Patents by Inventor VanDung To
VanDung To 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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Publication number: 20230279942Abstract: A shroud is provided and includes first and second curved sections, at least one of which defines a main interior channel and at least one of first and second lube jet sections integrated with the first and second curved sections. The first lube jet section includes a summit at which proximal portions of the first and second curved sections meet and defines a first jetting interior channel fluidly communicative with the main interior channel and terminating at the summit The second lube jet section includes an elongate member extending from one of the first and second curved sections and defines a second jetting interior channel fluidly communicative with the main interior channel and terminating at a distal end of the elongate member.Type: ApplicationFiled: March 7, 2022Publication date: September 7, 2023Inventors: Matthew Allen Slayter, James Vandung Nguyen
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Patent number: 11536199Abstract: A method of manufacturing a motoring system for a gas turbine having the steps of: assembling a pinned mechanical fuse, the pinned mechanical fuse including at least one shear pin; forming an outer housing; installing a reduction gear train into the outer housing, the reduction gear train having an input and an output; operably connecting a motor to the input; operably connecting a clutch to the output using the pinned mechanical fuse, the clutch in operation engages and disengages the reduction gear train; operably connecting a starter to the clutch, the starter having an output shaft; and operably connecting an accessory gearbox to the output shaft of the starter. The clutch is operably connected to the accessory gearbox through the starter and the output shaft. The at least one shear pin in operation shears when torque on the pinned mechanical fuse is greater than or equal to a selected value.Type: GrantFiled: June 28, 2019Date of Patent: December 27, 2022Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Matthew Allen Slayter, Richard Alan Davis, Paul F. Fox, Jeffrey Todd Roberts, Jeff A. Brown, James Vandung Nguyen, Benjamin T. Harder, Dwayne Leon Wilson, Brian McMasters, Daniel Richard Walker
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Patent number: 11313418Abstract: A method of manufacturing a motoring system for a gas turbine engine including the steps of: forming a mechanical shaft fuse, the mechanical shaft fuse including a plurality of through holes; forming an outer housing; installing a reduction gear train into the outer housing, the reduction gear train having an input and an output; operably connecting an electric motor to the input; operably connecting a clutch to the output using the mechanical shaft fuse, the clutch in operation engages and disengages the reduction gear train; operably connecting a starter to the clutch, the starter having an output shaft; and operably connecting an accessory gearbox to the output shaft of the starter. The mechanical shaft fuse in operation shears when torque on the mechanical is greater than or equal to a selected value.Type: GrantFiled: November 1, 2019Date of Patent: April 26, 2022Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Matthew Allen Slayter, Richard Alan Davis, Benjamin T. Harder, James Vandung Nguyen, Paul F. Fox, Jeffrey Todd Roberts, Jeff A. Brown, Brian McMasters, Dwayne Leon Wilson, Daniel Richard Walker
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Patent number: 10975772Abstract: A starter for a gas turbine engine includes a rotor shaft rotatable about an axis and includes an inner bore extending from an axial end of the rotor shaft with respect to the axis. A sun gear is on the rotor shaft. A lock nut is received against an axial end face of the sun gear and threadedly engaged with an outer diameter of the rotor shaft. A retainer is positioned to bias the nut against the axial end face and includes a projection portion threadedly engaged with the rotor shaft in the inner bore. A bolt through the projection portion is threadedly engaged with the rotor shaft.Type: GrantFiled: February 7, 2019Date of Patent: April 13, 2021Assignee: Hamilton Sundstrand CorporationInventors: Yiwei Jiang, James Vandung Nguyen, Edward W. Goy
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Publication number: 20200256256Abstract: A starter for a gas turbine engine includes a rotor shaft rotatable about an axis and includes an inner bore extending from an axial end of the rotor shaft with respect to the axis. A sun gear is on the rotor shaft. A lock nut is received against an axial end face of the sun gear and threadedly engaged with an outer diameter of the rotor shaft. A retainer is positioned to bias the nut against the axial end face and includes a projection portion threadedly engaged with the rotor shaft in the inner bore. A bolt through the projection portion is threadedly engaged with the rotor shaft.Type: ApplicationFiled: February 7, 2019Publication date: August 13, 2020Inventors: Yiwei Jiang, James Vandung Nguyen, Edward W. Goy
