Patents by Inventor Bala Muralidhar Singh Bahadur

Bala Muralidhar Singh Bahadur 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: 11187560
    Abstract: A traverse mechanism for measuring flow characteristics in a fluid flow path is provided. The traverse mechanism includes a rotating member configured to rotate 360 degrees about an axis in a circumferential direction. The traverse mechanism also includes a probe coupled to the rotating member. The probe extends in a radial direction relative to the axis through a portion the rotating member into the fluid flow path. Rotation of the rotating member enables the probe to map or measure one or more flow characteristic in the fluid flow path 360 degrees about the axis in the circumferential direction.
    Type: Grant
    Filed: October 3, 2019
    Date of Patent: November 30, 2021
    Assignee: GENERAL ELECTRIC COMPANY
    Inventors: Bala Muralidhar Singh Bahadur, Joshy John, Srinivas Rao Pakkala
  • Publication number: 20210102824
    Abstract: A traverse mechanism for measuring flow characteristics in a fluid flow path is provided. The traverse mechanism includes a rotating member configured to rotate 360 degrees about an axis in a circumferential direction. The traverse mechanism also includes a probe coupled to the rotating member. The probe extends in a radial direction relative to the axis through a portion the rotating member into the fluid flow path. Rotation of the rotating member enables the probe to map or measure one or more flow characteristic in the fluid flow path 360 degrees about the axis in the circumferential direction.
    Type: Application
    Filed: October 3, 2019
    Publication date: April 8, 2021
    Inventors: Bala Muralidhar Singh Bahadur, Joshy John, Srinivas Rao Pakkala
  • Patent number: 8602727
    Abstract: Turbine nozzle segments with trimmed leading edges are disclosed. In one embodiment of the invention, a turbine static nozzle airfoil includes: an arcuate concave leading edge; and a substantially flat trailing edge.
    Type: Grant
    Filed: July 22, 2010
    Date of Patent: December 10, 2013
    Assignee: General Electric Company
    Inventor: Bala Muralidhar Singh Bahadur
  • Publication number: 20120020804
    Abstract: Turbine nozzle segments with trimmed leading edges are disclosed. In one embodiment of the invention, a turbine static nozzle airfoil includes: an arcuate concave leading edge; and a substantially flat trailing edge.
    Type: Application
    Filed: July 22, 2010
    Publication date: January 26, 2012
    Applicant: GENERAL ELECTRIC COMPANY
    Inventor: Bala Muralidhar Singh Bahadur