Patents by Inventor Andreas HARTUNG

Andreas HARTUNG 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).

  • Publication number: 20140348639
    Abstract: A blade (1) for a turbomachine, including a turbine blade (1.1) which has a channel (1.5), an impact chamber (2) having a constricted cross section being situated in the channel for the purpose of accommodating a single impulse body (3) is provided.
    Type: Application
    Filed: May 21, 2014
    Publication date: November 27, 2014
    Inventors: Frank STIEHLER, Andreas Hartung
  • Publication number: 20140348657
    Abstract: A blade (1) for a turbomachine, including an impact chamber (2), a single impulse body (3) being situated in the impact chamber, a clearance (S1+S2) between the impulse body and the impact chamber being at least 10 ?m and/or at most 1.5 mm in at least one direction.
    Type: Application
    Filed: May 21, 2014
    Publication date: November 27, 2014
    Inventors: Frank Stiehler, Andreas Hartung
  • Publication number: 20130280083
    Abstract: In a moving blade system for a turbomachine, in particular a gas turbine, having at least one moving blade (1), the moving blade system having at least one cavity (3) in which at least one tuning mass (2) is movably situated, the tuning mass and/or the cavity is/are adapted in such a way that the tuning mass rests against an inner wall (3.1) of the cavity in a predefined first operating state of the turbomachine and at least temporarily moves away from the inner wall in a second predefined operating state of the turbomachine.
    Type: Application
    Filed: November 5, 2011
    Publication date: October 24, 2013
    Applicant: MTU AERO ENGINES GMBH
    Inventor: Andreas Hartung
  • Publication number: 20120102701
    Abstract: The English-language Abstract from the international application is to be retained and is therefore not duplicated in the specification.
    Type: Application
    Filed: July 7, 2010
    Publication date: May 3, 2012
    Applicant: MTU AERO ENGINES GMBH
    Inventors: Hans Peter Borufka, Hernan Victor Arrieta, Andreas Hartung, Ulrich Retze
  • Publication number: 20110255973
    Abstract: A damping system for damping vibrations of a rotor blade of a rotor of a turbomachine is disclosed. A damping element is guided on a support such that the damping element is radially outwardly movable during a rotation of the rotor and is contactable with a lower platform area of a rotor blade. A circumferential contact surface is formed by an elevation on the lower platform area, where the circumferential contact surface is a limit stop for a movement of the damping element.
    Type: Application
    Filed: April 15, 2011
    Publication date: October 20, 2011
    Applicant: MTU Aero Engines GmbH
    Inventors: Hans Peter BORUFKA, Andreas HARTUNG, Patrick PROKOPCZUK, Frank STIEHLER