Patents by Inventor Bruce D. Hansen

Bruce D. Hansen 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: 11655880
    Abstract: A gear system for a rotary wing aircraft includes a first gear including an inner gear portion having a first pitch and an outer gear portion having a second pitch that is distinct from the first pitch. A second gear includes a third pitch driven at a driving rotational speed. An actuator member is coupled to the second gear while driven at the driving rotational speed. The actuator member shifts the second gear along the first gear to engage with one of the inner gear portion and the outer gear portion to drive the first gear at a first rotational speed and engage with other one of the inner gear portion and the outer gear portion to drive the first gear at a second rotational speed. A controller is operable to control the actuator member to shift the second gear between the inner gear portion and the outer gear portion.
    Type: Grant
    Filed: July 8, 2020
    Date of Patent: May 23, 2023
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventor: Bruce D. Hansen
  • Patent number: 11391356
    Abstract: A hybrid gear includes a first portion having a plurality of first engagement features formed from a first material and having a first stiffness and a second portion having a plurality of second engagement features in intermeshing arrangement with the plurality of first engagement features. The plurality of second engagement features is formed from a second material distinct from the first material and having a second stiffness. The first stiffness of the plurality of first engagement features is within 20% of the second stiffness of the plurality of second engagement features.
    Type: Grant
    Filed: July 17, 2019
    Date of Patent: July 19, 2022
    Assignee: Sikorsky Aircraft Corporation
    Inventors: Wei Hu, Shane Lewis, Bruce D. Hansen, Bryan Kenneth Baskin
  • Publication number: 20220010862
    Abstract: A gear system for a rotary wing aircraft includes a first gear including an inner gear portion having a first pitch and an outer gear portion having a second pitch that is distinct from the first pitch. A second gear includes a third pitch driven at a driving rotational speed. An actuator member is coupled to the second gear while driven at the driving rotational speed. The actuator member shifts the second gear along the first gear to engage with one of the inner gear portion and the outer gear portion to drive the first gear at a first rotational speed and engage with other one of the inner gear portion and the outer gear portion to drive the first gear at a second rotational speed. A controller is operable to control the actuator member to shift the second gear between the inner gear portion and the outer gear portion.
    Type: Application
    Filed: July 8, 2020
    Publication date: January 13, 2022
    Inventor: Bruce D. Hansen
  • Patent number: 11041221
    Abstract: A method of manufacturing a part is provided. The method includes heating a gear in the presence of carbon to carburize a material of the gear to create a carburized gear, the gear having a plurality of gear teeth and which comprises a selected material. Next, the carburized gear is high pressure gas quenched to drive the carbon into the material of the gear to create a quenched gear. Next, the quenched gear is at least one of cavitation peened and laser peened to create a peened gear. Finally, superfinishing is performed on surfaces of the peened gear.
    Type: Grant
    Filed: October 14, 2019
    Date of Patent: June 22, 2021
    Assignee: Sikorsky Aircraft Corporation
    Inventor: Bruce D. Hansen
  • Patent number: 10821532
    Abstract: A herringbone gear includes a cylindrical body having a circumferential face having a width. A first helical gear tooth on the circumferential face has a first configuration, a second helical gear tooth on the circumferential face has a second configuration, and a transition on the circumferential face extends between the first helical gear tooth and the second helical gear tooth. An involute form taken within a transverse plane of the circumferential face remains constant over the width.
    Type: Grant
    Filed: January 30, 2017
    Date of Patent: November 3, 2020
    Assignee: Sikorsky Aircraft Corporation
    Inventors: Edward H. Bittner, Bruce D. Hansen, Christopher John Mussel
  • Patent number: 10746226
    Abstract: A method of making bearings includes treating a metallic surface of a bearing raceway with a pulsed electrochemical processing nozzle to transform the amorphous oxide into a crystalline structure on the metallic surface electro-chemically and convert the metallic surface into a ceramic like hardness surface. Treating the metallic surface can include forming a gradient in material composition transitioning from a purely metallic material at a cross-sectional position within the bearing raceway to a purely crystalline structure material at the ceramic like hardness surface of the bearing raceway.
    Type: Grant
    Filed: October 10, 2019
    Date of Patent: August 18, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Bruce D. Hansen, William P. Fallon, Jr.
  • Patent number: 10717154
    Abstract: A gearbox is provided having a housing, a gear having a plurality of teeth operationally configured within the housing, and a laser peening device located within the housing and configured to perform active laser peening on a predetermined surface of the gear while the gear is rotated within the housing. A method of maintaining compressive residual stresses in a gear is provided, the method including operating a gearbox to rotate a gear within the gearbox and laser peening a predetermined surface of the gear with a laser peening device located within the gearbox.
