Patents by Inventor Carnell E. Williams

Carnell E. Williams 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).

  • Publication number: 20130255253
    Abstract: A turbocharger for an internal combustion engine includes a shaft, a first turbine wheel, a compressor wheel, and a second turbine wheel. The shaft includes a first end and a second end and is supported for rotation about an axis. The first turbine wheel is mounted on the shaft proximate to the first end and configured to be rotated about the axis by post-combustion gasses emitted by the engine. The compressor wheel is mounted on the shaft between the first and second ends and configured to pressurize an airflow being received from the ambient for delivery to the engine. The second turbine wheel is mounted on the shaft proximate to the second end and configured to be rotated about the axis by a pressurized fluid. An internal combustion engine employing such a turbocharger is also disclosed.
    Type: Application
    Filed: March 28, 2012
    Publication date: October 3, 2013
    Applicant: GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Louis P. Begin, Carnell E. Williams
  • Patent number: 8197199
    Abstract: A turbocharger includes a center housing having a bearing surface configured to contact an inner surface of a unison ring. A conversion coating is impregnated onto at least the bearing surface of the center housing.
    Type: Grant
    Filed: December 2, 2008
    Date of Patent: June 12, 2012
    Assignee: GM Global Technology Operations LLC
    Inventors: Thomas A. Perry, Carnell E. Williams, Julian Velosa, Anil K. Sachdev
  • Publication number: 20120124994
    Abstract: A centrifugal compressor wheel for a turbocharger is disclosed. The wheel includes an axially extending hub having an inlet end, an outlet end, an arcuate outer surface and a shaft bore. The wheel also includes a blade array disposed on the outer surface of the hub, the blade array comprising a plurality of circumferentially-spaced, radially and axially extending, arcuate centrifugal impeller blades disposed thereon; the hub and the blade array comprising a non-woven, discontinuous-fiber-filled, polymer matrix composite material.
    Type: Application
    Filed: November 23, 2010
    Publication date: May 24, 2012
    Applicant: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: Daniel J. Hommes, Carnell E. Williams
  • Patent number: 8109256
    Abstract: An engine control system comprises a current control module and a solenoid actuator module. The current control module determines a duty cycle based on a desired current through a solenoid of an engine system and a resistance of the solenoid and corrects the resistance based on an actual current through the solenoid. The solenoid actuator module actuates the solenoid based on the duty cycle.
    Type: Grant
    Filed: November 17, 2008
    Date of Patent: February 7, 2012
    Inventors: Yun Xiao, Steven Douglas Stiles, Carnell E. Williams, Ping Ge
  • Publication number: 20110255952
    Abstract: A turbocharger compressor includes a compressor housing having a housing wall that includes a shroud that defines a central air channel and a compressor inlet in fluid communication with the central channel and an inlet duct. It also includes a compressor wheel configured to draw air into the compressor inlet from the inlet duct and create a main airflow in the central air channel axially toward a compressor outlet. The compressor also includes a bypass channel that extends between an opening in the main channel located between the compressor inlet and compressor outlet proximate the compressor blades and the compressor inlet. The compressor also includes a deflector that includes a deflector surface that is configured to direct a bypass airflow in the bypass channel, and flowing in a direction from the main channel toward the compressor inlet, into the compressor inlet axially and radially inwardly toward the compressor wheel.
    Type: Application
    Filed: April 18, 2011
    Publication date: October 20, 2011
    Applicant: GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Carnell E. Williams, Timothy J. Johnson, Tracy M. Farell, Kulwinder Singh, Gary J. Hazelton
  • Publication number: 20110067680
    Abstract: A turbocharger for an internal combustion engine includes a turbine comprising a turbine wheel attached to a turbine shaft, the turbine wheel and shaft rotatably disposed in a turbine housing, the turbine housing comprising a turbine volute conduit, the turbine volute conduit having a turbine volute inlet and an EGR conduit inlet, the EGR conduit inlet radially spaced from the turbine volute inlet along the turbine volute conduit and opening into an EGR conduit that is joined to the turbine volute conduit. The turbine volute inlet is configured for fluid communication of an exhaust gas received from an engine to the turbine wheel, the EGR conduit configured for fluid communication of the exhaust gas to an engine intake conduit. The turbocharger also includes a compressor comprising a compressor wheel attached to the turbine shaft, the compressor wheel and turbine shaft rotatably disposed in compressor housing.
    Type: Application
    Filed: September 22, 2009
    Publication date: March 24, 2011
    Applicant: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: Carnell E. Williams, Ronald M. Tkac
  • Publication number: 20100122691
    Abstract: An engine control system comprises a current control module and a solenoid actuator module. The current control module determines a duty cycle based on a desired current through a solenoid of an engine system and a resistance of the solenoid and corrects the resistance based on an actual current through the solenoid. The solenoid actuator module actuates the solenoid based on the duty cycle.
    Type: Application
    Filed: November 17, 2008
    Publication date: May 20, 2010
    Applicant: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: Yun Xiao, Steven Douglas Stiles, Carnell E. Williams, Ping Ge
  • Patent number: 7712311
    Abstract: A turbocharger assembly is provided. The turbocharger assembly includes a turbine assembly having at least one internal aerodynamic surface and a compressor assembly having at least one internal aerodynamic surface. At least one of the at least one internal aerodynamic surface of the turbine assembly and the at least one internal aerodynamic surface of the compressor assembly is at least partially coated with a catalyst material. The internal aerodynamic surfaces of the turbine assembly may include a volute, variable geometry mechanism, turbine wheel, and outlet. The internal aerodynamic surfaces of the compressor assembly may include and inlet, compressor impeller, diffuser, variable geometry mechanism, and a volute. An internal combustion engine incorporating the disclosed turbocharger assembly is also provided.
    Type: Grant
    Filed: March 14, 2007
    Date of Patent: May 11, 2010
    Assignee: GM Global Technology Operations, Inc.
    Inventors: Shouxian Ren, Carnell E. Williams
  • Publication number: 20090304500
    Abstract: A turbocharger includes a center housing having a bearing surface configured to contact an inner surface of a unison ring. A conversion coating is impregnated onto at least the bearing surface of the center housing.
    Type: Application
    Filed: December 2, 2008
    Publication date: December 10, 2009
    Applicant: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: Thomas A. Perry, Carnell E. Williams, Julian Velosa, Anil K. Sachdev
  • Publication number: 20080223037
    Abstract: A turbocharger assembly is provided. The turbocharger assembly includes a turbine assembly having at least one internal aerodynamic surface and a compressor assembly having at least one internal aerodynamic surface. At least one of the at least one internal aerodynamic surface of the turbine assembly and the at least one internal aerodynamic surface of the compressor assembly is at least partially coated with a catalyst material. The internal aerodynamic surfaces of the turbine assembly may include a volute, variable geometry mechanism, turbine wheel, and outlet. The internal aerodynamic surfaces of the compressor assembly may include and inlet, compressor impeller, diffuser, variable geometry mechanism, and a volute. An internal combustion engine incorporating the disclosed turbocharger assembly is also provided.
    Type: Application
    Filed: March 14, 2007
    Publication date: September 18, 2008
    Inventors: Shouxian Ren, Carnell E. Williams