Patents by Inventor Sean Rylance

Sean Rylance 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: 10494990
    Abstract: An exhaust gas turbocharger (1) including a compressor housing (2), a bearing housing (3), a turbine housing (4) in which a turbine wheel (5) is arranged, which has a housing inlet (6), which has a turbine spiral (7) connecting to the housing inlet (6), which has a housing outlet (8), and which has a wastegate arrangement (9), which in the open state brings the housing inlet (6) into flow connection with the housing outlet (8) for guiding a wastegate mass flow. The wastegate insert part (10) is arranged in the turbine housing (4) between the turbine wheel (5) and the housing outlet (8) and the open wastegate arrangement (9) introduces the wastegate mass flow into the wastegate insert arrangement (9).
    Type: Grant
    Filed: February 2, 2016
    Date of Patent: December 3, 2019
    Assignee: BorgWarner Inc.
    Inventors: Rolf Sauerstein, Philip Christoph Parma, Sean Rylance, Andrew Day
  • Patent number: 10273827
    Abstract: A bearing housing, or integrated turbocharger housing, with the oil, and optionally air and water galleries, included as as-cast features, thereby avoiding the problems, design limitations and expense associated with conventional post-casting machining. The method of casting preferably uses lost foam casting, or a technique similar to lost foam casting but in which a ceramic shell is formed on the foam form prior to metal casting, but can use any of a variety of casting techniques or a combination of two or more techniques.
    Type: Grant
    Filed: January 17, 2013
    Date of Patent: April 30, 2019
    Assignee: BorgWarner Inc.
    Inventors: Simon Malins, Sean Rylance, James Finley, Rob Daniels
  • Patent number: 10240469
    Abstract: A turbocharger (1) includes a compressor section and a cast turbine section. The turbine section includes a turbine wheel (4), and a turbine housing (11) that defines a gas inlet (13), a gas outlet (10), a volute (9) disposed between the gas inlet (13) and the gas outlet (10). The turbine housing (11) also includes vanes (20) that protrude integrally from, and have a fixed orientation relative to, an inner surface of the turbine housing (11). The turbine wheel (4) is disposed in the turbine housing (11) between the volute (9) and the gas outlet (10), and the vanes (20) are disposed in the turbine housing (11) between the turbine wheel (4) and the volute (9). A method of casting the turbine housing (11) and the vanes (20) together as a single piece is described.
    Type: Grant
    Filed: March 2, 2015
    Date of Patent: March 26, 2019
    Assignee: BorgWarner Inc.
    Inventors: Sean Rylance, Nathan McArdle
  • Patent number: 10006468
    Abstract: Conventionally, turbocharger bearing housings are cast, and then oil passageways are drilled or bored into the casting. As a result, bores are limited to straight lines extending from drill access points. Greater design flexibility is provided by pre-staging in a mold a collection of metal pipes which will define one or more of oil, air and water galleries, and then casting a bearing housing around the pipes. This provides almost unlimited freedom in shaping and locating the oil bores and other features.
    Type: Grant
    Filed: March 19, 2013
    Date of Patent: June 26, 2018
    Assignee: BorgWarner Inc.
    Inventors: Michael Fischer, Martin Bihy, Sean Rylance, Rob Daniels, James Finley
  • Patent number: 9926840
    Abstract: A turbine (32) section of a turbocharger (30) includes a turbine wheel (37) disposed in a turbine housing (33), the turbine housing (33) defining a gas inlet (34), a volute configured to direct gas from the inlet (34) to the turbine (32) wheel, and a gas outlet. A rotary diverter valve (100, 200) is disposed in the gas inlet (34) upstream of the volute, and provides three modes of controlling exhaust gas flow about the turbocharger (30).
    Type: Grant
    Filed: February 3, 2015
    Date of Patent: March 27, 2018
    Assignee: BorgWarner Inc.
    Inventors: James Mawer, Kiumars Shoghi, Steve Birnie, Sean Rylance
  • Publication number: 20180023459
    Abstract: An exhaust gas turbocharger (1) including a compressor housing (2), a bearing housing (3), a turbine housing (4) in which a turbine wheel (5) is arranged, which has a housing inlet (6), which has a turbine spiral (7) connecting to the housing inlet (6), which has a housing outlet (8), and which has a wastegate arrangement (9), which in the open state brings the housing inlet (6) into flow connection with the housing outlet (8) for guiding a wastegate mass flow. The wastegate insert part (10) is arranged in the turbine housing (4) between the turbine wheel (5) and the housing outlet (8) and the open wastegate arrangement (9) introduces the wastegate mass flow into the wastegate insert arrangement (9).
