Adebukola O Benson

age ~46

from Pewaukee, WI

Also known as:
  • Adebukola Benson
  • Adebukola Bwenson
  • Adebukola O'Benson

Adebukola Benson Phones & Addresses

  • Pewaukee, WI
  • Brookfield, WI
  • Greenville, SC
  • 14 Open Range Ln, Simpsonville, SC 29681 • 8649630194
  • Baltimore, MD

Education

  • Degree:
    High school graduate or higher

Us Patents

  • Airfoil Cooling Hole Flag Region

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  • US Patent:
    20110236220, Sep 29, 2011
  • Filed:
    Mar 25, 2010
  • Appl. No.:
    12/731783
  • Inventors:
    Adebukola Benson - Greenville SC, US
    Gary Michael Itzel - Simpsonville SC, US
  • Assignee:
    GENERAL ELECTRIC COMPANY - Schenectady NY
  • International Classification:
    F01D 5/18
  • US Classification:
    416 97 R
  • Abstract:
    An airfoil is provided and includes a body formed to define a substantially radially extending cooling hole therein, which is configured to be receptive of a supply of a coolant for removing heat from the body, and a flag region therein, which is fluidly communicative with the cooling hole and thereby configured to be receptive of a portion of the supply of the coolant such that the coolant portion is directed to form a vortex within the flag region to increase heat removal from the body beyond that provided by the coolant flow through the cooling hole.
  • Turbomachine Airfoil Component And Cooling Method Therefor

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  • US Patent:
    20120171047, Jul 5, 2012
  • Filed:
    Jan 3, 2011
  • Appl. No.:
    12/983400
  • Inventors:
    Gary Michael Itzel - Simpsonville SC, US
    Adebukola O. Benson - Simpsonville SC, US
  • Assignee:
    GENERAL ELECTRIC COMPANY - Schenectady NY
  • International Classification:
    F01D 5/18
  • US Classification:
    416 97 R
  • Abstract:
    An airfoil component for use in a turbomachine, and method of promoting the heat transfer characteristics within the component. The component includes an airfoil portion having a span-wise direction delimited by an airfoil root and airfoil tip, and a chord-wise direction delimited by leading and trailing edges. A chamber within the airfoil portion contains a permeable foam member. The chamber is fluidically connected to a cooling fluid source and to a cooling hole through first and second passages, respectively, within the airfoil portion. The chamber is located relative to the first and second passages so as to be offset in the chord-wise direction therefrom so that cooling fluid entering the chamber through the first passage is diverted by the foam member in the chord-wise direction before exiting the airfoil portion through the cooling hole.
  • Gas Turbine Pattern Swirl Film Cooling

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  • US Patent:
    20130195650, Aug 1, 2013
  • Filed:
    Jan 27, 2012
  • Appl. No.:
    13/359691
  • Inventors:
    Adebukola O. Benson - Greenville SC, US
    Xiuzhang James Zhang - Greenville SC, US
    Gary Michael Itzel - Greenville SC, US
  • International Classification:
    F01D 5/18
  • US Classification:
    416 1, 416 97 R
  • Abstract:
    A turbine airfoil includes a blade having a leading and trailing edges and an internal cooling circuit, and a plurality of film holes extending between the internal cooling circuit and an exterior of the blade. The plurality of film holes are shaped to generate a swirling flow exiting the film holes adjacent the leading edge to thereby enhance local convection and provide an insulating barrier to gaspath flow.
  • Cooling Arrangement For Platform Region Of Turbine Rotor Blade

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  • US Patent:
    20140064984, Mar 6, 2014
  • Filed:
    Aug 31, 2012
  • Appl. No.:
    13/600782
  • Inventors:
    Xiuzhang James Zhang - Simpsonville SC, US
    Camilo Andres Sampayo - Greer SC, US
    Adebukola Oluwaseun Benson - Simpsonville SC, US
    Christopher William Kester - Greenville SC, US
  • International Classification:
    F01D 5/18
  • US Classification:
    416 97 R
  • Abstract:
    A platform cooling arrangement in a turbine rotor blade having a platform at an interface between an airfoil and a root. The platform may include a pressure side slashface and a suction side slashface. The platform cooling arrangement may include: a cooling channel formed within the interior of the platform, the cooling channel extending from a first end toward one of the pressure side slashface and the suction side slashface. At a second end, the cooling channel may include a pocket. The pocket may include an abrupt increase in cross-sectional flow area just before the cooling channel reaches the slashface.

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