Patents by Inventor Eric William Engebretsen

Eric William Engebretsen 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: 10024191
    Abstract: A containment system for a gas turbine engine includes a fan track assembly for use with a containment case. The fan track assembly includes a body of collapsible material that is positioned within a cavity of the fan case, and voids are provided for providing space in the event of a catastrophic blade failure. Various configurations of the fan track liner assembly are provided along with various mounting methodologies for securing the track liner assembly to the fan case of a gas turbine engine.
    Type: Grant
    Filed: September 5, 2013
    Date of Patent: July 17, 2018
    Assignee: ROLLS-ROYCE CORPORATION
    Inventors: Trevor John Totten, Jonathan Michael Rivers, Eric William Engebretsen, Matthew Joseph Kappes
  • Patent number: 9481448
    Abstract: An aerodynamic fan nosecone for a gas turbine engine is provided and includes a fan nosecone that may be made of composite material. To improve airflow transition to the blade members, aerodynamic fairings are provided and are secured to an exterior surface of the nosecone which enhances fuel economy. The fairings may be secured to the nosecone by various methods, including providing for the fairings to be changed out and replaced with other fairings on the same nosecone assembly.
    Type: Grant
    Filed: September 24, 2013
    Date of Patent: November 1, 2016
    Assignee: Rolls-Royce Corporation
    Inventors: Trevor John Totten, Jonathan Michael Rivers, Eric William Engebretsen
  • Publication number: 20140255152
    Abstract: A containment system for a gas turbine engine includes a fan track assembly for use with a containment case. The fan track assembly includes a body of collapsible material that is positioned within a cavity of the fan case, and voids are provided for providing space in the event of a catastrophic blade failure. Various configurations of the fan track liner assembly are provided along with various mounting methodologies for securing the track liner assembly to the fan case of a gas turbine engine.
    Type: Application
    Filed: September 5, 2013
    Publication date: September 11, 2014
    Applicant: Rolls-Royce Corporation
    Inventors: Trevor John Totten, Jonathan Michael Rivers, Eric William Engebretsen, Matthew Joseph Kappes
  • Publication number: 20140255204
    Abstract: An aerodynamic fan nosecone for a gas turbine engine is provided and includes a fan nosecone that may be made of composite material. To improve airflow transition to the blade members, aerodynamic fairings are provided and are secured to an exterior surface of the nosecone which enhances fuel economy. The fairings may be secured to the nosecone by various methods, including providing for the fairings to be changed out and replaced with other fairings on the same nosecone assembly.
    Type: Application
    Filed: September 24, 2013
    Publication date: September 11, 2014
    Applicant: Rolls-Royce Corporation
    Inventors: Trevor John Totten, Jonathan Michael Rivers, Eric William Engebretsen
  • Patent number: 8322991
    Abstract: A balance weight adapted to be assembled to a nose cone assembly of a turbine engine for improving a balance of the nose cone assembly is disclosed herein. The balance weight is one-piece and formed from a plurality of different materials including at least first and second materials. The first and second materials are arranged substantially heterogeneously relative to one another such that said first and second materials are separate from one another and fixed together.
    Type: Grant
    Filed: April 10, 2009
    Date of Patent: December 4, 2012
    Assignee: Rolls-Royce Corporation
    Inventors: Russel MacFarlane, Eric William Engebretsen
  • Publication number: 20100260605
    Abstract: A balance weight adapted to be assembled to a nose cone assembly of a turbine engine for improving a balance of the nose cone assembly is disclosed herein. The balance weight is one-piece and formed from a plurality of different materials including at least first and second materials. The first and second materials are arranged substantially heterogeneously relative to one another such that said first and second materials are separate from one another and fixed together.
    Type: Application
    Filed: April 10, 2009
    Publication date: October 14, 2010
    Inventors: Russel MACFARLANE, Eric William Engebretsen