Patents by Inventor Harsha Sanjeewa Bulathsinghalage

Harsha Sanjeewa Bulathsinghalage 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).

  • Publication number: 20240116708
    Abstract: Various embodiments are directed to a carriage lift assembly comprising: at least one frame element configured to secure the carriage lift assembly relative to a first mast and a second mast; and at least one spreader arm extending laterally and defining at least a portion of a lift width; wherein the spreader arm width of the spreader arm comprises a selectively adjustable configuration, wherein the lift width is configured to be selectively adjustable based at least in part on the adjustable configuration of the spreader arm width. In various embodiments, the at least one spreader arm comprises an at least partially resilient configuration such that, in response to a force acting on the spreader arm in one or more directions, the spreader arm may exhibit a movement in the one or more directions so as to absorb at least a portion of the force.
    Type: Application
    Filed: September 22, 2023
    Publication date: April 11, 2024
    Inventors: Anthony James Turco, Harsha Sanjeewa Bulathsinghalage, Justen Pahls
  • Patent number: 11795000
    Abstract: Various embodiments are directed to a carriage lift assembly comprising: at least one frame element configured to secure the carriage lift assembly relative to a first mast and a second mast; and at least one spreader arm extending laterally and defining at least a portion of a lift width; wherein the spreader arm width of the spreader arm comprises a selectively adjustable configuration, wherein the lift width is configured to be selectively adjustable based at least in part on the adjustable configuration of the spreader arm width. In various embodiments, the at least one spreader arm comprises an at least partially resilient configuration such that, in response to a force acting on the spreader arm in one or more directions, the spreader arm may exhibit a movement in the one or more directions so as to absorb at least a portion of the force.
    Type: Grant
    Filed: July 9, 2021
    Date of Patent: October 24, 2023
    Assignee: INTELLIGRATED HEADQUARTERS, LLC
    Inventors: Anthony James Turco, Harsha Sanjeewa Bulathsinghalage, Justen Pahls
  • Publication number: 20230011706
    Abstract: Various embodiments are directed to a carriage lift assembly comprising: at least one frame element configured to secure the carriage lift assembly relative to a first mast and a second mast; and at least one spreader arm extending laterally and defining at least a portion of a lift width; wherein the spreader arm width of the spreader arm comprises a selectively adjustable configuration, wherein the lift width is configured to be selectively adjustable based at least in part on the adjustable configuration of the spreader arm width. In various embodiments, the at least one spreader arm comprises an at least partially resilient configuration such that, in response to a force acting on the spreader arm in one or more directions, the spreader arm may exhibit a movement in the one or more directions so as to absorb at least a portion of the force.
    Type: Application
    Filed: July 9, 2021
    Publication date: January 12, 2023
    Inventors: Anthony James Turco, Harsha Sanjeewa Bulathsinghalage, Justen Pahls
  • Patent number: 11512646
    Abstract: An air starter for starting a turbine engine that includes a housing, a turbine, an output shaft, and at least one bearing. The housing can define an interior where the turbine couples to the output shaft. A primary air flow path extends through the housing where air from the turbine can be exhausted through a primary outlet or a cooling outlet.
    Type: Grant
    Filed: December 23, 2019
    Date of Patent: November 29, 2022
    Assignee: Unison Industries, LLC
    Inventors: Shiloh Montegomery Meyers, Subrata Nayak, Pradeep Hemant Sangli, David Allan Dranschak, Santosh Kumar Prasad, Marc David Zinger, Sharad Pundlik Patil, Harsha Sanjeewa Bulathsinghalage, Sumathi P
  • Patent number: 11053857
    Abstract: A method and decoupler for disengaging an output shaft from an engine in a back drive event with a backdrive decoupler. The backdrive decoupler includes a an output shaft, drive shaft, and a retention mechanism selectively coupling the output shaft to the drive shaft. In a backdrive event, the decoupler decouples the output shaft from the drive shaft.
