Patents by Inventor Josef Scott Cummins
Josef Scott Cummins 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).
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Patent number: 9194257Abstract: Systems and devices configured to shield portions of turbine conduits from contact with a working fluid flow and reduce the associated thermal gradients therein are disclosed. In one embodiment, a sleeve includes: a base portion defining a shield aperture, the base portion including an external surface configured to contact an internal surface of a turbine conduit; and a neck portion connected to the base portion and defining a neck aperture proximate a terminus of the turbine conduit, the neck aperture fluidly connected to the shield aperture.Type: GrantFiled: August 8, 2012Date of Patent: November 24, 2015Assignee: General Electric CompanyInventors: Mayur Abhay Keny, Josef Scott Cummins, Scott Jacob Huth, Thangaraj Subbareddyar
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Patent number: 8998568Abstract: A turbine is provided and includes a rotor, which is rotatable about a centerline thereof, a sensor to measure a condition at a point of measurement interest defined on the rotor at a radial distance from the centerline, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder to secure the sensor and a portion of the communication system on the rotor proximate to the point of measurement interest.Type: GrantFiled: October 21, 2010Date of Patent: April 7, 2015Assignee: General Electric CompanyInventors: Kurt Kramer Schleif, Gregory Quentin Brown, Philip Michael Caruso, Fernando Jorge Casanova, Seung-Woo Choi, Josef Scott Cummins, Matthew Ryan Ferslew, Andrew Clifford Hart, Robert David Jones, Jong Youn Pak, Francesco Soranna
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Publication number: 20140044533Abstract: Systems and devices configured to shield portions of turbine conduits from contact with a working fluid flow and reduce the associated thermal gradients therein are disclosed. In one embodiment, a sleeve includes: a base portion defining a shield aperture, the base portion including an external surface configured to contact an internal surface of a turbine conduit; and a neck portion connected to the base portion and defining a neck aperture proximate a terminus of the turbine conduit, the neck aperture fluidly connected to the shield aperture.Type: ApplicationFiled: August 8, 2012Publication date: February 13, 2014Applicant: GENERAL ELECTRIC COMPANYInventors: Mayur Abhay Keny, Josef Scott Cummins, Scott Jacob Huth, Thangaraj Subbareddyar
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Patent number: 8511976Abstract: In accordance with one embodiment, a system includes a multi-stage turbine including a first turbine stage including a first wheel having multiple first slots spaced circumferentially about the first wheel, and multiple first blade segments each coupled to at least one of the multiple first slots. The multi-stage turbine also includes a second turbine stage including a second wheel having multiple second slots spaced circumferentially about the second wheel, and multiple second blade segments each coupled to at least one of the multiple second slots. The multi-stage turbine further includes a one-piece interstage seal extending axially between the first and second turbine stages, wherein the one-piece interstage seal comprises a first radial support coupled to the first wheel and a second radial support coupled to the second wheel, and the one-piece interstage seal extends circumferentially across at least two of the multiple first slots or at least two of the multiple second slots.Type: GrantFiled: August 2, 2010Date of Patent: August 20, 2013Assignee: General Electric CompanyInventors: Josef Scott Cummins, Ian David Wilson
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Patent number: 8235656Abstract: In one embodiment, a catenary seal structure may be mechanically supported only by two adjacent rotor wheels to isolate a volume between the two adjacent rotor wheels. The catenary seal structure may be annularly disposed about the rotational axis of the adjacent rotor wheels.Type: GrantFiled: February 13, 2009Date of Patent: August 7, 2012Assignee: General Electric CompanyInventors: Ian Wilson, Kenneth Black, Josef Scott Cummins
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Patent number: 8220319Abstract: A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wiring including a first wiring section coupled to the sensor, a second wiring section and a first connection by which the first and second wiring sections are connectable, a second connection by which the second wiring section transmits a signal reflective of the detected condition to a non-rotating recording element and a temperature compensation module disposed on the second wiring section to adjust the signal.Type: GrantFiled: October 21, 2010Date of Patent: July 17, 2012Assignee: General Electric CompanyInventors: Kurt Kramer Schleif, Gregory Quentin Brown, Philip Michael Caruso, Fernando Jorge Casanova, Seung-Woo Choi, Josef Scott Cummins, Matthew Ryan Ferslew, Andrew Clifford Hart, Robert David Jones, Jong Youn Pak, Francesco Soranna
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Publication number: 20120134782Abstract: A method for assembling a rotary machine includes providing a first rotatable element. The method also includes coupling a second rotatable element to the first rotatable element. The first rotatable element and the second rotatable element at least partially define a cavity therein and at least one conduit extending substantially axially therebetween. Further, the method includes coupling a purge device including at least one radial channel defined therein and extending to the first rotatable element and to the second rotatable element such that the at least one radial channel is coupled in flow communication with the cavity and with the at least one axial conduit.Type: ApplicationFiled: November 30, 2010Publication date: May 31, 2012Inventors: Creston Lewis Dempsey, Seung-Woo Choi, Raymond Joseph Lecuyer, Matthew Ryan Ferslew, Jong Youn Pak, Josef Scott Cummins
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Publication number: 20120096961Abstract: A turbine is provided and includes a component having a body, which is rotatable about a rotor centerline and which is formed to define a cavity radially proximate to a point of measurement interest defined at a radial distance from the centerline, a sensor to measure a condition at the point of measurement interest, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder insertible into the cavity to secure the sensor proximate to the point of measurement interest.Type: ApplicationFiled: October 21, 2010Publication date: April 26, 2012Applicant: GENERAL ELECTRIC COMPANYInventors: Kurt Kramer Schleif, Gregory Quentin Brown, Philip Michael Caruso, Fernando Jorge Casanova, Seung-Woo Choi, Josef Scott Cummins, Matthew Ryan Ferslew, Andrew Clifford Hart, Robert David Jones, Jong Youn Pak
