Patents by Inventor Kevin Slupski

Kevin Slupski 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: 8480357
    Abstract: A variable geometry turbocharger assembly comprises a unison ring which rotates about a longitudinal axis defined by a shaft on which a turbine wheel and compressor wheel are attached in order to pivot a plurality of vanes and thereby control a flow of exhaust gas to the turbine wheel. The unison ring rotates on at least one guide pin which is secured to the turbocharger. The guide pins may be press-fit into apertures in a center housing at an outer pilot surface. In other embodiments the guide pins may be press-fit into a different part of the turbocharger such as a nozzle ring. The guide pins may each have a wear surface which defines a circumferential radius of curvature which is substantially equal to a circumferential radius of curvature of a radially inner surface of the unison ring.
    Type: Grant
    Filed: November 9, 2009
    Date of Patent: July 9, 2013
    Assignee: Honeywell International Inc.
    Inventors: Kolja Nikolic, Michael Moyer, George Adeff, Kevin Slupski, Matthew Oakes, Dennis L. Brookshire
  • Publication number: 20110110768
    Abstract: A variable geometry turbocharger assembly comprises a unison ring which rotates about a longitudinal axis defined by a shaft on which a turbine wheel and compressor wheel are attached in order to pivot a plurality of vanes and thereby control a flow of exhaust gas to the turbine wheel. The unison ring rotates on at least one guide pin which is secured to the turbocharger. The guide pins may be press-fit into apertures in a center housing at an outer pilot surface. In other embodiments the guide pins may be press-fit into a different part of the turbocharger such as a nozzle ring. The guide pins may each have a wear surface which defines a circumferential radius of curvature which is substantially equal to a circumferential radius of curvature of a radially inner surface of the unison ring.
    Type: Application
    Filed: November 9, 2009
    Publication date: May 12, 2011
    Inventors: Kolja Nikolic, Michael Moyer, George Adeff, Kevin Slupski, Matthew Oakes, Dennis L. Brookshire
  • Publication number: 20050123394
    Abstract: A compressor diffuser for a vehicle engine turbocharger, the diffuser comprising: a diffuser housing having a gas flow path having a side wall connecting a gas inlet to a gas outlet; a plurality of pivotally mounted diffuser vanes arranged in the flow path to control gas flow, and a vane angle control device for adjusting the angle of each of the plurality of vanes in the flow path; the control device comprising a unison ring coupled to the plurality of vanes in such a way that rotation of the unison ring pivots each of the vanes by interaction of a cam surface with a respective cam follower.
    Type: Application
    Filed: August 9, 2004
    Publication date: June 9, 2005
    Inventors: Nathan McArdle, Stephen Ellis, Hua Chen, Steve Arnold, John Allen, Kevin Slupski
  • Publication number: 20050123397
    Abstract: A compressor diffuser for a vehicle engine turbocharger, the diffuser comprising: a diffuser housing having a gas flow path having a side wall connecting a gas inlet to a gas outlet; a plurality of pivotally mounted diffuser vanes arranged in the flow path to control gas flow, and a vane angle control device for adjusting the angle of each of the plurality of vanes in the flow path; the control device comprising a unison ring coupled to the plurality of vanes in such a way that rotation of the unison ring pivots each of the vanes by interaction of a cam surface with a respective cam follower.
    Type: Application
    Filed: December 3, 2003
    Publication date: June 9, 2005
    Inventors: Nathan McArdle, Stephen Ellis, Steven Arnold, John Allen, Kevin Slupski
  • Publication number: 20050066657
    Abstract: A variable geometry turbocharger includes vanes disposed therein having an inner airfoil surface oriented adjacent a turbine wheel, and an outer airfoil surface oriented opposite and parallel to the inner airfoil surface. The vane includes first and second axial surfaces that are each positioned perpendicular to and interposed between the inner and outer airfoil surfaces. A vane leading edge is positioned along a first inner and outer airfoil surface junction, and a trailing edge is positioned along a second inner and outer airfoil surface junction. One or more of the first and second axial surfaces have a composite construction comprising a solid section that extends a distance from the leading edge towards the trailing edge, and a cored-out section that extends a distance from the trailing edge towards the leading edge.
    Type: Application
    Filed: September 25, 2003
    Publication date: March 31, 2005
    Applicant: Honeywell International Inc.
    Inventors: Brent Zollinger, Kevin Slupski, Douglas Riethmeier
  • Patent number: 6269642
    Abstract: A variable geometry turbocharger employs multiple vanes in the turbine inlet with a unison ring and integral cast wall in the turbine housing forming the nozzle walls. The unison ring incorporates actuation slots receiving tabs on the vanes for opening the closing the nozzle area upon rotation of the unison ring. An integral electrohydraulic actuator rotates the unison ring through a rack and pinion driven crank shaft with direct position feedback to the spring biased variable current solenoid via a cam on the crank shaft.
    Type: Grant
    Filed: September 30, 1999
    Date of Patent: August 7, 2001
    Assignee: AlliedSignal Inc.
    Inventors: Steven Don Arnold, Steven P. Martin, Kevin Slupski, Voytek Kanigowski