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Publication number: 20200141452Abstract: A method of manufacturing a motoring system for a gas turbine engine including the steps of: forming a mechanical shaft fuse, the mechanical shaft fuse including a plurality of through holes; forming an outer housing; installing a reduction gear train into the outer housing, the reduction gear train having an input and an output; operably connecting an electric motor to the input; operably connecting a clutch to the output using the mechanical shaft fuse, the clutch in operation engages and disengages the reduction gear train; operably connecting a starter to the clutch, the starter having an output shaft; and operably connecting an accessory gearbox to the output shaft of the starter. The mechanical shaft fuse in operation shears when torque on the mechanical is greater than or equal to a selected value.Type: ApplicationFiled: November 1, 2019Publication date: May 7, 2020Inventors: Matthew Allen Slayter, Richard Alan Davis, Benjamin T. Harder, James Vandung Nguyen, Paul F. Fox, Jeffrey Todd Roberts, Jeff A. Brown, Brian McMasters, Dwayne Leon Wilson, Daniel Richard Walker
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Patent number: 10495003Abstract: According to an aspect, a system for a gas turbine engine includes a reduction gear train operable to drive rotation of a starter gear train that interfaces to an accessory gearbox of the gas turbine engine. The reduction gear train includes a starter interface gear that engages the starter gear train and a core-turning clutch operably connected to the starter interface gear. The reduction gear train also includes a planetary gear system operably connected to the core-turning clutch and a jacking gear system operably connected to the planetary gear system and a core-turning input.Type: GrantFiled: July 5, 2016Date of Patent: December 3, 2019Assignee: HAMILTON SUNSTRAND CORPORATIONInventors: Matthew Allen Slayter, James Vandung Nguyen, Paul F. Fox, Richard Alan Davis, Jeff A. Brown, Jeffrey Todd Roberts, Daniel Richard Walker, Richard R. Hergert, Dwayne Leon Wilson, Brian McMasters, Benjamin T. Harder
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Patent number: 10473164Abstract: A motoring system for a gas turbine engine having: a reduction gear train having an input and an output; an electric motor operably connected to the input; a clutch operably connected to the output, the clutch in operation engages and disengages the reduction gear train; and a mechanical shaft fuse operably connecting the output to the clutch, the mechanical shaft fuse in operation shears when torque on the mechanical shaft fuse is greater than or equal to a selected value. The mechanical shaft fuse includes a plurality of through holes.Type: GrantFiled: July 5, 2016Date of Patent: November 12, 2019Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Matthew Allen Slayter, Richard Alan Davis, Benjamin T. Harder, James Vandung Nguyen, Paul F. Fox, Jeffrey Todd Roberts, Jeff A. Brown, Brian McMasters, Dwayne Leon Wilson, Daniel Richard Walker
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Patent number: 10473034Abstract: According to an aspect, a system for a gas turbine engine includes a reduction gear train operable to drive rotation of a starter gear train that interfaces to an accessory gearbox of the gas turbine engine. The reduction gear train includes a starter interface gear that engages the starter gear train and a core-turning clutch operably connected to the starter interface gear. The reduction gear train also includes a geared rotary actuator including a primary planetary gear system, where the geared rotary actuator is operably connected to the core-turning clutch. The reduction gear train further includes a secondary planetary gear system operably connected to the primary planetary gear system and a core-turning input. The system also includes a mounting pad with an interface to couple a core-turning motor to the core-turning input of the reduction gear train.Type: GrantFiled: July 5, 2016Date of Patent: November 12, 2019Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Benjamin T. Harder, Brian McMasters, James Vandung Nguyen, Dwayne Leon Wilson, Paul F. Fox, Richard Alan Davis, Richard R. Hergert, Jeffrey Todd Roberts, Jeff A. Brown, Daniel Richard Walker, Matthew Allen Slayter, William G. Sheridan
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Publication number: 20190323434Abstract: A method of manufacturing a motoring system for a gas turbine having the steps of: assembling a pinned mechanical fuse, the pinned mechanical fuse including at least one shear pin; forming an outer housing; installing a reduction gear train into the outer housing, the reduction gear train having an input and an output; operably connecting a motor to the input; operably connecting a clutch to the output using the pinned mechanical fuse, the clutch in operation engages and disengages the reduction gear train; operably connecting a starter to the clutch, the starter having an output shaft; and operably connecting an accessory gearbox to the output shaft of the starter. The clutch is operably connected to the accessory gearbox through the starter and the output shaft. The at least one shear pin in operation shears when torque on the pinned mechanical fuse is greater than or equal to a selected value.Type: ApplicationFiled: June 28, 2019Publication date: October 24, 2019Inventors: Matthew Allen Slayter, Richard Alan Davis, Paul F. Fox, Jeffrey Todd Roberts, Jeff A. Brown, James Vandung Nguyen, Benjamin T. Harder, Dwayne Leon Wilson, Brian McMasters, Daniel Richard Walker
