Patents by Inventor MARCUS TIMOTHY HOLCOMB

MARCUS TIMOTHY HOLCOMB 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).

  • Combustor liner
    Patent number: 8863527
    Abstract: A combustor liner for a turbine engine is disclosed herein. The combustor liner includes an inner liner surface operable to define at least part of a combustion chamber in a turbine engine. The inner liner surface extends along a portion of a chordal arc on a first side of the chordal arc. The combustor liner also includes a bearing surface operable to support a floating dome panel. At least part of the bearing surface is spaced from the chordal arc on a second side of the chordal arc opposite the first side.
    Type: Grant
    Filed: April 30, 2009
    Date of Patent: October 21, 2014
    Assignee: Rolls-Royce Corporation
    Inventors: Marcus Timothy Holcomb, Todd Taylor, Randall E. Yount
  • GAS TURBINE ENGINE, COMBUSTOR AND DOME PANEL
    Publication number: 20130174562
    Abstract: One embodiment of the present invention is a unique dome panel for a gas turbine engine combustor. Another embodiment is a unique gas turbine combustor. Yet another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and combustion systems and components. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
    Type: Application
    Filed: January 11, 2012
    Publication date: July 11, 2013
    Inventors: Marcus Timothy Holcomb, Todd Taylor
  • COMBUSTOR LINER
    Publication number: 20100275606
    Abstract: A combustor liner for a turbine engine is disclosed herein. The combustor liner includes an inner liner surface operable to define at least part of a combustion chamber in a turbine engine. The inner liner surface extends along a portion of a chordal arc on a first side of the chordal arc. The combustor liner also includes a bearing surface operable to support a floating dome panel. At least part of the bearing surface is spaced from the chordal arc on a second side of the chordal arc opposite the first side.
    Type: Application
    Filed: April 30, 2009
    Publication date: November 4, 2010
    Inventors: MARCUS TIMOTHY HOLCOMB, Todd Taylor, Randall E. Yount