Patents by Inventor Sunil James

Sunil James 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: 10412131
    Abstract: Described herein are various embodiments of systems, methods, and apparatus that allow a user to share data, such as one or more files from within an application with one or more other (not necessarily co-located) computing devices using a gesture-based sharing function. In a particular example, systems, methods, and apparatus described herein may be used to share graphical representations of chemical structures within a chemical structure rendering application between two or more user devices. By offering a user a quick and visually intuitive option for sharing a file with other user(s) without exiting a current application, the systems, methods, and apparatus described herein provide efficient and engaging tools for sharing work product in real time between two or more users.
    Type: Grant
    Filed: February 6, 2014
    Date of Patent: September 10, 2019
    Assignee: PerkinElmer Informatics, Inc.
    Inventors: Robin Smith, Sunil Anant Gupta, Michael Stapleton, Benjamin James Davis, Amy Annette Hahn, Jordan Haneil Shatsoff, Joshua Benjamin Wakefield, Biying Huang, Shadrack Cgar Frazier, Sr., Brandon William Arther Graham, Beau Guy Tremblay, Sonal Shashikant Kulkarni, Daniel Oberlin, Julie E. Nelson
  • Publication number: 20190147878
    Abstract: Some implementations are directed to selective invocation of a particular third-party (3P) agent by an automated assistant to achieve an intended action determined by the automated assistant during a dynamic dialog between the automated assistant and a user. In some of those implementations, the particular 3P agent is invoked with value(s) for parameter(s) that are determined during the dynamic dialog; and/or the particular 3P agent is selected, from a plurality of candidate 3P agents, for invocation based on the determined value(s) for the parameter(s) and/or based on other criteria. In some of those implementations, the automated assistant invokes the particular 3P agent by transmitting, to the particular 3P agent, a 3P invocation request that includes the determined value(s) for the parameter(s).
    Type: Application
    Filed: January 10, 2019
    Publication date: May 16, 2019
    Inventors: Ulas Kirazci, Bo Wang, Steve Chen, Sunil Vemuri, Barnaby James, Valerie Nygaard
  • Publication number: 20190063754
    Abstract: A combustion system and a method of combustion for a gas turbine engine includes a combustor liner defining a combustion chamber. A plurality of fuel nozzle sets extend into, and supply fuel flow to, the combustion chamber. A pilot fuel nozzle injects a first fuel spray in a tangential direction relative to the combustion liner and toward the upstream end of the combustion chamber. A main fuel nozzle injects a second fuel spray toward the exit end of the combustion chamber. At ignition conditions, a majority of the fuel flow is injected through the pilot fuel nozzles, and at high power conditions a majority of the fuel flow is injected through the main fuel nozzles. At high power conditions, a fuel rich mixture is supplied to the combustion chamber, and a row of quench jets are configured to supply air to the combustion chamber, providing rich-quench-lean combustion.
    Type: Application
    Filed: August 25, 2017
    Publication date: February 28, 2019
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Rodolphe Dudebout, Sunil James
  • Patent number: 9400110
    Abstract: A combustor for a gas turbine engine is provided. The combustor includes an annular inner liner; an annular outer liner circumscribing the annular inner liner; and a combustor dome having a first edge coupled to the annular inner liner and a second edge coupled to the annular outer liner, the combustor dome forming a combustion chamber with the annular inner liner and the annular outer liner. The combustion chamber accommodates fluid flow through the annular inner and annular outer liners. The combustion chamber converges in the direction of the air flow to reduce a diameter of the combustion chamber. The combustor dome is configured to bifurcate the air flow at the combustor dome into a first stream directed to the annular inner liner and a second stream directed to the annular outer liner.
    Type: Grant
    Filed: October 19, 2012
    Date of Patent: July 26, 2016
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Rodolphe Dudebout, Terrel Kuhn, Vinayender Kuchana, Veeraraghava Raju Hasti, Raymond Gage, Sunil James
  • Patent number: 9080770
    Abstract: A combustor for a gas turbine engine is provided. The combustor includes an inner liner; an outer liner circumscribing the inner liner; and a combustor dome having a first edge coupled to the inner liner and a second edge coupled to the outer liner. The combustor dome forms a combustion chamber with the inner liner and the outer liner. The combustion chamber receives air flow through the inner and outer liners, and the combustor dome is configured to bifurcate the air flow at the combustor dome into a first stream directed to the inner liner and a second stream directed to the outer liner.
    Type: Grant
    Filed: June 6, 2011
    Date of Patent: July 14, 2015
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Rodolphe Dudebout, Veeraraghave Raju Hasti, Terrel Kuhn, Sunil James, Mario Scaini
  • Publication number: 20140109581
    Abstract: A combustor for a gas turbine engine is provided. The combustor includes an annular inner liner; an annular outer liner circumscribing the annular inner liner; and a combustor dome having a first edge coupled to the annular inner liner and a second edge coupled to the annular outer liner, the combustor dome forming a combustion chamber with the annular inner liner and the annular outer liner. The combustion chamber accommodates fluid flow through the annular inner and annular outer liners. The combustion chamber converges in the direction of the air flow to reduce a diameter of the combustion chamber. The combustor dome is configured to bifurcate the air flow at the combustor dome into a first stream directed to the annular inner liner and a second stream directed to the annular outer liner.
    Type: Application
    Filed: October 19, 2012
    Publication date: April 24, 2014
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Rodolphe Dudebout, Terrel Kuhn, Vinayender Kuchana, Veeraraghava Raju Hasti, Raymond Gage, Sunil James
  • Publication number: 20120304647
    Abstract: A combustor for a gas turbine engine is provided. The combustor includes an inner liner; an outer liner circumscribing the inner liner; and a combustor dome having a first edge coupled to the inner liner and a second edge coupled to the outer liner. The combustor dome forms a combustion chamber with the inner liner and the outer liner. The combustion chamber receives air flow through the inner and outer liners, and the combustor dome is configured to bifurcate the air flow at the combustor dome into a first stream directed to the inner liner and a second stream directed to the outer liner.
    Type: Application
    Filed: June 6, 2011
    Publication date: December 6, 2012
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Rodolphe Dudebout, Veeraraghava Raju Hasti, Terrel Kuhn, Sunil James, Mario Scaini