Patents by Inventor Moorthi Subramaniyan
Moorthi Subramaniyan 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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Patent number: 11859817Abstract: A system and method of igniting a coal air-fuel mixture, including a burner having a burner tube operable to carry a flowing mixture of fuel and air to a furnace for combustion therein and a first flow directing device disposed within the tube, operable to direct a first portion of the flowing fuel and air mixture to a location in the burner tube. The system also includes a laser igniter within the burner tube, the laser igniter including a laser tube having a first end with a laser light input and a second end with a light output, and a laser light source operably coupled to the laser light input. The laser light source, including a laser. The laser ignitor directing photons from the light output at the location in the burner tube to ignite at least a part of the first portion of the fuel.Type: GrantFiled: December 7, 2020Date of Patent: January 2, 2024Assignee: GENERAL ELECTRIC COMPANYInventors: Sameer Dinkar Vartak, Sreenivasa Rao Gubba, Kamesh Lakshmi Narayanan, Arun Kumar Sridharan, Ankur Maheshwari, Dragisa Ristic, Moorthi Subramaniyan
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Patent number: 11804984Abstract: Described embodiments provide systems and methods of forming overlay tunnels for delivery of data between networked devices. A first intermediary device may transmit, responsive to a connection request from a client, a request having a source IP address corresponding to a first virtual IP address of the first device and a first payload including first security hash information to be processed by a second intermediary device. The first device may receive, from the second intermediary device, a response. The response may have a source IP address corresponding to the IP address of the server and a second payload including a virtual IP address of the second device, responsive to second security hash information corresponding to the first security hash information. The first device may establish an overlay tunnel using the first virtual IP address and the second virtual IP address for communicating data between the client and the server.Type: GrantFiled: May 18, 2021Date of Patent: October 31, 2023Inventors: Karthick Srivatsan, Chaitra Maraliga Ramaiah, Anand Medikeri, Rajnesh Raturi, Moorthi Subramaniyan, Sandeep Manohar Nirikhi
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Patent number: 11519273Abstract: A rotor blade includes an airfoil having an airfoil shape. The airfoil shape has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, Table VIII, or Table IX. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape.Type: GrantFiled: July 16, 2021Date of Patent: December 6, 2022Assignee: General Electric CompanyInventors: Michael James Healy, Matthew John McKeever, Sabarinath Devarajan, Uday Krishna Pappala, Kevin Michael Barnett, Kumaran Vale Mudaliar, Wilfried Rick, Moorthi Subramaniyan, Karan Ghule, Denis Stankovic, Yu Wang, Marco Micheli, Mariadas Anton Charles Anandarajah, Michael Loetzerich
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Publication number: 20220372878Abstract: A rotor blade includes an airfoil having an airfoil shape. The airfoil shape has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, Table VIII, or Table IX. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape.Type: ApplicationFiled: July 16, 2021Publication date: November 24, 2022Inventors: Michael James Healy, Matthew John McKeever, Sabarinath Devarajan, Uday Krishna Pappala, Kevin Michael Barnett, Kumaran Vale Mudaliar, Wilfried Rick, Moorthi Subramaniyan, Karan Ghule, Denis Stankovic, Yu Wang, Marco Micheli, Mariadas Anton Charles Anandarajah, Michael Loetzerich
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Patent number: 11459892Abstract: A stator vane includes an airfoil having an airfoil shape. The airfoil shape having has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, Table IV, Table V, Table VI, Table VII, Table VIII, Table IX, Table X, Table XI, or Table XII. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape.Type: GrantFiled: November 9, 2021Date of Patent: October 4, 2022Assignee: General Electric CompanyInventors: Matthew John McKeever, Michael James Healy, Wilfried Rick, Rozila Nausheen, Sabarinath Devarajan, Moorthi Subramaniyan, Vsevolod Yuriyevich Ostrovskiy, Kumaran Vale Mudaliar, Damir Novak, Thomas Sommer, Aditya Rajeshbhai Shah, Uday Krishna Pappala, Kevin Michael Barnett, Josip Galic, Gurulakshmi Polisetty, Paul G. Deivernois, Dejan Mikasinovic
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Patent number: 11454120Abstract: A turbine blade for a rotary machine includes an airfoil that extends from a root to a tip along a radial span. The airfoil further includes a first sidewall and a second sidewall that are coupled together at a leading edge of the airfoil and that extend aftward to a trailing edge of the airfoil. One of the first sidewall or the second sidewall includes a tip region having an increased stagger angle that produces a non-linear, over-hanging trailing edge.Type: GrantFiled: December 7, 2018Date of Patent: September 27, 2022Assignee: GENERAL ELECTRIC COMPANYInventors: Adam Fredmonski, Moorthi Subramaniyan
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Publication number: 20220178539Abstract: A system and method of igniting a coal air-fuel mixture, including a burner having a burner tube operable to carry a flowing mixture of fuel and air to a furnace for combustion therein and a first flow directing device disposed within the tube, operable to direct a first portion of the flowing fuel and air mixture to a location in the burner tube. The system also includes a laser igniter within the burner tube, the laser igniter including a laser tube having a first end with a laser light input and a second end with a light output, and a laser light source operably coupled to the laser light input. The laser light source, including a laser. The laser ignitor directing photons from the light output at the location in the burner tube to ignite at least a part of the first portion of the fuel.Type: ApplicationFiled: December 7, 2020Publication date: June 9, 2022Applicant: GENERAL ELECTRIC COMPANYInventors: SAMEER DINKAR VARTAK, SREENIVASA RAO GUBBA, KAMESH LAKSHMI NARAYANAN, ARUN KUMAR SRIDHARAN, ANKUR MAHESHWARI, DRAGISA RISTIC, MOORTHI SUBRAMANIYAN
