Patents by Inventor Steffen Gerloff

Steffen Gerloff 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: 11306596
    Abstract: The present invention relates to an impulse body module group with at least two impulse body modules, which, in particular, are identical in construction, for a gas turbine blade, wherein each of the impulse body modules comprises a housing, which, in particular, is of one piece and which has a first cavity, which is closed, in particular in an airtight manner, by a first cover, which is joined to the housing, in particular in a material-bonded manner, and in which a single, in particular spherical or cylindrical, first impulse body is accommodated with play of movement in at least one first direction of impact, wherein the housing has no additional cavity or a single additional cavity, in which a single, in particular spherical or cylindrical, additional impulse body is accommodated with play of movement in at least one direction of impact.
    Type: Grant
    Filed: December 12, 2019
    Date of Patent: April 19, 2022
    Assignee: MTU Aero Engines AG
    Inventors: Karl-Hermann Richter, Herbert Hanrieder, Steffen Gerloff
  • Publication number: 20220032384
    Abstract: The present invention relates to a method for manufacturing a plate of a turbomachine having a plurality of receiving grooves, which are formed on the cylindrical peripheral surface of the plate in order to receive blade roots of blades of the turbomachine. The receiving grooves extend in a straight line from one face of the plate to the other face of the plate, such that a straight line delimits the receiving groove from each point on the cross section of the receiving groove on one of the faces to the corresponding point on the cross section on the other face. A circular plate is provided and a plurality of receiving grooves are introduced into the plate simultaneously on opposing regions relative to a central axis of rotation of the plate.
    Type: Application
    Filed: May 2, 2019
    Publication date: February 3, 2022
    Applicant: MTU Aero Engines AG
    Inventors: Albin Platz, Martin Bussmann, Steffen Gerloff, Nicole Feiling, Anna Carina Kuepper, Norbert Huber, Hermann Klingels
  • Publication number: 20200190986
    Abstract: The present invention relates to an impulse body module group with at least two impulse body modules, which, in particular, are identical in construction, for a gas turbine blade, wherein each of the impulse body modules comprises a housing, which, in particular, is of one piece and which has a first cavity, which is closed, in particular in an airtight manner, by a first cover, which is joined to the housing, in particular in a material-bonded manner, and in which a single, in particular spherical or cylindrical, first impulse body is accommodated with play of movement in at least one first direction of impact, wherein the housing has no additional cavity or a single additional cavity, in which a single, in particular spherical or cylindrical, additional impulse body is accommodated with play of movement in at least one direction of impact.
    Type: Application
    Filed: December 12, 2019
    Publication date: June 18, 2020
    Applicant: MTU Aero Engines AG
    Inventors: Karl-Hermann Richter, Herbert Hanrieder, Steffen Gerloff