Patents by Inventor Santhosh Kumar Vijayan

Santhosh Kumar Vijayan 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: 20250055163
    Abstract: A system includes a first battery, a second battery, and a battery connector coupling the first battery to the second battery. The battery connector includes a first portion and a second portion. The second portion is narrower than the first portion. The second portion is configured to decouple the first battery from the second battery when a current above a threshold current passes through the second portion.
    Type: Application
    Filed: August 1, 2024
    Publication date: February 13, 2025
    Inventors: Santhosh Kumar Vijayan, Sumandra Ghosh Chowdhury, Rajeev Bammanni, Mohan Narasaiah
  • Publication number: 20250055125
    Abstract: A system includes an enclosure, a heat-source component disposed in the enclosure, and an exhaust associated with the enclosure. The exhaust is configured to exhaust heat generated by the heat-source component. The system further includes an arrester plate assembly disposed within the enclosure. The arrester plate assembly includes perforations formed therein. The arrester plate assembly is approximately parallel to the exhaust.
    Type: Application
    Filed: August 1, 2024
    Publication date: February 13, 2025
    Inventors: Santhosh Kumar Vijayan, Sumandra Ghosh Chowdhury, Rajeev Bammanni, Mohan Narasaiah
  • Publication number: 20240222943
    Abstract: A power system includes an enclosure and a sliding power distribution unit (PDU) configured to be at least partially within the enclosure in a closed position and to at least partially extend beyond the enclosure in an open position. The sliding PDU includes a plurality of outlets. The sliding PDU is configured to present a desired number of outlets of the plurality of outlets. The enclosure includes a locking screw to secure the sliding PDU in place in the open position. The enclosure further includes a stopper flange to limit movement of the sliding PDU to the open position. The sliding PDU may include a holding knob to secure and move the sliding PDU.
    Type: Application
    Filed: December 5, 2023
    Publication date: July 4, 2024
    Inventors: Dileep Anekal Venkataramanappa, Santhosh Kumar Vijayan, Aravindhan Rajendhiran
  • Publication number: 20230244574
    Abstract: An aspect of the present disclosure facilitates manual snapshot and restore of user applications hosted on cloud infrastructures. In one embodiment, a system receives setup data specifying a first set of actions (such as shutting off and restarting related services, etc.) to be performed upon receipt of a manual snapshot command with respect to a component of a user application hosted on a cloud infrastructure. Upon receiving the manual snapshot command to capture a current state of the component, the system performs the first set of actions along with capturing the current state of the component.
    Type: Application
    Filed: October 31, 2022
    Publication date: August 3, 2023
    Inventors: Santhosh Kumar Vijayan, Sampanna Hegde, Pranav Gupta, Esha Doda
  • Patent number: 10563543
    Abstract: The present disclosure provides an exhaust diffuser for a gas turbine engine. The exhaust diffuser may include a hub, a casing, and a strut extending between the hub and the casing. The hub may include an angled configuration about the strut and a substantially flat configuration downstream of the angled configuration.
    Type: Grant
    Filed: May 31, 2016
    Date of Patent: February 18, 2020
    Assignee: General Electric Company
    Inventors: Santhosh Kumar Vijayan, Deepesh Dinesh Nanda, Manjunath Bangalore Chengappa
  • Patent number: 10392975
    Abstract: An exhaust gas diffuser (38) including: a radially-outer peripheral casing (46); a hub (42) located within said radially-outer peripheral casing and coaxial with a center axis (40) of the casing; main struts (44) located at circumferentially-spaced locations about the hub and extending radially-outwardly to the radially outer peripheral casing; and small struts (52) located at circumferentially-spaced locations between the main struts; wherein the main struts and small struts have substantially parallel longitudinal chord lines and each of the small struts have a cross-sectional area smaller than a cross-sectional area of the main struts.
    Type: Grant
    Filed: March 18, 2014
    Date of Patent: August 27, 2019
    Assignee: General Electric Company
    Inventors: Deepesh D. Nanda, Santhosh Kumar Vijayan, Chengappa Manjunath, Tomasz Jendrzejewski
  • Patent number: 10253638
    Abstract: Embodiments of the present disclosure are directed toward systems including a turbomachine blade tip shroud having a pressure side portion and a suction side portion. The pressure side portion and the suction side portion are divided by a mean camber line of a turbomachine blade, and the pressure side portion has a greater surface area than the suction side portion.