    Type: Grant
    Filed: February 12, 2020
    Date of Patent: July 6, 2021
    Assignee: GE AVIATION SYSTEMS LLC
    Inventors: Eliel Fresco Rodriguez, David Allan Dranschak, Shiloh Montegomery Emerson Meyers, Harsha Sanjeewa Bulathsinghalage
  • Publication number: 20210189967
    Abstract: An air starter for starting a turbine engine that includes a housing, a turbine, an output shaft, and at least one bearing. The housing can define an interior where the turbine couples to the output shaft. A primary air flow path extends through the housing where air from the turbine can be exhausted through a primary outlet or a cooling outlet.
    Type: Application
    Filed: December 23, 2019
    Publication date: June 24, 2021
    Inventors: Shiloh Montegomery Meyers, Subrata Nayak, Pradeep Hemant Sangli, David Allan Dranschak, Santosh Kumar Prasad, Marc David Zinger, Sharad Pundlik Patil, Harsha Sanjeewa Bulathsinghalage, Sumathi P
  • Publication number: 20200182156
    Abstract: A method and decoupler for disengaging an output shaft from an engine in a back drive event with a backdrive decoupler. The backdrive decoupler includes a an output shaft, drive shaft, and a retention mechanism selectively coupling the output shaft to the drive shaft. In a backdrive event, the decoupler decouples the output shaft from the drive shaft.
    Type: Application
    Filed: February 12, 2020
    Publication date: June 11, 2020
    Inventors: Eliel Fresco Rodriguez, David Allan Dranschak, Shiloh Montegomery Emerson Meyers, Harsha Sanjeewa Bulathsinghalage
  • Patent number: 10584640
    Abstract: A method and decoupler for disengaging an output shaft from an engine in a back drive event with a backdrive decoupler. The backdrive decoupler includes a an output shaft, drive shaft, and a retention mechanism selectively coupling the output shaft to the drive shaft. In a backdrive event, the decoupler decouples the output shaft from the drive shaft.
    Type: Grant
    Filed: June 13, 2016
    Date of Patent: March 10, 2020
    Assignee: GE Aviation Systems LLC
    Inventors: Eliel Fresco Rodriguez, David Allan Dranschak, Shiloh Montegomery Emerson Meyers, Harsha Sanjeewa Bulathsinghalage
  • Patent number: 10495182
    Abstract: An apparatus for an air turbine starter for an engine. The air turbine starter includes a housing defining an inlet, an outlet, and a flow path extending between the inlet and the outlet for communicating a flow of gas there through. A turbine member is journaled within the housing and disposed within the flow path for rotatably extracting mechanical power from the flow of gas and having a turbine output shaft. The air turbine starter further includes a planetary gear system drivingly coupled with the turbine output shaft and including a sun gear, a ring gear mounted to the housing, and a set of planetary gears operably coupling the sun gear and the ring gear with the sun gear is coupled to the turbine output shaft.
    Type: Grant
    Filed: May 9, 2017
    Date of Patent: December 3, 2019
    Assignee: Unison Industries, LLC
    Inventors: Subrata Nayak, Ravindra Shankar Ganiger, David Allan Dranschak, Marc David Zinger, Shiloh Montgomery Emerson Meyers, Pallavi Tripathi, Sharad Pundlik Patil, Mark Leslie Rickert, Harsha Sanjeewa Bulathsinghalage, Matthew Keith Murdock
  • Publication number: 20180347669
    Abstract: An apparatus for an air turbine starter for an engine. The air turbine starter includes a housing defining an inlet, an outlet, and a flow path extending between the inlet and the outlet for communicating a flow of gas there through. A turbine member is journaled within the housing and disposed within the flow path for rotatably extracting mechanical power from the flow of gas and having a turbine output shaft. The air turbine starter further includes a planetary gear system drivingly coupled with the turbine output shaft and including a sun gear, a ring gear mounted to the housing, and a set of planetary gears operably coupling the sun gear and the ring gear with the sun gear is coupled to the turbine output shaft.
    Type: Application
    Filed: May 9, 2017
    Publication date: December 6, 2018
    Inventors: Subrata Nayak, Ravindra Shankar Ganiger, David Allan Dranschak, Marc David Zinger, Shiloh Montgomery Emerson Meyers, Pallavi Tripathi, Sharad Pundlik Patil, Mark Leslie Rickert, Harsha Sanjeewa Bulathsinghalage, Matthew Keith Murdock