Patents by Inventor Mohan Razdan

Mohan Razdan 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: 20200025378
    Abstract: A gas turbine engine includes a combustor having a dual-wall impingement convention effusion combustor tile assembly. The dual-wall tile assembly provides a cooling air flow channel and attachments for securing the tile to the cold skin liner of the combustor. Cooling is more efficient in part due to the dual wall construction and in part due to reduced parasitic leakage, and the design is less sensitive to attachment features which operate at lower temperatures.
    Type: Application
    Filed: July 31, 2019
    Publication date: January 23, 2020
    Inventors: Jack D. Petty, SR., Mohan Razdan, Michael S. Bell, Michel S. Smallwood, Tab M. Heffernan
  • Patent number: 10451276
    Abstract: A gas turbine engine includes a combustor having a dual-wall impingement convention effusion combustor tile assembly. The dual-wall tile assembly provides a cooling air flow channel and attachments for securing the tile to the cold skin liner of the combustor. Cooling is more efficient in part due to the dual wall construction and in part due to reduced parasitic leakage, and the design is less sensitive to attachment features which operate at lower temperatures.
    Type: Grant
    Filed: December 20, 2013
    Date of Patent: October 22, 2019
    Assignees: Rolls-Royce North American Technologies, Inc., Rolls-Royce Corporation
    Inventors: Jack D. Petty, Sr., Mohan Razdan, Michael S. Bell, Michel S. Smallwood, Tab M. Heffernan
  • Publication number: 20140250894
    Abstract: A gas turbine engine includes a combustor having a dual-wall impingement convention effusion combustor tile assembly. The dual-wall tile assembly provides a cooling air flow channel and attachments for securing the tile to the cold skin liner of the combustor. Cooling is more efficient in part due to the dual wall construction and in part due to reduced parasitic leakage, and the design is less sensitive to attachment features which operate at lower temperatures.
    Type: Application
    Filed: December 20, 2013
    Publication date: September 11, 2014
    Applicants: Rolls-Royce North American Technologies, Inc., Rolls-Royce Corporation
    Inventors: Jack D. Petty, SR., Mohan Razdan, Michael S. Bell, Michel S. Smallwood, Tab M. Heffernan, Charles B. Graves