Patents by Inventor Prem Navin DHAYANANDAM

Prem Navin DHAYANANDAM 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: 11028709
    Abstract: An airfoil and shroud assembly includes an airfoil including a root end, a free end and a tenon extending from the free end, the tenon including a base and an externally threaded stud extending from the base. A shroud includes an opening configured to receive the base of the tenon. A nut is configured to be threadably coupled to the externally threaded stud on the tenon on the airfoil to couple the shroud to the airfoil.
    Type: Grant
    Filed: September 18, 2018
    Date of Patent: June 8, 2021
    Assignee: General Electric Company
    Inventors: Vasantharuban Subramanian, Ronald Denmark, Prem Navin Dhayanandam, Richard Gutta, Sanjeev Kumar Jha
  • Patent number: 10774652
    Abstract: An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in a scalable table identified as TABLE 1, wherein the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y, and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape. The resulting article may be used as a stator vane in a compressor.
    Type: Grant
    Filed: August 21, 2018
    Date of Patent: September 15, 2020
    Assignee: General Electric Company
    Inventors: Vasantharuban S, Prem Navin Dhayanandam, Lakshmanan Valliappan
  • Publication number: 20200088049
    Abstract: An airfoil and shroud assembly includes an airfoil including a root end, a free end and a tenon extending from the free end, the tenon including a base and an externally threaded stud extending from the base. A shroud includes an opening configured to receive the base of the tenon. A nut is configured to be threadably coupled to the externally threaded stud on the tenon on the airfoil to couple the shroud to the airfoil.
    Type: Application
    Filed: September 18, 2018
    Publication date: March 19, 2020
    Inventors: Vasantharuban Subramanian, Ronald Denmark, Prem Navin Dhayanandam, Richard Gutta, Sanjeev Kumar Jha
  • Publication number: 20190063228
    Abstract: An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in a scalable table identified as TABLE 1, wherein the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y, and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape. The resulting article may be used as a stator vane in a compressor.
    Type: Application
    Filed: August 21, 2018
    Publication date: February 28, 2019
    Inventors: Vasantharuban S, Prem Navin DHAYANANDAM, Lakshmanan VALLIAPPAN