Patents by Inventor Bjoern Dorr

Bjoern Dorr 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).

  • High lift system for an aircraft
    Patent number: 9278751
    Abstract: A high lift system for an aircraft, which extends and retracts the landing flaps of the aircraft in a fully electric manner. In this context, a fully electric drive is used, comprising an electric motor having an internal redundancy, in such a way that the electric motor is configured as a fault-tolerant electric motor. It may thus be possible to do without a coupling gear unit in the electric motor.
    Type: Grant
    Filed: October 3, 2013
    Date of Patent: March 8, 2016
    Assignee: AIRBUS OPERATIONS GMBH
    Inventors: Markus Christmann, Christoph Giebeler, Martin Recksiek, Bjoern Dorr
  • Closing device, housing part of a lubricant container, diagnostic system and diagnostic method for monitoring the operating state of a lubricant in the housing part
    Patent number: 9182079
    Abstract: The invention relates to a housing part containing a lubricant reservoir and at least one respective inlet and outlet opening for filling and draining a lubricating fluid into and from the lubricant reservoir. The inlet and outlet openings are sealed by releasable closure devices each comprising a sensor means for determining the operation parameters in a lubricant contained in the lubricant reservoir and for generating and/or storing sensor signals, as well as a transceiver for the transmission of the sensor signals to an external processing unit.
    Type: Grant
    Filed: April 7, 2010
    Date of Patent: November 10, 2015
    Assignee: Airbus Operations GmbH
    Inventors: Bjoern Dorr, Franz Nuscheler, Sumit Paul
  • HIGH LIFT SYSTEM FOR AN AIRCRAFT
    Publication number: 20140027580
    Abstract: A high lift system for an aircraft, which extends and retracts the landing flaps of the aircraft in a fully electric manner. In this context, a fully electric drive is used, comprising an electric motor having an internal redundancy, in such a way that the electric motor is configured as a fault-tolerant electric motor. It may thus be possible to do without a coupling gear unit in the electric motor.
    Type: Application
    Filed: October 3, 2013
    Publication date: January 30, 2014
    Inventors: Markus Christmann, Christoph Giebeler, Martin Recksiek, Bjoern Dorr
  • CLOSING DEVICE, HOUSING PART OF A LUBRICANT CONTAINER, DIAGNOSTIC SYSTEM AND DIAGNOSTIC METHOD FOR MONITORING THE OPERATING STATE OF A LUBRICANT IN THE HOUSING PART
    Publication number: 20120123738
    Abstract: The invention relates to a housing part containing a lubricant reservoir and at least one respective inlet and outlet opening for filling and draining a lubricating fluid into and from the lubricant reservoir. The inlet and outlet openings are sealed by releasable closure devices each comprising a sensor means for determining the operation parameters in a lubricant contained in the lubricant reservoir and for generating and/or storing sensor signals, as well as a transceiver for the transmission of the sensor signals to an external processing unit.
    Type: Application
    Filed: April 7, 2010
    Publication date: May 17, 2012
    Applicant: AIRBUS OPERATIONS GMBH
    Inventors: Bjoern Dorr, Franz Nuscheler, Sumit Paul