Patents by Inventor Hubertus Edward Paprotna

Hubertus Edward Paprotna 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: 7686569
    Abstract: A blade gap control system configured to move a blade ring of a turbine engine relative to a blade assembly to reduce the gaps between the tips of the blades and the blade rings to increase the efficiency of the turbine engine is provided. The blade rings can be at an acute angle with respect to the rotational axis of the blade assembly. The axial movement of the blade ring can be done by a pressure differential supplied across the blade ring, the thermal expansion and/or contraction of a linkage or by a piston.
    Type: Grant
    Filed: December 4, 2006
    Date of Patent: March 30, 2010
    Assignee: Siemens Energy, Inc.
    Inventors: Hubertus Edward Paprotna, Oran Bertsch
  • Patent number: 7562880
    Abstract: A seal usable between two thermally movable components to prevent fluids from mixing. For instance, the seal may be used to seal thermally movable components of a turbine engine that may include, but are not limited to, leading edge shrouds, isolation rings, ring segments, and vane segments. The seal may be formed from a body having a cross-section generally orthogonal to a longitudinal axis and include a first side, a second side generally opposite to the first side, a first end, and a second end generally opposite to the first end. A compliant material may be coupled to the first or second end, or both, and may absorb thermal expansion of the two thermally movable components. The seal may reduce leakage flow paths between the seal and the thermally movable components.
    Type: Grant
    Filed: February 9, 2004
    Date of Patent: July 21, 2009
    Assignee: Siemens Energy, Inc.
    Inventors: Hubertus Edward Paprotna, David A. Little
  • Publication number: 20080131270
    Abstract: A blade gap control system configured to move a blade ring of a turbine engine relative to a blade assembly to reduce the gaps between the tips of the blades and the blade rings to increase the efficiency of the turbine engine is provided. The blade rings can be at an acute angle with respect to the rotational axis of the blade assembly. The axial movement of the blade ring can be done by a pressure differential supplied across the blade ring, the thermal expansion and/or contraction of a linkage or by a piston.
    Type: Application
    Filed: December 4, 2006
    Publication date: June 5, 2008
    Inventors: Hubertus Edward Paprotna, Oran Bertsch
  • Patent number: 6854736
    Abstract: A seal assembly and a rotary machine in combination with the seal assembly are provided. The seal assembly includes a seal and a biasing device configured to produce a force for mechanically biasing the seal toward a first position relative to the rotatable portion. The seal is further responsive to pressurized fluid for creating a force opposed to the biasing force to cause movement of the seal toward a second position closer to the rotatable portion than the first position, thereby reducing flow leakage between the stationary portion and the rotatable portion. The pressurized fluid may be the working fluid produced by or used within the rotary machine.
    Type: Grant
    Filed: March 26, 2003
    Date of Patent: February 15, 2005
    Assignee: Siemens Westinghouse Power Corporation
    Inventor: Hubertus Edward Paprotna
  • Publication number: 20040188947
    Abstract: A seal assembly and a rotary machine in combination with the seal assembly are provided. The seal assembly includes a seal and a biasing device configured to produce a force for mechanically biasing the seal toward a first position relative to the rotatable portion. The seal is further responsive to pressurized fluid for creating a force opposed to the biasing force to cause movement of the seal toward a second position closer to the rotatable portion than the first position, thereby reducing flow leakage between the stationary portion and the rotatable portion. The pressurized fluid may be the working fluid produced by or used within the rotary machine.
    Type: Application
    Filed: March 26, 2003
    Publication date: September 30, 2004
    Applicant: Siemens Westinghouse Power Corporation
    Inventor: Hubertus Edward Paprotna
  • Patent number: 5918466
    Abstract: A gas turbine system in which substantially all of the compressed air from the compressor portion of the gas turbine is used to fluidize a bed of solid fuel, such as char, in a pressurized fluidized bed gasifier so as to produce a hot gas. The hot gas flows through a heat recovery steam generator so as to produce steam, which is expanded in a steam turbine so as to produce shaft power. A first portion of the hot gas from the heat recovery steam generator is expanded in the turbine section of the gas turbine so as to produce additional shaft power. A second portion of the hot gas from the heat recovery steam generator is then used to cool the turbine section of the gas turbine, after further cooling and filtering. Since none of the turbine cooling fluid is obtained by bleeding compressed air directly from the compressor, the mass flow of the hot gas flowing through the gasifier, and, therefore, the hot gas it produces is maximized, thereby maximizing steam generation in the heat recovery steam generator.
    Type: Grant
    Filed: February 27, 1997
    Date of Patent: July 6, 1999
    Assignee: Siemens Westinghouse Power Corporation
    Inventors: Scott Thorsten Cloyd, Brian Joseph Bohinsky, Hubertus Edward Paprotna