Patents by Inventor Werner Mangler

Werner Mangler 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).

  • CONTROL UNIT, SYSTEM AND METHOD
    Publication number: 20250178717
    Abstract: The present disclosure relates to a control unit for actuating at least two components of an aircraft, comprising a control part and a switching part, wherein the control part and the switching part are configured such that the components can be actuated sequentially, wherein at one timepoint just one of the components can be actuated, or that at least two components cannot be actuated simultaneously.
    Type: Application
    Filed: November 18, 2024
    Publication date: June 5, 2025
    Inventors: Christian KOHLÖFFEL, Werner MANGLER
  • Drive system for a variable camber aircraft wing
    Patent number: 9260181
    Abstract: The present invention relates to a drive system for a variable camber aircraft wing having position variable front flaps and/or rear flaps, having drive shafts, which are arranged such that that the flaps undergo a change of position in operation of the drive shafts, and having one or more drive units in driving connection with the drive shafts, wherein at least one switchable coupling is provided via which the drive shafts of two flaps of an aircraft wing can be coupled to one another.
    Type: Grant
    Filed: May 22, 2015
    Date of Patent: February 16, 2016
    Assignee: Liebherr-Aerospace Lindenberg GmbH
    Inventors: Susanne Conrad, Werner Mangler, Josef Bär, Bernd Schievelbusch
  • Drive system for a variable camber aircraft wing
    Publication number: 20080283672
    Abstract: The present invention relates to a drive system for a variable camber aircraft wing having position variable front flaps and/or rear flaps, having drive shafts, which are arranged such that that the flaps undergo a change of position in operation of the drive shafts, and having one or more drive units in driving connection with the drive shafts, wherein at least one switchable coupling is provided via which the drive shafts of two flaps of an aircraft wing can be coupled to one another.
    Type: Application
    Filed: May 8, 2008
    Publication date: November 20, 2008
    Inventors: Susanne Denzler, Werner Mangler, Josef Bar, Bernd Schievelbusch