Patents by Inventor Ulrike GRAEBER

Ulrike GRAEBER 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).

  • Self-supporting cabin structure
    Patent number: 9387920
    Abstract: A cabin structural unit for attaching cabin installation elements is provided for an aircraft. The cabin structural unit is set up in such a way that a cabin installation element is attachable. The cabin structural unit is implemented as self-supporting and fastenable to an aircraft structure.
    Type: Grant
    Filed: April 8, 2009
    Date of Patent: July 12, 2016
    Assignee: AIRBUS OPERATIONS GMBH
    Inventors: Ulrike Graeber, Peter Grosse-Plankermann, Martin Paetz
  • Aircraft having a force transmission element between a cabin structural element and a primary structure
    Patent number: 8430362
    Abstract: The invention relates to an aircraft comprising a force transmission element which detachably connects a cabin structural segment to an aircraft primary structure and which comprises a cabin bearing element and a structure bearing element, the cabin bearing element being connected to the cabin structural segment and the structure bearing element being connected to the aircraft primary structure. The force transmission element is designed in such a manner that a force transmission can take place between the cabin structural segment and the aircraft primary structure with at least one degree of freedom of movement.
    Type: Grant
    Filed: March 20, 2009
    Date of Patent: April 30, 2013
    Assignee: Airbus Operations GmbH
    Inventors: Ulrike Graeber, Peter Grosse-Plankermann, Martin Pätz, Holger Becker
  • AIRCRAFT HAVING A FORCE TRANSMISSION ELEMENT BETWEEN A CABIN STRUCTURAL ELEMENT AND A PRIMARY STRUCTURE
    Publication number: 20110133027
    Abstract: The invention relates to an aircraft comprising a force transmission element which detachably connects a cabin structural segment to an aircraft primary structure and which comprises a cabin bearing element and a structure bearing element, the cabin bearing element being connected to the cabin structural segment and the structure bearing element being connected to the aircraft primary structure. The force transmission element is designed in such a manner that a force transmission can take place between the cabin structural segment and the aircraft primary structure with at least one degree of freedom of movement.
    Type: Application
    Filed: March 20, 2009
    Publication date: June 9, 2011
    Applicant: AIRBUS OPERATIONS GMBH
    Inventors: Ulrike Graeber, Peter Grosse-Plankermann, Martin Pätz, Holger Becker
  • SELF-SUPPORTING CABIN STRUCTURE
    Publication number: 20090250554
    Abstract: A cabin structural unit for attaching cabin installation elements is provided for an aircraft. The cabin structural unit is set up in such a way that a cabin installation element is attachable. The cabin structural unit is implemented as self-supporting and fastenable to an aircraft structure.
    Type: Application
    Filed: April 8, 2009
    Publication date: October 8, 2009
    Applicant: AIRBUS DEUTSCHLAND GMBH
    Inventors: Ulrike GRAEBER, Peter GROSSE-PLANKERMANN, Martin PAETZ