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Patent number: 10422284Abstract: A motoring system for a gas turbine engine having: a reduction gear train having an input and output; a motor operably connected to the input; a clutch operably connected to the output, the clutch in operation engages and disengages the reduction gear train; and a pinned mechanical fuse operably connecting the output to the clutch, the pinned mechanical fuse having at least one shear pin. The pinned mechanical fuse having: an outer sleeve having a first section, second section, inner chamber, outer wall, and at least one through hole connecting the inner chamber to the outer wall within the first section; and an inner sleeve having a first portion, second portion, outer surface, and at least one blind hole located in the outer surface within the second portion. The second portion being located within the inner chamber and operably connected to the outer sleeve through at least one shear pin.Type: GrantFiled: July 5, 2016Date of Patent: September 24, 2019Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Matthew Allen Slayter, Richard Alan Davis, Paul F. Fox, Jeffrey Todd Roberts, Jeff A. Brown, James Vandung Nguyen, Benjamin T. Harder, Dwayne Leon Wilson, Brian McMasters, Daniel Richard Walker
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Patent number: 10330016Abstract: According to an aspect, a system for a gas turbine engine includes a reduction gear train operable to drive rotation of a starter gear train that interfaces to an accessory gearbox of the gas turbine engine. The reduction gear train includes a starter interface gear that engages the starter gear train, a core-turning clutch operably connected to the starter interface gear, and a plurality of stacked planetary gear systems operably connected to the core-turning clutch and a core-turning input. The system also includes a mounting pad including an interface to couple a core-turning motor to the core-turning input of the reduction gear train.Type: GrantFiled: July 5, 2016Date of Patent: June 25, 2019Assignee: HAMILTON SUNDSTRAND CORPORATIONInventors: Benjamin T. Harder, Matthew Allen Slayter, Brian McMasters, James Vandung Nguyen, Dwayne Leon Wilson, Paul F. Fox, Richard Alan Davis, Richard R. Hergert, Jeffrey Todd Roberts, Jeff A. Brown, Daniel Richard Walker
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Publication number: 20180010521Abstract: A motoring system for a gas turbine engine having: a reduction gear train having an input and output; a motor operably connected to the input; a clutch operably connected to the output, the clutch in operation engages and disengages the reduction gear train; and a pinned mechanical fuse operably connecting the output to the clutch, the pinned mechanical fuse having at least one shear pin. The pinned mechanical fuse having: an outer sleeve having a first section, second section, inner chamber, outer wall, and at least one through hole connecting the inner chamber to the outer wall within the first section; and an inner sleeve having a first portion, second portion, outer surface, and at least one blind hole located in the outer surface within the second portion. The second portion being located within the inner chamber and operably connected to the outer sleeve through at least one shear pin.Type: ApplicationFiled: July 5, 2016Publication date: January 11, 2018Inventors: Matthew Allen Slayter, Richard Alan Davis, Paul F. Fox, Jeffrey Todd Roberts, Jeff A. Brown, James Vandung Nguyen, Benjamin T. Harder, Dwayne Leon Wilson, Brian McMasters, Daniel Richard Walker
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Publication number: 20180010523Abstract: According to an aspect, a system for a gas turbine engine includes a reduction gear train operable to drive rotation of a starter gear train that interfaces to an accessory gearbox of the gas turbine engine. The reduction gear train includes a starter interface gear that engages the starter gear train and a core-turning clutch operably connected to the starter interface gear. The reduction gear train also includes a geared rotary actuator including a primary planetary gear system, where the geared rotary actuator is operably connected to the core-turning clutch. The reduction gear train further includes a secondary planetary gear system operably connected to the primary planetary gear system and a core-turning input. The system also includes a mounting pad with an interface to couple a core-turning motor to the core-turning input of the reduction gear train.Type: ApplicationFiled: July 5, 2016Publication date: January 11, 2018Inventors: Benjamin T. Harder, Brian McMasters, James Vandung Nguyen, Dwayne Leon Wilson, Paul F. Fox, Richard Alan Davis, Richard R. Hergert, Jeffrey Todd Roberts, Jeff A. Brown, Daniel Richard Walker, Matthew Allen Slayter, William G. Sheridan
