Patents by Inventor Sukeyuki Kobayashi

Sukeyuki Kobayashi 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: 10767500
    Abstract: There are provided techniques and apparatuses for fan blade pitch setting. For example, there is provided an impeller including a ring disposed in a hub of the impeller. The ring can include a recess shaped and positioned to impart a specified pitch angle to a blade extending outwardly from the ring through the hub.
    Type: Grant
    Filed: May 6, 2016
    Date of Patent: September 8, 2020
    Assignee: GE AVIATION SYSTEMS, LLC
    Inventor: Sukeyuki Kobayashi
  • Publication number: 20190390681
    Abstract: A fan with a housing defining an interior and a flow path therein and a valve assembly including a valve element disposed in the flow path and configured to rotate between an opened position and a closed position, wherein the valve element closes the flow path and a linkage assembly and a method of operating.
    Type: Application
    Filed: September 6, 2019
    Publication date: December 26, 2019
    Inventor: Sukeyuki Kobayashi
  • Patent number: 10408218
    Abstract: A fan with a housing defining an interior and a flow path therein and a valve assembly including a valve element disposed in the flow path and configured to rotate between an opened position and a closed position, wherein the valve element closes the flow path and a linkage assembly and a method of operating.
    Type: Grant
    Filed: November 21, 2016
    Date of Patent: September 10, 2019
    Assignee: GE Aviation Systems LLC
    Inventor: Sukeyuki Kobayashi
  • Patent number: 10240609
    Abstract: An impeller fan assembly that includes a housing, a stator, a rotor having a hub and an annular array of non-stationary blades extending from the hub, at least two spaced apart bearings mounted to the stator, and a pump in fluid communication with the bearings to provide fluid to the bearings. A screw pump is provided within the hollow portion of the shaft. Inlet of the screw pump is fluidly coupled to the sump and outlet is in fluid communication with the bearings. Rotation of the screw pump pumps fluid from the sump to the bearings. A de-swirler is provided within the sump to reduce rotational movement of the fluid within the sump. The de-swirler has a hub with fixed curved vanes extending from the centerline of the hub. The curved vanes have curvature in a direction opposite from a rotational direction of the screw pump.
    Type: Grant
    Filed: May 29, 2015
    Date of Patent: March 26, 2019
    Assignee: GE Aviation Systems LLC
    Inventors: Sukeyuki Kobayashi, Frank Leslie Sincox, III, Richard George Hext, III
  • Publication number: 20180142692
    Abstract: A fan with a housing defining an interior and a flow path therein and a valve assembly including a valve element disposed in the flow path and configured to rotate between an opened position and a closed position, wherein the valve element closes the flow path and a linkage assembly and a method of operating.
    Type: Application
    Filed: November 21, 2016
    Publication date: May 24, 2018
    Inventor: Sukeyuki Kobayashi
  • Publication number: 20170321561
    Abstract: There are provided techniques and apparatuses for fan blade pitch setting. For example, there is provided an impeller including a ring disposed in a hub of the impeller. The ring can include a recess shaped and positioned to impart a specified pitch angle to a blade extending outwardly from the ring through the hub.
    Type: Application
    Filed: May 6, 2016
    Publication date: November 9, 2017
    Inventor: Sukeyuki Kobayashi
  • Publication number: 20160177823
    Abstract: A turbine engine system includes an inlet particle separator receiving an inlet fluid flow and having a clean outlet for a first flow of substantially clean fluid, and a scavenge outlet for a second flow of scavenge fluid. A fluid pump communicates with the scavenge outlet. The flow of scavenge fluid through the fluid pump is selectively regulated.
    Type: Application
    Filed: December 22, 2014
    Publication date: June 23, 2016
    Inventors: Firas Younes, Sukeyuki Kobayashi
  • Patent number: 9217436
    Abstract: An impeller fan assembly that includes a housing, a stator, a rotor having a hub and an annular array of non-stationary blades extending from the hub, at least two spaced apart bearings mounted to the stator, and a pump in fluid communication with the bearings to provide fluid to the bearings.
