Patents by Inventor Michael Nesteroff

Michael Nesteroff 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: 10408226
    Abstract: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of a segregated impeller shroud in a turbine engine. The system comprises a driving mechanism coupled to a portion of a segregated impeller shroud. The driving mechanism comprises a driving arm and threaded axial member configured to translate motion of an actuator ring into axially forward and aft motion of the portion of the segregated impeller shroud.
    Type: Grant
    Filed: May 26, 2016
    Date of Patent: September 10, 2019
    Assignee: ROLLS-ROYCE CORPORATION
    Inventors: Nathan Ottow, Jonathan Acker, Nate Cooper, Mark Whitlock, Michael Nesteroff
  • Patent number: 10352329
    Abstract: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a thermal driver coupled between the impeller shroud and engine casing by hinged linkages. The thermal driver includes an annular ring and annular seal which together define thermal driver cavity. Relatively warm or relatively cool air supplied to the thermal driver cavity cause expansion and contraction, respectively, of the annular ring which is translated by linkages into axially forward and aft motion, respectively.
    Type: Grant
    Filed: May 26, 2016
    Date of Patent: July 16, 2019
    Assignee: ROLLS-ROYCE CORPORATION
    Inventors: Michael Nesteroff, Jonathan Acker, Nate Cooper, Nathan Ottow
  • Patent number: 10309409
    Abstract: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a high pressure air source, an air piston mounted between an engine casing and the shroud and adapted to receive high pressure air from the high pressure air source, a mounting arm coupling the shroud and air piston, and a slidable coupling adapted to allow axial movement of the shroud and joining the shroud to an axial member.
    Type: Grant
    Filed: May 26, 2016
    Date of Patent: June 4, 2019
    Assignee: ROLLS-ROYCE CORPORATION
    Inventors: Michael Nesteroff, Jonathan Acker, Jeffrey Crutchfield, Nathan Ottow
  • Publication number: 20170342994
    Abstract: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a thermal driver coupled between the impeller shroud and engine casing by hinged linkages. The thermal driver includes an annular ring and annular seal which together define thermal driver cavity. Relatively warm or relatively cool air supplied to the thermal driver cavity cause expansion and contraction, respectively, of the annular ring which is translated by linkages into axially forward and aft motion, respectively.
    Type: Application
    Filed: May 26, 2016
    Publication date: November 30, 2017
    Applicant: Rolls-Royce Corporation
    Inventors: Michael Nesteroff, Jonathan Acker, Nate Cooper, Nathan Ottow
  • Publication number: 20170343001
    Abstract: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a high pressure air source, an air piston mounted between an engine casing and the shroud and adapted to receive high pressure air from the high pressure air source, a mounting arm coupling the shroud and air piston, and a slidable coupling adapted to allow axial movement of the shroud and joining the shroud to an axial member.
    Type: Application
    Filed: May 26, 2016
    Publication date: November 30, 2017
    Applicant: Rolls-Royce Corporation
    Inventors: Michael Nesteroff, Jonathan Acker, Jeffrey Crutchfield, Nathan Ottow
  • Publication number: 20170342996
    Abstract: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a high pressure air source, an air piston mounted between an engine casing and the shroud and adapted to receive high pressure air from the high pressure air source, a mounting arm coupling the shroud and air piston, and a slidable coupling adapted to allow axial movement of the shroud and joining the shroud to an axial member.
    Type: Application
    Filed: August 11, 2016
    Publication date: November 30, 2017
    Applicants: Rolls-Royce Corporation, Rolls-Royce North American Technologies Inc.
    Inventors: Michael Nesteroff, Jonathan Acker, Jeffrey Crutchfield, Nate Cooper, Mark Whitlock, Nathan Ottow
  • Publication number: 20170342995
    Abstract: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of a segregated impeller shroud in a turbine engine. The system comprises a driving mechanism coupled to a portion of a segregated impeller shroud. The driving mechanism comprises a driving arm and threaded axial member configured to translate motion of an actuator ring into axially forward and aft motion of the portion of the segregated impeller shroud.
    Type: Application
    Filed: May 26, 2016
    Publication date: November 30, 2017
    Applicant: Rolls-Royce Corporation
    Inventors: Nathan Ottow, Jonathan Acker, Nate Cooper, Mark Whitlock, Michael Nesteroff