    Type: Grant
    Filed: August 29, 2016
    Date of Patent: July 21, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventor: Bruce D. Hansen
  • Patent number: 10646938
    Abstract: A method of manufacturing a gear, the method includes applying a first charge to a workpiece and applying a second, opposite charge to an electrochemical machining (ECM) attachment, the ECM attachment having a pattern. The method further includes simultaneously forming a plurality of surfaces of a gear tooth in the workpiece using the pattern of the ECM attachment while applying the first charge to the workpiece and applying the second charge to the ECM attachment and turning the workpiece and the ECM attachment in opposite rotational directions. The plurality of surfaces includes at least one end face and a top land of the gear tooth.
    Type: Grant
    Filed: January 11, 2018
    Date of Patent: May 12, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Edward H. Bittner, William Patrick Murphy, Bruce D. Hansen, Christopher J. Mussel, Yuriy Gmirya
  • Publication number: 20200063798
    Abstract: A method of making bearings includes treating a metallic surface of a bearing raceway with a pulsed electrochemical processing nozzle to transform the amorphous oxide into a crystalline structure on the metallic surface electro-chemically and convert the metallic surface into a ceramic like hardness surface. Treating the metallic surface can include forming a gradient in material composition transitioning from a purely metallic material at a cross-sectional position within the bearing raceway to a purely crystalline structure material at the ceramic like hardness surface of the bearing raceway.
    Type: Application
    Filed: October 10, 2019
    Publication date: February 27, 2020
    Inventors: Bruce D. Hansen, William P. Fallon, JR.
  • Publication number: 20200040414
    Abstract: A method of manufacturing a part is provided. The method includes heating a gear in the presence of carbon to carburize a material of the gear to create a carburized gear, the gear having a plurality of gear teeth and which comprises a selected material. Next, the carburized gear is high pressure gas quenched to drive the carbon into the material of the gear to create a quenched gear. Next, the quenched gear is at least one of cavitation peened and laser peened to create a peened gear. Finally, superfinishing is performed on surfaces of the peened gear.
    Type: Application
    Filed: October 14, 2019
    Publication date: February 6, 2020
    Inventor: Bruce D. Hansen
  • Publication number: 20200025279
    Abstract: A hybrid gear includes a first portion having a plurality of first engagement features formed from a first material and having a first stiffness and a second portion having a plurality of second engagement features in intermeshing arrangement with the plurality of first engagement features. The plurality of second engagement features is formed from a second material distinct from the first material and having a second stiffness. The first stiffness of the plurality of first engagement features is within 20% of the second stiffness of the plurality of second engagement features.
    Type: Application
    Filed: July 17, 2019
    Publication date: January 23, 2020
    Inventors: Wei Hu, Shane Lewis, Bruce D. Hansen, Bryan Kenneth Baskin
  • Patent number: 10494708
    Abstract: A method of carburizing a steel component having a composition of Fe-16.3Co-7.5Ni-3.5Cr-1.75Mo-0.2W-0.11C-0.03Ti-0.02V includes generating a low pressure vacuum in a carburization furnace having the steel component therein, heating the steel component to an optimal carburization temperature while in the low pressure vacuum, performing a boost cycle to introduce carbon rich gas into the carburization furnace while the steel component is at the optimal carburization temperature and in the low pressure vacuum, and performing a diffuse cycle by ceasing introduction of the carbon rich gas into the carburization furnace to allow for diffusion of the carbon into the steel component to occur and while the steel component is at the optimal carburization temperature and in the low pressure vacuum. The boost cycle and the diffuse cycle are repeated to achieve a carbon content at a surface of the steel component of between 0.40 wt. % and 0.55 wt. %.
    Type: Grant
    Filed: March 29, 2016
    Date of Patent: December 3, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Jonathan Buckley, Bruce D. Hansen
  • Patent number: 10494687
    Abstract: A method of manufacturing a part is provided. The method includes heating a gear in the presence of carbon to carburize a material of the gear to create a carburized gear, the gear having a plurality of gear teeth and which comprises a selected material. Next, the carburized gear is high pressure gas quenched to drive the carbon into the material of the gear to create a quenched gear. Next, the quenched gear is at least one of cavitation peened and laser peened to create a peened gear. Finally, superfinishing is performed on surfaces of the peened gear.