    Type: Grant
    Filed: August 12, 2015
    Date of Patent: April 9, 2019
    Assignee: General Electric Company
    Inventors: Rohit Chouhan, Sumeet Soni, Paul Kendall Smith, Srinivasa Govardhan Jayana, Sylvain Pierre, Harish Bommanakatte, Santhosh Kumar Vijayan, Spencer Aaron Kareff
  • Publication number: 20170342862
    Abstract: The present application provides an exhaust diffuser for a gas turbine engine. The exhaust diffuser may include a hub, a casing, and a strut extending between the hub and the casing. The hub may include an angled configuration about the strut and a substantially flat configuration downstream of the angled configuration.
    Type: Application
    Filed: May 31, 2016
    Publication date: November 30, 2017
    Inventors: Santhosh Kumar Vijayan, Deepesh Dinesh Nanda, Manjunath Bangalore Chengappa
  • Publication number: 20170130610
    Abstract: An exhaust gas diffuser (38) including: a radially-outer peripheral casing (46); a hub (42) located within said radially-outer peripheral casing and coaxial with a center axis (40) of the casing; main struts (44) located at circumferentially-spaced locations about the hub and extending radially-outwardly to the radially outer peripheral casing; and small struts (52) located at circumferentially-spaced locations between the main struts; wherein the main struts and small struts have substantially parallel longitudinal chord lines and each of the small struts have a cross-sectional area smaller than a cross-sectional area of the main struts.
    Type: Application
    Filed: March 18, 2014
    Publication date: May 11, 2017
    Inventors: Deepesh D. Nanda, Santhosh Kumar Vijayan, Chengappa Manjunath, Tomasz Jendrzejewski
  • Patent number: 9291061
    Abstract: Embodiments of the present disclosure include a turbomachine having a turbomachine blade and a stationary structural component. The turbomachine blade includes a tip shroud having a leading edge portion where the leading edge portion has a first surface. The stationary structural component is disposed about the turbomachine blade and includes a corresponding portion corresponding to the leading edge portion of the tip shroud, where the corresponding portion has a second surface, where the first surface and the second surface have generally parallel contours.
    Type: Grant
    Filed: April 13, 2012
    Date of Patent: March 22, 2016
    Assignee: General Electric Company
    Inventors: Rohit Chouhan, Sylvain Pierre, Gunnar Leif Siden, Santhosh Kumar Vijayan, Joseph Anthony Cotroneo
  • Patent number: 9267391
    Abstract: A diffuser assembly is provided herein. In certain embodiments, the diffuser assembly may include an outer boundary member and an inner boundary member, with the inner boundary member being positioned radially inward of the outer boundary member. The diffuser assembly also may include an exhaust flow path defined between the outer boundary member and the inner boundary member. Further, the diffuser assembly may include at least one flow deflecting member operatively attached to the outer boundary member. The flow deflecting member may be adjustable about the outer boundary member to produce a substantially uniform velocity distribution within the exhaust flow path.
    Type: Grant
    Filed: December 21, 2012
    Date of Patent: February 23, 2016
    Assignee: General Electric Company
    Inventors: Santhosh Kumar Vijayan, Deepesh D Nanda
  • Publication number: 20150345306
    Abstract: Embodiments of the present disclosure are directed toward systems including a turbomachine blade tip shroud having a pressure side portion and a suction side portion. The pressure side portion and the suction side portion are divided by a mean camber line of a turbomachine blade, and the pressure side portion has a greater surface area than the suction side portion.
    Type: Application
    Filed: August 12, 2015
    Publication date: December 3, 2015
    Applicant: General Electric Company
    Inventors: Rohit Chouhan, Sumeet Soni, Paul Kendall Smith, Srinivasa Govardhan Jayana, Sylvain Pierre, Harish Bommanakatte, Santhosh Kumar Vijayan, Spencer Aaron Kareff
  • Publication number: 20150240667
    Abstract: An exhaust gas diffuser for a turbomachine includes a diffuser supported on a turbine rotor, aligned with an axis of said turbine rotor. The diffuser is configured to re-direct turbine exhaust gas substantially ninety degrees from a first direction of flow along the rotor axis. A plenum chamber is in fluid communication with and surrounds an outlet end of the diffuser. The plenum chamber is in fluid communication with a transition duct adapted to supply the exhaust gas to another turbomachine. The plenum chamber expands in volume between the diffuser and the transition duct.
