brake rotor (2) and which multi-layer measuring film (3) comprises a sensor layer (6) with pressure-dependent changing electrical properties and two electrically conductive layers (7) connected to an evaluation device (5). For assignment of the determined clamping forces to the area of the sensor layer (6) exposed to the respective pressurization, the measuring film (3) has two electrode layers (8) connected to the evaluation device (5) for determining the film capacitance between the electrode layers (8).
    Type: Application
    Filed: July 26, 2022
    Publication date: November 21, 2024
    Inventors: Walter Rieger, Gernot Theuermann, Christian Zuber
  • Patent number: 8147206
    Abstract: A jet vane for use in streams of hot gas, comprising a wing having a core area and a cover skin area surrounding the core area, is proposed. The cover skin area is made of a fiber-reinforced material, and the fibers in the cover skin area are oriented substantially parallel to the wing surface, and/or the cover skin area is made of a fiber-reinforced material that is reinforced with short fibers.
    Type: Grant
    Filed: January 18, 2007
    Date of Patent: April 3, 2012
    Assignee: Deutsches Zentrum fuer Luft-und Raumfahrt e.V.
    Inventors: Bernhard Heidenreich, Christian Zuber
  • Publication number: 20100272577
    Abstract: A jet vane for use in streams of hot gas, comprising a wing having a core area and a cover skin area surrounding the core area, is proposed. The cover skin area is made of a fiber-reinforced material, and the fibers in the cover skin area are oriented substantially parallel to the wing surface, and/or the cover skin area is made of a fiber-reinforced material that is reinforced with short fibers.
    Type: Application
    Filed: January 18, 2007
    Publication date: October 28, 2010
    Applicant: Deutsches Zentrum fuer Luft-und Raumfahrt e.V.
    Inventors: Bernhard Heidenreich, Christian Zuber
  • Publication number: 20090239434
    Abstract: A method of producing a fiber-reinforced carbide-ceramic component includes producing a carbonaceous article from at least one unidirectional tape by pyrolysis, infiltrating the carbonaceous article with carbide former, and coating the at least one unidirectional tape with a coating material being volatile in pyrolysis and/or providing the at least one unidirectional tape with a transverse thread system including transverse threads composed of a material being volatile in pyrolysis. A fiber-reinforced carbide ceramic component is also provided.
    Type: Application
    Filed: June 5, 2009
    Publication date: September 24, 2009
    Applicants: SGL CARBON AG, DEUTSCHES ZENTRUM FUR LUFT- UND RAUMFAHRT E. V.
    Inventors: Bodo Benitsch, Bernhard Heidenreich, Christian Zuber