    Type: Grant
    Filed: August 10, 2012
    Date of Patent: December 22, 2015
    Assignee: GE AVIATION SYSTEMS LLC
    Inventors: Sukeyuki Kobayashi, Frank Leslie Sincox, III, Richard George Hext, III
  • Publication number: 20150167692
    Abstract: An apparatus for a fan having an impeller with a hub and a plurality of blades extending from the hub includes a hub cap configured to mount to the hub of the impeller. The hub cap can include a plurality of slots corresponding to the blades of the impeller. The slots are sized to receive the blades when the hub cap is mounted to the hub, which shortens the working length of the blades.
    Type: Application
    Filed: December 12, 2013
    Publication date: June 18, 2015
    Applicant: GE Aviation Systems LLC
    Inventor: Sukeyuki Kobayashi
  • Publication number: 20140064958
    Abstract: A fan assembly that includes a housing having an inner peripheral wall defining a flow through opening, a stator located within the through opening and comprising an annular array of stationary blades provided along the inner peripheral wall, a rotor comprising a hub having a front wall supporting an outer peripheral wall having a forward balancing ring and an aft balancing ring, and an annular array of non-stationary blades extending from the outer peripheral wall, and strengthening ribs.
    Type: Application
    Filed: August 31, 2012
    Publication date: March 6, 2014
    Applicant: GE AVIATION SYSTEMS LLC
    Inventors: Sukeyuki Kobayashi, Frank Leslie Sincox, III
  • Publication number: 20140044524
    Abstract: An impeller fan assembly that includes a housing, a stator, a rotor having a hub and an annular array of non-stationary blades extending from the hub, at least two spaced apart bearings mounted to the stator, and a pump in fluid communication with the bearings to provide fluid to the bearings.
    Type: Application
    Filed: August 10, 2012
    Publication date: February 13, 2014
    Applicant: GE AVIATION SYSTEMS LLC
    Inventors: Sukeyuki Kobayashi, Frank Leslie Sincox, III, Richard George Hext, III
  • Patent number: 8562289
    Abstract: A method and system for a fan assembly that includes a fan casing having a longitudinal centerline axis extending from an upstream inlet opening to a downstream outlet opening is provided. The fan assembly also includes a first substantially cylindrical casing segment extending circumferentially about and substantially axially aligned with tips of a plurality of blades extending from a rotor hub, the first casing segment including a first inner diameter that is greater than the rotor diameter, a second casing segment configured to extend axially in a direction opposite a flow of fluid through the fan casing, the second casing segment including a second inner diameter, the second inner diameter less than the first inner diameter and the rotor diameter, and a third casing segment including the first inner diameter along a first circumferential edge, the second inner diameter along a second circumferential edge, and a surface extending therebetween.
    Type: Grant
    Filed: February 26, 2010
    Date of Patent: October 22, 2013
    Assignee: GE Aviation Systems, LLC
    Inventor: Sukeyuki Kobayashi
  • Publication number: 20110211942
    Abstract: A method and system for a fan assembly that includes a fan casing having a longitudinal centerline axis extending from an upstream inlet opening to a downstream outlet opening is provided. The fan assembly also includes a first substantially cylindrical casing segment extending circumferentially about and substantially axially aligned with tips of a plurality of blades extending from a rotor hub, the first casing segment including a first inner diameter that is greater than the rotor diameter, a second casing segment configured to extend axially in a direction opposite a flow of fluid through the fan casing, the second casing segment including a second inner diameter, the second inner diameter less than the first inner diameter and the rotor diameter, and a third casing segment including the first inner diameter along a first circumferential edge, the second inner diameter along a second circumferential edge, and a surface extending therebetween.
    Type: Application
    Filed: February 26, 2010
    Publication date: September 1, 2011
    Inventor: Sukeyuki Kobayashi
  • Publication number: 20050135947
    Abstract: An engine cooling fan motor has a water baffle positioned in a water line of sight passage through structures surrounding the motor to prevent water from impacting on the air vents at the front end of the motor. The baffle blocks the water line of sight passage. In one aspect, a rear cover is spaced from the rear endwall of the motor and has one or more baffled inlets to create an airflow passage to air inlet vents on the rear endwall of the motor.
    Type: Application
    Filed: December 22, 2003
    Publication date: June 23, 2005
    Applicant: Valeo Electrical Systems, Inc.
    Inventors: John Savage, Sukeyuki Kobayashi