    Type: Application
    Filed: February 26, 2014
    Publication date: August 27, 2015
    Applicant: General Electric Company
    Inventors: Deepesh D. Nanda, Santhosh Kumar Vijayan, Chengappa Manjunath
  • Patent number: 9109455
    Abstract: Embodiments of the present disclosure are directed toward systems including a turbomachine blade tip shroud having a pressure side portion and a suction side portion. The pressure side portion and the suction side portion are divided by a mean camber line of a turbomachine blade, and the pressure side portion has a greater surface area than the suction side portion.
    Type: Grant
    Filed: January 20, 2012
    Date of Patent: August 18, 2015
    Assignee: General Electric Company
    Inventors: Rohit Chouhan, Sumeet Soni, Paul Kendall Smith, Srinivasa Govardhan Jayana, Sylvain Pierre, Harish Bommanakatte, Santhosh Kumar Vijayan, Spencer Aaron Kareff
  • Patent number: 8807927
    Abstract: A flow control assembly is provided, including a member and a wall. The member has a surface, a flow diverting member and a rail member. The rail member is situated upstream of the flow diverting member. The flow diverting member and the rail member each project from the surface of the member. The flow diverting member has a distal end. The wall is disposed in relation to the member to create a clearance gap between the distal end of the flow diverting member and the wall. A fluid path is created between the member and the wall, and flows from an upstream section and through the clearance gap. A first chamber and a second chamber are defined by the wall and located upstream of the clearance gap.
    Type: Grant
    Filed: September 29, 2011
    Date of Patent: August 19, 2014
    Assignee: General Electric Company
    Inventors: Ramesh Kempanna Babu, Rohit Chouhan, Santhosh Kumar Vijayan
  • Publication number: 20140178191
    Abstract: A diffuser assembly is provided herein. In certain embodiments, the diffuser assembly may include an outer boundary member and an inner boundary member, with the inner boundary member being positioned radially inward of the outer boundary member. The diffuser assembly also may include an exhaust flow path defined between the outer boundary member and the inner boundary member. Further, the diffuser assembly may include at least one flow deflecting member operatively attached to the outer boundary member. The flow deflecting member may be adjustable about the outer boundary member to produce a substantially uniform velocity distribution within the exhaust flow path.
    Type: Application
    Filed: December 21, 2012
    Publication date: June 26, 2014
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Santhosh Kumar Vijayan, Deepesh D. Nanda
  • Publication number: 20130272888
    Abstract: Embodiments of the present disclosure include a turbomachine having a turbomachine blade and a stationary structural component. The turbomachine blade includes a tip shroud having a leading edge portion where the leading edge portion has a first surface. The stationary structural component is disposed about the turbomachine blade and includes a corresponding portion corresponding to the leading edge portion of the tip shroud, where the corresponding portion has a second surface, where the first surface and the second surface have generally parallel contours.
    Type: Application
    Filed: April 13, 2012
    Publication date: October 17, 2013
    Applicant: General Electric Company
    Inventors: Rohit Chouhan, Sylvain Pierre, Gunnar Leif Siden, Santhosh Kumar Vijayan, Joseph Anthony Cotroneo
  • Publication number: 20130189106
    Abstract: Embodiments of the present disclosure are directed toward systems including a turbomachine blade tip shroud having a pressure side portion and a suction side portion. The pressure side portion and the suction side portion are divided by a mean camber line of a turbomachine blade, and the pressure side portion has a greater surface area than the suction side portion.
    Type: Application
    Filed: January 20, 2012
    Publication date: July 25, 2013
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Rohit Chouhan, Sumeet Soni, Paul Kendall Smith, Srinivasa Govardhan Jayana, Sylvain Pierre, Harish Bommanakatte, Santhosh Kumar Vijayan, Spencer Aaron Kareff
  • Publication number: 20130084168
    Abstract: A flow control assembly is provided, including a member and a wall. The member has a surface, a flow diverting member and a rail member. The rail member is situated upstream of the flow diverting member. The flow diverting member and the rail member each project from the surface of the member. The flow diverting member has a distal end. The wall is disposed in relation to the member to create a clearance gap between the distal end of the flow diverting member and the wall. A fluid path is created between the member and the wall, and flows from an upstream section and through the clearance gap. A first chamber and a second chamber are defined by the wall and located upstream of the clearance gap.
    Type: Application
    Filed: September 29, 2011
    Publication date: April 4, 2013
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Ramesh Kempanna Babu, Rohit Chouhan, Santhosh Kumar Vijayan