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Publication number: 20180010648Abstract: A motoring system for a gas turbine engine having: a reduction gear train having an input and an output; an electric motor operably connected to the input; a clutch operably connected to the output, the clutch in operation engages and disengages the reduction gear train; and a mechanical shaft fuse operably connecting the output to the clutch, the mechanical shaft fuse in operation shears when torque on the mechanical shaft fuse is greater than or equal to a selected value. The mechanical shaft fuse includes a plurality of through holes.Type: ApplicationFiled: July 5, 2016Publication date: January 11, 2018Inventors: Matthew Allen Slayter, Richard Alan Davis, Benjamin T. Harder, James Vandung Nguyen, Paul F. Fox, Jeffrey Todd Roberts, Jeff A. Brown, Brian McMasters, Dwayne Leon Wilson, Daniel Richard Walker
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Publication number: 20180010522Abstract: According to an aspect, a system for a gas turbine engine includes a reduction gear train operable to drive rotation of a starter gear train that interfaces to an accessory gearbox of the gas turbine engine. The reduction gear train includes a starter interface gear that engages the starter gear train, a core-turning clutch operably connected to the starter interface gear, and a plurality of stacked planetary gear systems operably connected to the core-turning clutch and a core-turning input. The system also includes a mounting pad including an interface to couple a core-turning motor to the core-turning input of the reduction gear train.Type: ApplicationFiled: July 5, 2016Publication date: January 11, 2018Inventors: Benjamin T. Harder, Matthew Allen Slayter, Brian McMasters, James Vandung Nguyen, Dwayne Leon Wilson, Paul F. Fox, Richard Alan Davis, Richard R. Hergert, Jeffrey Todd Roberts, Jeff A. Brown, Daniel Richard Walker
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Patent number: 9194295Abstract: A mechanical system has a component to be lubricated that requires greater lubrication at lower speed conditions than would be required at higher speed conditions. A lubricant tower is biased to a position allowing a greater flow of lubrication to the component at lower speed conditions, then moved to a position at higher speed conditions where there is a lesser flow of lubrication.Type: GrantFiled: November 26, 2012Date of Patent: November 24, 2015Assignee: Hamilton Sundstrand CorporationInventors: Matthew Slayter, James Vandung Nguyen, Jeffrey A. Stadler, Timothy A. Johnson
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Publication number: 20140144120Abstract: A mechanical system has a component to be lubricated that requires greater lubrication at lower speed conditions than would be required at higher speed conditions. A lubricant tower is biased to a position allowing a greater flow of lubrication to the component at lower speed conditions, then moved to a position at higher speed conditions where there is a lesser flow of lubrication.Type: ApplicationFiled: November 26, 2012Publication date: May 29, 2014Applicant: HAMILTON SUNDSTRAND CORPORATIONInventors: Matthew Slayter, James Vandung Nguyen, Jeffrey A. Stadler, Timothy A. Johnson
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Patent number: 7737970Abstract: An image is generated that includes ray traced pixel data and rasterized pixel data. A synergistic processing unit (SPU) uses a rendering algorithm to generate ray traced data for objects that require high-quality image rendering. The ray traced data is fragmented, whereby each fragment includes a ray traced pixel depth value and a ray traced pixel color value. A rasterizer compares ray traced pixel depth values to corresponding rasterized pixel depth values, and overwrites ray traced pixel data with rasterized pixel data when the corresponding rasterized fragment is “closer” to a viewing point, which results in composite data. A display subsystem uses the resultant composite data to generate an image on a user's display.Type: GrantFiled: July 1, 2008Date of Patent: June 15, 2010Assignee: International Business Machines CorporationInventors: Gordon Clyde Fossum, Barry L Minor, VanDung Dang To
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Patent number: 7694306Abstract: Computational load is balanced across a plurality of processors. Source code subtasks are compiled into byte code subtasks whereby the byte code subtasks are translated into processor-specific object code subtasks at runtime. The processor-type selection is based upon one of three approaches which are 1) a brute force approach, 2) higher-level approach, or 3) processor availability approach. Each object code subtask is loaded in a corresponding processor type for execution. In one embodiment, a compiler stores a pointer in a byte code file that references the location of a byte code subtask. In this embodiment, the byte code subtask is stored in a shared library and, at runtime, a runtime loader uses the pointer to identify the location of the byte code subtask in order to translate the byte code subtask.Type: GrantFiled: June 25, 2008Date of Patent: April 6, 2010Assignee: International Business Machines CorporationInventors: Barry L Minor, Mark Richard Nutter, VanDung Dang To