Patents by Inventor Frank Truckenmueller

Frank Truckenmueller 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: 7794202
    Abstract: A turbine blade is provided, comprising a stator-side end located toward a stationary stator cylinder of the turbine, a rotor-side end located toward an axial rotor of the turbine, a leading edge located between the stator-side end and the rotor-side end, a trailing edge located between the stator-side end and the rotor-side end and located down-stream of the leading edge with respect to a fluid flow direction, wherein the rotor-side and stator-side ends have a negative sweep angle as measured between the instantaneous tangent of the blade surface and the fluid flow direction.
    Type: Grant
    Filed: June 18, 2004
    Date of Patent: September 14, 2010
    Assignee: Siemens Aktiengesellschaft
    Inventors: Donald Borthwick, Shun Chen, Heinrich Stüer, Frank Truckenmüller
  • Patent number: 7753652
    Abstract: An array of blades for use in a turbomachine is provided comprising a plurality of blades mounted to a rotor disk. A plurality of first blades form a first set of blades and a plurality of second blades form a second set of blades. A blade-to-blade flow field defined between successive ones of the first set of blades is interrupted by the second set of blades to form an asymmetric blade-to-blade flow field around the array of blades. The trailing edges of the second set of blades are positioned forwardly from a line connecting the trailing edges of the first set of blades such that shock forces in the flow field around the array of blades will generally impinge on a stable region of the first set of blades.
    Type: Grant
    Filed: December 15, 2006
    Date of Patent: July 13, 2010
    Assignee: Siemens Energy, Inc.
    Inventors: Frank Truckenmueller, Heinrich Stueer, Harry F. Martin, Lewis Gray
  • Publication number: 20080145228
    Abstract: An array of blades for use in a turbomachine is provided comprising a plurality of blades mounted to a rotor disk. A plurality of first blades form a first set of blades and a plurality of second blades form a second set of blades. A blade-to-blade flow field defined between successive ones of the first set of blades is interrupted by the second set of blades to form an asymmetric blade-to-blade flow field around the array of blades. The trailing edges of the second set of blades are positioned forwardly from a line connecting the trailing edges of the first set of blades such that shock forces in the flow field around the array of blades will generally impinge on a stable region of the first set of blades.
    Type: Application
    Filed: December 15, 2006
    Publication date: June 19, 2008
    Inventors: Frank Truckenmueller, Heinrich Stueer, Harry F. Martin, Lewis Gray