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Publication number: 20220082023Abstract: Turbine blades with non-axisymmetric forward features are provided. A turbine blade may include a platform and an airfoil extending radially outward from the platform and configured to extend into a fluid flowpath. The airfoil separates an upstream portion of the fluid flowpath from a downstream portion of the fluid flowpath. A sealing member extends axially from the platform toward a stationary nozzle adjacent the platform and separates the fluid flowpath from a wheel space. The platform may have a forward face between the sealing member and the airfoil and, optionally, a forward axial face between the forward face and the airfoil. The forward face or forward axial face may face the upstream portion of the fluid flowpath and may have a profile that is non-axisymmetric with respect to its centerline axis.Type: ApplicationFiled: September 18, 2020Publication date: March 17, 2022Inventors: Moorthi Subramaniyan, Adam John Fredmonski
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Publication number: 20210281444Abstract: Described embodiments provide systems and methods of forming overlay tunnels for delivery of data between networked devices. A first intermediary device may transmit, responsive to a connection request from a client, a request having a source IP address corresponding to a first virtual IP address of the first device and a first payload including first security hash information to be processed by a second intermediary device. The first device may receive, from the second intermediary device, a response. The response may have a source IP address corresponding to the IP address of the server and a second payload including a virtual IP address of the second device, responsive to second security hash information corresponding to the first security hash information. The first device may establish an overlay tunnel using the first virtual IP address and the second virtual IP address for communicating data between the client and the server.Type: ApplicationFiled: May 18, 2021Publication date: September 9, 2021Applicant: Citrix Systems, Inc.Inventors: Karthick Srivatsan, Chaitra Maraliga Ramaiah, Anand Medikeri, Rajnesh Raturi, Moorthi Subramaniyan, Sandeep Manohar Nirikhi
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Patent number: 11044117Abstract: Described embodiments provide systems and methods of forming overlay tunnels for delivery of data between networked devices. A first intermediary device may transmit, responsive to a connection request from a client, a request having a source IP address corresponding to a first virtual IP address of the first device and a first payload including first security hash information to be processed by a second intermediary device. The first device may receive, from the second intermediary device, a response. The response may have a source IP address corresponding to the IP address of the server and a second payload including a virtual IP address of the second device, responsive to second security hash information corresponding to the first security hash information. The first device may establish an overlay tunnel using the first virtual IP address and the second virtual IP address for communicating data between the client and the server.Type: GrantFiled: December 26, 2018Date of Patent: June 22, 2021Assignee: Citrix Systems, Inc.Inventors: Karthick Srivatsan, Chaitra Maraliga Ramaiah, Anand Medikeri, Rajnesh Raturi, Moorthi Subramaniyan, Sandeep Manohar Nirikhi
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Patent number: 10982549Abstract: Stator vanes including curved trailing edges are disclosed. The stator vanes may include a body including a central section, a tip section positioned radially above the central section, and a root section positioned radially below the central section. The body of the stator vanes may also include a leading edge extending radially adjacent the root section, central section, and tip section, respectively, and a trailing edge positioned opposite and aft to the leading edge. The trailing edge may include a concave contour including a first portion radially aligned with the central section of the body. The first portion may be axially offset and forward of a reference line that may be perpendicular to an axial direction and intersects the concave contour at the tip section and the root section. A concavity of the first portion of the concave contour may be formed radially aft of the central section.Type: GrantFiled: March 21, 2018Date of Patent: April 20, 2021Assignee: General Electric CompanyInventors: Moorthi Subramaniyan, Adam John Fredmonski, Francesco Soranna
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Patent number: 10830082Abstract: A system for a turbomachine includes a rotor blade configured to rotate along a circumferential direction within a casing of the turbomachine and a shroud positioned outward of the rotor blade along a radial direction. The rotor blade includes a root, a tip spaced radially outward from the root, a pressure side tip rail that extends around the tip of the rotor blade along a pressure side wall, and a suction side tip rail that extends around the tip of the rotor blade along a suction side wall. The shroud includes a radially inner surface facing the pressure side tip rail and the suction side tip rail of the rotor blade and spaced from the pressure side tip rail and the suction side tip rail of the rotor blade by a clearance gap. The shroud also includes a plurality of grooves extending continuously along the circumferential direction.Type: GrantFiled: July 7, 2018Date of Patent: November 10, 2020Assignee: General Electric CompanyInventor: Moorthi Subramaniyan