    Type: Grant
    Filed: January 26, 2016
    Date of Patent: December 3, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventor: Bruce D. Hansen
  • Patent number: 10480581
    Abstract: A method of making bearings includes treating a metallic surface of a bearing raceway with a pulsed electrochemical processing nozzle to transform the amorphous oxide into a crystalline structure on the metallic surface electro-chemically and convert the metallic surface into a ceramic like hardness surface. Treating the metallic surface can include forming a gradient in material composition transitioning from a purely metallic material at a cross-sectional position within the bearing raceway to a purely crystalline structure material at the ceramic like hardness surface of the bearing raceway.
    Type: Grant
    Filed: April 13, 2018
    Date of Patent: November 19, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Bruce D. Hansen, William P. Fallon, Jr.
  • Publication number: 20190210130
    Abstract: A method of manufacturing a gear, the method includes applying a first charge to a workpiece and applying a second, opposite charge to an electrochemical machining (ECM) attachment, the ECM attachment having a pattern. The method further includes simultaneously forming a plurality of surfaces of a gear tooth in the workpiece using the pattern of the ECM attachment while applying the first charge to the workpiece and applying the second charge to the ECM attachment and turning the workpiece and the ECM attachment in opposite rotational directions. The plurality of surfaces includes at least one end face and a top land of the gear tooth.
    Type: Application
    Filed: January 11, 2018
    Publication date: July 11, 2019
    Inventors: EDWARD H. BITTNER, WILLIAM PATRICK MURPHY, BRUCE D. HANSEN, CHRISTOPHER J. MUSSEL, YURIY GMIRYA
  • Patent number: 10295039
    Abstract: A method of manufacturing a gear is provided. The method includes forming a plurality of gear teeth in a surface of a gear, the gear teeth having tooth faces defining tooth edges including tooth edge flanks and tooth edge top land and generating a convex contour at an edge break of at least one of the tooth edge flanks and tooth edge top land.
    Type: Grant
    Filed: January 23, 2017
    Date of Patent: May 21, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Edward H. Bittner, Bruce D. Hansen, Christopher John Mussel
  • Publication number: 20190022778
    Abstract: A herringbone gear includes a cylindrical body having a circumferential face having a width. A first helical gear tooth on the circumferential face has a first configuration, a second helical gear tooth on the circumferential face has a second configuration, and a transition on the circumferential face extends between the first helical gear tooth and the second helical gear tooth. An involute form taken within a transverse plane of the circumferential face remains constant over the width.
    Type: Application
    Filed: January 30, 2017
    Publication date: January 24, 2019
    Inventors: Edward H. BITTNER, Bruce D. HANSEN, Christopher John MUSSEL
  • Publication number: 20180347630
    Abstract: A method of making bearings includes treating a metallic surface of a bearing raceway with a pulsed electrochemical processing nozzle to transform the amorphous oxide into a crystalline structure on the metallic surface electro-chemically and convert the metallic surface into a ceramic like hardness surface. Treating the metallic surface can include forming a gradient in material composition transitioning from a purely metallic material at a cross-sectional position within the bearing raceway to a purely crystalline structure material at the ceramic like hardness surface of the bearing raceway.
    Type: Application
    Filed: April 13, 2018
    Publication date: December 6, 2018
    Inventors: Bruce D. Hansen, William P. Fallon, JR.
  • Publication number: 20180236599
    Abstract: A gearbox is provided having a housing, a gear having a plurality of teeth operationally configured within the housing, and a laser peening device located within the housing and configured to perform active laser peening on a predetermined surface of the gear while the gear is rotated within the housing. A method of maintaining compressive residual stresses in a gear is provided, the method including operating a gearbox to rotate a gear within the gearbox and laser peening a predetermined surface of the gear with a laser peening device located within the gearbox.
    Type: Application
    Filed: August 29, 2016
    Publication date: August 23, 2018
    Inventor: Bruce D. Hansen
  • Publication number: 20180119266
    Abstract: A method of carburizing a steel component having a composition of Fe-16.3Co-7.5Ni-3.5Cr-1.75Mo-0.2W-0.11C-0.03Ti-0.02V includes generating a low pressure vacuum in a carburization furnace having the steel component therein, heating the steel component to an optimal carburization temperature while in the low pressure vacuum, performing a boost cycle to introduce carbon rich gas into the carburization furnace while the steel component is at the optimal carburization temperature and in the low pressure vacuum, and performing a diffuse cycle by ceasing introduction of the carbon rich gas into the carburization furnace to allow for diffusion of the carbon into the steel component to occur and while the steel component is at the optimal carburization temperature and in the low pressure vacuum. The boost cycle and the diffuse cycle are repeated to achieve a carbon content at a surface of the steel component of between 0.40 wt. % and 0.55 wt. %.
    Type: Application
    Filed: March 29, 2016
    Publication date: May 3, 2018
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Jonathan Buckley, Bruce D. Hansen