Patents by Inventor Vinod Govind Mengle

Vinod Govind Mengle 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: 20170082063
    Abstract: A method and apparatus for reducing noise generated during operation of a propulsion system. In one illustrative embodiment, a nozzle system comprises a first nozzle and a second nozzle at least partially surrounded by the first nozzle. An outer surface of an aft portion of the second nozzle has a shape configured such that a radial cross-section of the outer surface of the aft portion of the second nozzle has a curve that is different from at least one other curve for another radial cross-section of the outer surface of the aft portion of the second nozzle and such that an axial cross-section of the outer surface of the aft portion of the second nozzle has a wavy shape.
    Type: Application
    Filed: December 5, 2016
    Publication date: March 23, 2017
    Inventor: Vinod Govind Mengle
  • Patent number: 9511873
    Abstract: A method and apparatus for reducing noise generated during operation of an engine. In one illustrative embodiment, a nozzle system comprises a first nozzle and a second nozzle at least partially surrounded by the first nozzle. An outer surface of an aft portion of the second nozzle has a shape configured such that a radial cross-section of the outer surface of the aft portion of the second nozzle has a curve that is different from at least one other curve for another radial cross-section of the outer surface of the aft portion of the second nozzle and such that an axial cross-section of the outer surface of the aft portion of the second nozzle has a wavy shape.
    Type: Grant
    Filed: March 9, 2012
    Date of Patent: December 6, 2016
    Assignee: THE BOEING COMPANY
    Inventor: Vinod Govind Mengle
  • Publication number: 20130232948
    Abstract: A method and apparatus for reducing noise generated during operation of an engine. In one illustrative embodiment, a nozzle system comprises a first nozzle and a second nozzle at least partially surrounded by the first nozzle. An outer surface of an aft portion of the second nozzle has a shape configured such that a radial cross-section of the outer surface of the aft portion of the second nozzle has a curve that is different from at least one other curve for another radial cross-section of the outer surface of the aft portion of the second nozzle and such that an axial cross-section of the outer surface of the aft portion of the second nozzle has a wavy shape.
    Type: Application
    Filed: March 9, 2012
    Publication date: September 12, 2013
    Applicant: THE BOEING COMPANY
    Inventor: Vinod Govind Mengle