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Publication number: 20200213151Abstract: Described embodiments provide systems and methods of forming overlay tunnels for delivery of data between networked devices. A first intermediary device may transmit, responsive to a connection request from a client, a request having a source IP address corresponding to a first virtual IP address of the first device and a first payload including first security hash information to be processed by a second intermediary device. The first device may receive, from the second intermediary device, a response. The response may have a source IP address corresponding to the IP address of the server and a second payload including a virtual IP address of the second device, responsive to second security hash information corresponding to the first security hash information. The first device may establish an overlay tunnel using the first virtual IP address and the second virtual IP address for communicating data between the client and the server.Type: ApplicationFiled: December 26, 2018Publication date: July 2, 2020Inventors: Karthick Srivatsan, Chaitra Maraliga Ramaiah, Anand Medikeri, Rajnesh Raturi, Moorthi Subramaniyan, Sandeep Manohar Nirikhi
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Publication number: 20200182065Abstract: A turbine blade for a rotary machine includes an airfoil that extends from a root to a tip along a radial span. The airfoil further includes a first sidewall and a second sidewall that are coupled together at a leading edge of the airfoil and that extend aftward to a trailing edge of the airfoil. One of the first sidewall or the second sidewall includes a tip region having an increased stagger angle that produces a non-linear, over-hanging trailing edge.Type: ApplicationFiled: December 7, 2018Publication date: June 11, 2020Inventors: Adam Fredmonski, Moorthi Subramaniyan
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Patent number: 10567348Abstract: Described embodiments establish at least one secure connection for a session. An intermediary device may intercept a domain name service (DNS) request from a client. The device may determine, according to the intercepted DNS request and configuration data of the device, that the client is preparing to establish a session with a server. The device may send a client hello message of the device to the server for establishing a first secure connection between the device and the server for the session, prior to the client sending a client hello message of the client for establishing a second secure connection between the client and the device for the session. The second secure connection may be established between the client and the device using a specified value for a session identifier received from the server in response to the client hello message of the device.Type: GrantFiled: July 6, 2017Date of Patent: February 18, 2020Assignee: Citrix Systems, Inc.Inventors: Moorthi Subramaniyan, Praveen Raja Dhanabalan
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Patent number: 10465709Abstract: A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances.Type: GrantFiled: September 28, 2016Date of Patent: November 5, 2019Assignee: General Electric CompanyInventors: Moorthi Subramaniyan, Sagar Kamble
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Patent number: 10465710Abstract: A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances.Type: GrantFiled: September 28, 2016Date of Patent: November 5, 2019Assignee: General Electric CompanyInventors: Moorthi Subramaniyan, Sagar Kamble
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Patent number: 10443405Abstract: A rotor blade includes an airfoil. The airfoil includes a leading edge and a trailing edge downstream of the leading edge. The airfoil also includes a radially outer tip with a pressure side tip rail and a suction side tip rail. A slot is formed in an aft portion of the suction side tip rail and an opening is positioned between the suction side tip rail and the pressure side tip rail at the trailing edge. Gas flows from the tip via the slot and the opening to inhibit formation of a vortex flow proximate to the suction side of the airfoil.Type: GrantFiled: May 10, 2017Date of Patent: October 15, 2019Assignee: General Electric CompanyInventors: Moorthi Subramaniyan, Adam John Fredmonski
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Publication number: 20190264569Abstract: A turbine blade including an airfoil extending radially from a platform above a shank is disclosed. The airfoil has a leading edge; a trailing edge; and a pressure side wall and a suction side wall extending between the leading edge and trailing edge. The turbine blade includes a chamber in at least one of the airfoil and platform. The chamber is configured to deliver a first fluid therein having a higher pressure than a second fluid in a wheel space adjacent the shank. The turbine blade includes an exiting hole in fluid communication with the chamber, positioned at a location upstream of the leading edge and circumferentially to a side of a selected side wall of the pressure side wall and suction side wall. In operation, the first fluid exits the exiting hole to increase a momentum of a boundary layer film near the selected side wall, preventing wheel space leakage from negatively impacting the boundary layer film.Type: ApplicationFiled: February 23, 2018Publication date: August 29, 2019Inventors: Moorthi Subramaniyan, Adam John Fredmonski
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Patent number: 10344604Abstract: A turbomachine diffuser includes a body having an inner surface defining a diffuser flow path, a plurality of stationary struts extending from the inner surface, and a plurality of flow mixing lobes arranged in an annular array on the inner surface. The plurality of flow mixing lobes is configured and disposed to guide a substantially high momentum flow toward the inner surface of the body.Type: GrantFiled: May 20, 2016Date of Patent: July 9, 2019Assignee: General Electric CompanyInventors: Moorthi Subramaniyan, Pradeep Patel