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Publication number: 20120096934Abstract: A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wiring including a first wiring section coupled to the sensor, a second wiring section and a first connection by which the first and second wiring sections are connectable, a second connection by which the second wiring section transmits a signal reflective of the detected condition to a non-rotating recording element and a temperature compensation module disposed on the second wiring section to adjust the signal.Type: ApplicationFiled: October 21, 2010Publication date: April 26, 2012Applicant: GENERAL ELECTRIC COMPANYInventors: Kurt Kramer Schleif, Gregory Quentin Brown, Philip Michael Caruso, Fernando Jorge Casanova, Seung-Woo Choi, Josef Scott Cummins, Matthew Ryan Ferslew, Andrew Clifford Hart, Robert David Jones, Jong Youn Pak, Francesco Soranna
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Publication number: 20120096946Abstract: A turbine is provided and includes a rotor, which is rotatable about a centerline thereof, a sensor to measure a condition at a point of measurement interest defined on the rotor at a radial distance from the centerline, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder to secure the sensor and a portion of the communication system on the rotor proximate to the point of measurement interest.Type: ApplicationFiled: October 21, 2010Publication date: April 26, 2012Applicant: GENERAL ELECTRIC COMPANYInventors: Kurt Kramer Schleif, Gregory Quentin Brown, Philip Michael Caruso, Fernando Jorge Casanova, Seung-Woo Choi, Josef Scott Cummins, Matthew Ryan Ferslew, Andrew Clifford Hart, Robert David Jones, Jong Youn Pak, Francesco Soranna
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Publication number: 20120027584Abstract: In accordance with one embodiment, a system includes a multi-stage turbine including a first turbine stage including a first wheel having multiple first slots spaced circumferentially about the first wheel, and multiple first blade segments each coupled to at least one of the multiple first slots. The multi-stage turbine also includes a second turbine stage including a second wheel having multiple second slots spaced circumferentially about the second wheel, and multiple second blade segments each coupled to at least one of the multiple second slots. The multi-stage turbine further includes a one-piece interstage seal extending axially between the first and second turbine stages, wherein the one-piece interstage seal comprises a first radial support coupled to the first wheel and a second radial support coupled to the second wheel, and the one-piece interstage seal extends circumferentially across at least two of the multiple first slots or at least two of the multiple second slots.Type: ApplicationFiled: August 2, 2010Publication date: February 2, 2012Applicant: General Electric CompanyInventors: Josef Scott Cummins, Ian David Wilson
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Publication number: 20120003076Abstract: A method for assembling a rotating machine includes providing a rotating element including a plurality of rotor wheels. The method also includes positioning the rotating element such that at least a portion of a stationary portion extends at least partially about the rotating element. The method further includes assembling an interstage seal mechanism including coupling at least a portion of a first hook device to the rotating element, and also including coupling at least a portion of a second hook device to the first hook device. The first hook device and the second hook device are radially inboard of at least a portion of the stationary portion.Type: ApplicationFiled: June 30, 2010Publication date: January 5, 2012Inventors: Josef Scott Cummins, Ian David Wilson
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Publication number: 20100209233Abstract: In one embodiment, a catenary seal structure may be mechanically supported only by two adjacent rotor wheels to isolate a volume between the two adjacent rotor wheels. The catenary seal structure may be annularly disposed about the rotational axis of the adjacent rotor wheels.Type: ApplicationFiled: February 13, 2009Publication date: August 19, 2010Applicant: GENERAL ELECTRIC COMPANYInventors: Ian Wilson, Kenneth Black, Josef Scott Cummins
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Patent number: 7597542Abstract: A method enables a stator assembly for a turbine engine to be assembled. The method comprises forming a recess within a portion of each base, and coupling the stator vanes within the turbine engine in a circumferentially-spaced arrangement such that the recessed portion of each base facilitates reducing excitation responses of each of the plurality of stator vanes during engine operation.Type: GrantFiled: August 30, 2005Date of Patent: October 6, 2009Assignee: General Electric CompanyInventors: Hani Ikram Noshi, Steven E. Tomberg, Josef Scott Cummins
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Patent number: 7467926Abstract: Tenth stage stator vanes for a compressor comprise airfoil profiles substantially in accordance with Cartesian coordinate values of x, Y and Z set forth in inches in Table I, wherein the Z coordinate values are perpendicular distances from planes normal to a radius from the compressor centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at a radial aerodynamic section of the airfoil. X and Y are coordinate values defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled to provide a scaled-up or scaled-down airfoil section for each stator vane.Type: GrantFiled: June 9, 2006Date of Patent: December 23, 2008Assignee: General Electric CompanyInventors: John David Stampfli, Josef Scott Cummins
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Publication number: 20070286718Abstract: Tenth stage stator vanes for a compressor comprise airfoil profiles substantially in accordance with Cartesian coordinate values of x, Y and Z set forth in inches in Table I, wherein the Z coordinate values are perpendicular distances from planes normal to a radius from the compressor centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at a radial aerodynamic section of the airfoil. X and Y are coordinate values defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled to provide a scaled-up or scaled-down airfoil section for each stator vane.Type: ApplicationFiled: June 9, 2006Publication date: December 13, 2007Applicant: General Electric CompanyInventors: John David Stampfli, Josef Scott Cummins