Patents by Inventor Johanna Pyrczek

Johanna Pyrczek 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).

  • Arrangement for guiding a cable between a wing and an aerodynamic body movably supported relative thereto; wing of an aircraft having such an arrangement and aircraft having such a wing
    Patent number: 9923349
    Abstract: An assembly for guiding a cable between a structural part of an aircraft and a movable aerodynamic body includes a chain of pivotally connected links, a first coil device arranged between each pair of the links for guiding the cable between two angular positions, and a second coil device arranged at the first end of the chain for passing the cable from the chain to the aerodynamic body. The support of the assembly is statically determinate through the use of a bracket pivotally connected to one of the links at the structural part, which bracket does not permit a translative motion relative to the structural part. This is further supported by a bearing located at one of the links which is connected to the second coil device, which bearing permits angular rotation at least in two orthogonal directions, but no translative motion relative to the aerodynamic body.
    Type: Grant
    Filed: September 3, 2014
    Date of Patent: March 20, 2018
    Assignee: Airbus Operations GmbH
    Inventors: Bernhard Schlipf, Johanna Pyrczek, Michael Roters
  • Arrangement For Guiding A Cable Between A Wing And An Aerodynamic Body Movably Supported Relative Thereto; Wing Of An Aircraft Having Such An Arrangement And Aircraft Having Such A Wing
    Publication number: 20150069183
    Abstract: An assembly for guiding a cable between a structural part of an aircraft and a movable aerodynamic body includes a chain of pivotally connected links, a first coil device arranged between each pair of the links for guiding the cable between two angular positions, and a second coil device arranged at the first end of the chain for passing the cable from the chain to the aerodynamic body. The support of the assembly is statically determinate through the use of a bracket pivotally connected to one of the links at the structural part, which bracket does not permit a translative motion relative to the structural part. This is further supported by a bearing located at one of the links which is connected to the second coil device, which bearing permits angular rotation at least in two orthogonal directions, but no translative motion relative to the aerodynamic body.
    Type: Application
    Filed: September 3, 2014
    Publication date: March 12, 2015
    Applicant: AIRBUS OPERATIONS GMBH
    Inventors: Bernhard Schlipf, Johanna Pyrczek, Michael Roters