Patents by Inventor Christoph Ader

Christoph Ader 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).

  • Device and method for the repair or production of blade tips of blades of a gas turbine, in particular of an aircraft engine
    Patent number: 8584357
    Abstract: The invention relates to a device for the production or repair of a blade for a gas turbine, said device comprising: a holding device for holding a blade or an aerofoil of a blade; a lowering mechanism for lowering the blade or the aerofoil; a container for receiving power and/or for receiving the blade or the aerofoil; a heating device; and a radiation source, wherein the heating device is formed as an induction coil.
    Type: Grant
    Filed: December 5, 2007
    Date of Patent: November 19, 2013
    Assignee: MTU Aero Engines AG
    Inventors: Karl-Hermann Richter, Herbert Hanrieder, Christoph Ader, Christoph Over
  • HIGH-PRESSURE TURBINE ROTOR, AND METHOD FOR THE PRODUCTION THEREOF
    Publication number: 20110052412
    Abstract: A method for producing a high-pressure turbine rotor, as well as a turbine rotor, is disclosed. The turbine rotor is designed as a blisk (i.e., bladed disk) and forms a radially inward disk and several vanes or blades that project from the disk. The turbine rotor has an internal duct system for air cooling and at least one section of the turbine rotor is manufactured in a generative production process.
    Type: Application
    Filed: October 10, 2007
    Publication date: March 3, 2011
    Applicant: MTU Aero Engines GmbH
    Inventors: Christoph Ader, Karl-Heinz Dusel, Roland Huttner, Steffen Schlothauer
  • DEVICE AND METHOD FOR THE REPAIR OR PRODUCTION OF BLADE TIPS OF BLADES OF A GAS TURBINE, IN PARTICULAR OF AN AIRCRAFT ENGINE
    Publication number: 20100151145
    Abstract: The invention relates to a device for the production or repair of a blade for a gas turbine, said device comprising: a holding device for holding a blade or an aerofoil of a blade; a lowering mechanism for lowering the blade or the aerofoil; a container for receiving power and/or for receiving the blade or the aerofoil; a heating device; and a radiation source, wherein the heating device is formed as an induction coil.
    Type: Application
    Filed: December 5, 2007
    Publication date: June 17, 2010
    Applicants: MTU AERO ENGINES, GMBH, INNO-SHAPE GMBH
    Inventors: Karl-Hermann Richter, Herbert Hanrieder, Christoph Ader, Christoph Over