    Type: Application
    Filed: February 2, 2016
    Publication date: January 25, 2018
    Inventors: Rolf SAUERSTEIN, Philip Christoph PARMA, Sean RYLANCE, Andrew DAY
  • Publication number: 20180023460
    Abstract: A turbine (32) section of a turbocharger (30) includes a turbine wheel (37) disposed in a turbine housing (33), the turbine housing (33) defining a gas inlet (34), a volute configured to direct gas from the inlet (34) to the turbine (32) wheel, and a gas outlet. A rotary diverter valve (100, 200) is disposed in the gas inlet (34) upstream of the volute, and provides three modes of controlling exhaust gas flow about the turbocharger (30).
    Type: Application
    Filed: February 3, 2015
    Publication date: January 25, 2018
    Inventors: James MAWER, Kiumars SHOGHI, Steve BIRNIE, Sean RYLANCE
  • Publication number: 20170081970
    Abstract: A turbocharger (1) includes a compressor section and a cast turbine section. The turbine section includes a turbine wheel (4), and a turbine housing (11) that defines a gas inlet (13), a gas outlet (10), a volute (9) disposed between the gas inlet (13) and the gas outlet (10). The turbine housing (11) also includes vanes (20) that protrude integrally from, and have a fixed orientation relative to, an inner surface of the turbine housing (11). The turbine wheel (4) is disposed in the turbine housing (11) between the volute (9) and the gas outlet (10), and the vanes (20) are disposed in the turbine housing (11) between the turbine wheel (4) and the volute (9). A method of casting the turbine housing (11) and the vanes (20) together as a single piece is described.
    Type: Application
    Filed: March 2, 2015
    Publication date: March 23, 2017
    Inventors: Sean RYLANCE, Nathan MCARDLE
  • Publication number: 20170067472
    Abstract: A turbocharger (1) includes compressor and turbine wheels (4, 5) and a shaft (6) that connects the compressor wheel (5) to the turbine wheel (4). The shaft (6) is supported by a thrust bearing assembly (20) that includes a pair of thrust washers (42a, 42b) mounted on the shaft (6), a hollow, cylindrical spacer (80) disposed on the shaft (6) between and abutting first faces (44) of the thrust washers (42a, 42b), and a thrust bearing (100) supported on the spacer (80) between the thrust washers (42a, 42b). One of the thrust bearing (100) or the first and second thrust washers (42a, 42b) includes a copper-alloy lining (60) where the lining (60) is provided in a first region (58a) and in a second region (58b), and the remainder of the thrust bearing (100) or the first and second thrust washers (42a, 42b) is lining free.
    Type: Application
    Filed: February 12, 2015
    Publication date: March 9, 2017
    Inventors: Andrew DAY, Tristram PALMER-WHITE, Sean RYLANCE, Martin JARVIS
  • Publication number: 20150330405
    Abstract: Conventionally, turbocharger bearing housings are cast, and then oil passageways are drilled or bored into the casting. As a result, bores are limited to straight lines extending from drill access points. Greater design flexibility is provided by pre-staging in a mold a collection of metal pipes which will define one or more of oil, air and water galleries, and then casting a bearing housing around the pipes. This provides almost unlimited freedom in shaping and locating the oil bores and other features.
    Type: Application
    Filed: March 19, 2013
    Publication date: November 19, 2015
    Inventors: Michael Fischer, Martin Bihy, Sean Rylance, Rob Daniels, James Finley
  • Patent number: 9163558
    Abstract: A product for use with a turbocharger that may include a complex sealing path between a lubricated area of a housing and a compressor wheel.
    Type: Grant
    Filed: March 11, 2015
    Date of Patent: October 20, 2015
    Assignee: BorgWarner Inc.
    Inventors: Sanjit Chaggar, Martin Jarvis, Sean Rylance
  • Publication number: 20140369811
    Abstract: A bearing housing, or integrated turbocharger housing, with the oil, and optionally air and water galleries, included as as-cast features, thereby avoiding the problems, design limitations and expense associated with conventional post-casting machining. The method of casting preferably uses lost foam casting, or a technique similar to lost foam casting but in which a ceramic shell is formed on the foam form prior to metal casting, but can use any of a variety of casting techniques or a combination of two or more techniques.
    Type: Application
    Filed: January 17, 2013
    Publication date: December 18, 2014
    Applicant: BorgWarner Inc.
    Inventors: Simon Malins, Sean Rylance, James Finley, Rob Daniels