Patents by Inventor Arun Kumar Jayasingh

Arun Kumar Jayasingh 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: 9759129
    Abstract: A gas turbine engine includes a nosecone assembly attached to a gas turbine engine. The nosecone assembly includes a support structure and a nosecone attached to the support structure. The nosecone includes at least a first tool hole extending through the nosecone. The first tool hole is structurally reinforced.
    Type: Grant
    Filed: December 26, 2013
    Date of Patent: September 12, 2017
    Assignee: United Technologies Corporation
    Inventors: Anthony T. Lindsey, Arun Kumar Jayasingh, Herbert L. Walker
  • Patent number: 9540939
    Abstract: A gas turbine engine includes a compressor section and a nosecone assembly. The compressor section includes an inlet guide vane assembly including an inner shroud, an outer shroud, and an inlet guide vane extending from the inner shroud to the outer shroud. The nosecone assembly is attached to the inner shroud.
    Type: Grant
    Filed: December 26, 2013
    Date of Patent: January 10, 2017
    Assignee: United Technologies Corporation
    Inventors: David Maliniak, Daniel J. Monahan, Jonathan D. Little, Veerachari J. Mayachari, Rakesh Sharma N. Dumavath, Arun Kumar Jayasingh, Herbert L. Walker
  • Publication number: 20150000304
    Abstract: A gas turbine engine includes a nosecone assembly attached to a gas turbine engine. The nosecone assembly includes a support structure and a nosecone attached to the support structure. The nosecone includes at least a first tool hole extending through the nosecone. The first tool hole is structurally reinforced.
    Type: Application
    Filed: December 26, 2013
    Publication date: January 1, 2015
    Inventors: Anthony T. Lindsey, Arun Kumar Jayasingh, Herbert L. Walker
  • Publication number: 20150003968
    Abstract: A gas turbine engine includes a compressor section and a nosecone assembly. The compressor section includes an inlet guide vane assembly including an inner shroud, an outer shroud, and an inlet guide vane extending from the inner shroud to the outer shroud. The nosecone assembly is attached to the inner shroud.
    Type: Application
    Filed: December 26, 2013
    Publication date: January 1, 2015
    Inventors: David Maliniak, Daniel J. Monahan, Jonathan D. Little, Veerachari J. Mayachari, Rakesh Sharma N. Dumavath, Arun Kumar Jayasingh, Herbert L. Walker