Patents by Inventor Till GUNDLACH

Till GUNDLACH 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).

  • Patent number: 10550951
    Abstract: An actuator includes a brushless DC motor, an output device, a reduction system coupled between the brushless DC motor and the output device, and a contactless position sensor configured to sense a position of the output device.
    Type: Grant
    Filed: November 2, 2017
    Date of Patent: February 4, 2020
    Assignee: Airbus Operations Limited
    Inventors: Till Gundlach, Kayvon Barad, Osama Al-Tayawe, Geoff Ward, Andrew Stewart, Christopher Lewis
  • Publication number: 20180135772
    Abstract: An actuator includes a brushless DC motor, an output device, a reduction system coupled between the brushless DC motor and the output device, and a contactless position sensor configured to sense a position of the output device.
    Type: Application
    Filed: November 2, 2017
    Publication date: May 17, 2018
    Inventors: Till GUNDLACH, Kayvon BARAD, Osama AL-TAYAWE, Geoff WARD, Andrew STEWART, Christopher LEWIS
  • Patent number: 8651926
    Abstract: An ice separator is provided that includes, but is not limited to at least one curved airflow deflection surface. The ice separator includes, but is not limited to an inflow aperture with a downstream trapping pocket at the airflow deflection surface, in which trapping pocket ice particles from an airflow flowing onto the ice separator are trapped due to their inertial forces. In this way with simple means an effective device for removing ice particles from airflow may be achieved.
    Type: Grant
    Filed: July 23, 2010
    Date of Patent: February 18, 2014
    Assignee: Airbus Operations GmbH
    Inventor: Till Gundlach
  • Publication number: 20110021129
    Abstract: An ice separator is provided that includes, but is not limited to at least one curved airflow deflection surface. The ice separator includes, but is not limited to an inflow aperture with a downstream trapping pocket at the airflow deflection surface, in which trapping pocket ice particles from an airflow flowing onto the ice separator are trapped due to their inertial forces. In this way with simple means an effective device for removing ice particles from airflow may be achieved.
    Type: Application
    Filed: July 23, 2010
    Publication date: January 27, 2011
    Applicant: AIRBUS OPERATIONS GMBH
    Inventor: Till GUNDLACH