Patents by Inventor Rüdy Gysemberg

Rüdy Gysemberg 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).

  • Supporting pillar for an aircraft's structural component manufactured by a selective laser melting process
    Patent number: 9187166
    Abstract: An elongated supporting pillar for a high-strength structural component is designed to absorb bending forces that act transversely to a longitudinal direction of extension of the supporting pillar. The supporting pillar comprises a wall which at least partially encloses an elongated cavity of the supporting pillar. A reinforcement structure is arranged within the cavity and transversely to the direction of longitudinal extension in such a manner that the reinforcement structure can absorb at least some of the bending forces. The reinforcement structure is designed integrally with the wall, wherein both the wall and the reinforcement structure comprise a meltable material. The supporting pillar has a conical shape, and wherein a first end of the supporting pillar is wider than a second end of the supporting pillar.
    Type: Grant
    Filed: January 9, 2015
    Date of Patent: November 17, 2015
    Assignee: Airbus Operations GmbH
    Inventors: Christoph Klahn, Rüdy Gysemberg, Olaf Rehme
  • SUPPORTING PILLAR FOR AN AIRCRAFT'S STRUCTURAL COMPONENT MANUFACTURED BY A SELECTIVE LASER MELTING PROCESS
    Publication number: 20150151827
    Abstract: An elongated supporting pillar for a high-strength structural component is designed to absorb bending forces that act transversely to a longitudinal direction of extension of the supporting pillar. The supporting pillar comprises a wall which at least partially encloses an elongated cavity of the supporting pillar. A reinforcement structure is arranged within the cavity and transversely to the direction of longitudinal extension in such a manner that the reinforcement structure can absorb at least some of the bending forces. The reinforcement structure is designed integrally with the wall, wherein both the wall and the reinforcement structure comprise a meltable material. The supporting pillar has a conical shape, and wherein a first end of the supporting pillar is wider than a second end of the supporting pillar.
    Type: Application
    Filed: January 9, 2015
    Publication date: June 4, 2015
    Inventors: Christoph Klahn, Rüdy Gysemberg, Olaf Rehme
  • Supporting pillar for an aircraft's structural component manufactured by a selective laser melting process
    Patent number: 8960605
    Abstract: The invention relates to an elongated supporting pillar for a high-strength structural component, wherein the supporting pillar is designed to absorb bending forces that act transversely to a longitudinal direction of extension of the supporting pillar. The supporting pillar comprises a wall which at least partially encloses an elongated cavity of the supporting pillar. A reinforcement structure is arranged within the cavity and transversely to the direction of longitudinal extension in such a manner that the reinforcement structure can absorb at least some of the bending forces. The reinforcement structure is designed integrally with the wall, wherein both the wall and the reinforcement structure comprise a meltable material.
    Type: Grant
    Filed: July 30, 2009
    Date of Patent: February 24, 2015
    Assignee: Airbus Operations GmbH
    Inventors: Christoph Klahn, Rüdy Gysemberg, Olaf Rehme
  • Attachment structure for affixing interior equipment components of an aircraft passenger cabin
    Patent number: 8403266
    Abstract: An attachment structure is provided by which interior equipment components of an aircraft passenger cabin can conveniently be affixed. The attachment structure includes, but is not limited to at least one system support that above the cabin floor extends at least along the spacing of two frame elements. The system support has a longitudinal extension along which it comprises a plurality of attachment means, evenly spaced apart from each other, for affixing interior equipment components, wherein the spacing of the attachment means is smaller than the spacing of the frame elements.
    Type: Grant
    Filed: May 15, 2008
    Date of Patent: March 26, 2013
    Assignee: Airbus Operations GmbH
    Inventors: Markus Fokken, Rüdy Gysemberg, Johannes Gonnsen, Uwe Johannsen, Helge Tiede
  • SUPPORTING PILLAR FOR AN AIRCRAFT'S STRUCTURAL COMPONENT MANUFACTURED BY A SELECTIVE LASER MELTING PROCESS
    Publication number: 20110253878
    Abstract: The invention relates to an elongated supporting pillar for a high-strength structural component, wherein the supporting pillar is designed to absorb bending forces that act transversely to a longitudinal direction of extension of the supporting pillar. The supporting pillar comprises a wall which at least partially encloses an elongated cavity of the supporting pillar. A reinforcement structure is arranged within the cavity and transversely to the direction of longitudinal extension in such a manner that the reinforcement structure can absorb at least some of the bending forces. The reinforcement structure is designed integrally with the wall, wherein both the wall and the reinforcement structure comprise a meltable material.
    Type: Application
    Filed: July 30, 2009
    Publication date: October 20, 2011
    Applicant: AIRBUS OPERATIONS GMBH
    Inventors: Christoph Klahn, Rüdy Gysemberg, Olaf Rehme
  • Wall element with an antenna device
    Patent number: 7701403
    Abstract: A wall element for emitting high-frequency radiation for an aircraft comprises an antenna device. The antenna device is adapted for emitting high frequency radiation. Furthermore, the antenna device is integrated in the wall element.
    Type: Grant
    Filed: November 30, 2007
    Date of Patent: April 20, 2010
    Assignee: Airbus Deutschland GmbH
    Inventors: Robert Kebel, Wolfgang Kuerner, Ruedy Gysemberg
  • Wall element with an antenna device
    Publication number: 20080158071
    Abstract: A wall element for emitting high-frequency radiation for an aircraft comprises an antenna device. The antenna device is adapted for emitting high frequency radiation. Furthermore, the antenna device is integrated in the wall element.
    Type: Application
    Filed: November 30, 2007
    Publication date: July 3, 2008
    Applicant: Airbus Deutschland GmbH
    Inventors: Robert Kebel, Wolfgang Kuerner, Ruedy Gysemberg