Patents by Inventor Thomas Konsolke

Thomas Konsolke 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: 10053205
    Abstract: A pressure bulkhead comprises a plurality of material plies arranged one above the other, wherein each material ply contains reinforcing fibers embedded in a matrix material. The reinforcing fibers, in at least one first material ply are oriented in such a manner that their longitudinal axes lie in an angle range of ±2° about a radial direction of the pressure bulkhead.
    Type: Grant
    Filed: March 28, 2016
    Date of Patent: August 21, 2018
    Assignee: Airbus Operations GmbH
    Inventors: Claas De Jong, Markus Mueller, Karim Grase, Matthias Jessrang, Thomas Konsolke, Lars Fiedler, Jelle Bloemhof
  • Publication number: 20160288897
    Abstract: A pressure bulkhead comprises a plurality of material plies arranged one above the other, wherein each material ply contains reinforcing fibers embedded in a matrix material. The reinforcing fibers, in at least one first material ply are oriented in such a manner that their longitudinal axes lie in an angle range of ±2° about a radial direction of the pressure bulkhead.
    Type: Application
    Filed: March 28, 2016
    Publication date: October 6, 2016
    Inventors: Claas De Jong, Markus Mueller, Karim Grase, Matthias Jessrang, Thomas Konsolke, Lars Fiedler, Jelle Bloemhof
  • Patent number: 8088236
    Abstract: The present invention provides an apparatus and a method for producing a large-area fibre-composite structural component, in particular for the aircraft sector, comprising a predetermined shaping element, a controllable laying device for the defined laying of at least one fibrous sheet over or into the predetermined shaping element, a controllable turning device for a defined turning of the predetermined shaping element and of the laying device in relation to each other by a predetermined turning angle, and a central control device, which is connected to the laying device and the turning device for controlling of the same.
    Type: Grant
    Filed: May 4, 2007
    Date of Patent: January 3, 2012
    Assignee: AIRBUS Deutschland GmbH
    Inventors: Joerg Schendel, Bernd Ostermeier, Thomas Konsolke, Ralf-Peter Dittmann
  • Publication number: 20100006202
    Abstract: The present invention provides an apparatus and a method for producing a large-area fibre-composite structural component, in particular for the aircraft sector, comprising a predetermined shaping element, a controllable laying device for the defined laying of at least one fibrous sheet over or into the predetermined shaping element, a controllable turning device for a defined turning of the predetermined shaping element and of the laying device in relation to each other by a predetermined turning angle, and a central control device, which is connected to the laying device and the turning device for controlling of the same.
    Type: Application
    Filed: May 4, 2007
    Publication date: January 14, 2010
    Applicant: AIRBUS Deutschland GmbH
    Inventors: Joerg Schendel, Bernd Ostermeier, Thomas Konsolke, Ralf-Peter Dittmann