Patents by Inventor Thilo DAUCH

Thilo DAUCH 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).

  • Nozzle for a combustion chamber of an engine
    Patent number: 11085632
    Abstract: A nozzle for a combustion chamber of an engine for providing a fuel-air mixture at a nozzle exit opening of the nozzle includes a nozzle main body including the nozzle exit opening and extends along a nozzle longitudinal axis. The nozzle main body has a first air guiding channel, a fuel guiding channel and a further, radially outwardly second air guiding channel. One end of the fuel guiding channel is positioned in front of the end of the second air guiding channel. A tapering channel portion with a shell surface inclined with respect to a nozzle longitudinal axis in the axial direction and connects to a radially outer shell surface of the fuel guiding channel is formed between the end of the fuel guiding channel and the end of the second air guiding channel at the nozzle.
    Type: Grant
    Filed: October 16, 2018
    Date of Patent: August 10, 2021
    Assignee: Rolls-Royce Deutschland Ltd & Co KG
    Inventors: Thomas Doerr, Sebastian Bake, Thilo Dauch, Rainer Koch, Hans-Joerg Bauer
  • NOZZLE FOR A COMBUSTION CHAMBER OF AN ENGINE
    Publication number: 20190113226
    Abstract: A nozzle for a combustion chamber of an engine for providing a fuel-air mixture at a nozzle exit opening of the nozzle includes a nozzle main body including the nozzle exit opening and extends along a nozzle longitudinal axis. The nozzle main body has a first air guiding channel, a fuel guiding channel and a further, radially outwardly second air guiding channel. One end of the fuel guiding channel is positioned in front of the end of the second air guiding channel. A tapering channel portion with a shell surface inclined with respect to a nozzle longitudinal axis in the axial direction and connects to a radially outer shell surface of the fuel guiding channel is formed between the end of the fuel guiding channel and the end of the second air guiding channel at the nozzle.
    Type: Application
    Filed: October 16, 2018
    Publication date: April 18, 2019
    Inventors: Thomas DOERR, Sebastian BAKE, Thilo DAUCH, Rainer KOCH, Hans-Joerg BAUER