Patents by Inventor Dennis A. McQueen

Dennis A. McQueen 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: 20170211478
    Abstract: A tubular fin heat exchanger is provided with an integrated fan within the confines of a duct assembly. The tubular heat exchanger provides a structure and pathway to minimize space and weight of the integrated heat exchanger into the gas turbine engine.
    Type: Application
    Filed: April 11, 2014
    Publication date: July 27, 2017
    Inventors: Michael Ralph STORAGE, Dennis MCQUEEN, Mark Phillip DRAKE, Maxime PEREIRA
  • Patent number: 8510945
    Abstract: A method of assembling a heat exchanger in a gas turbine engine assembly is provided. The method includes providing a structural body including a wall having an elongated slot, providing a heat exchanger operably associated with a bracket, and providing a slip joint for coupling the bracket to the structural body. The slip joint includes a standoff, an elongated member, and a biasing member disposed about the elongated member. The standoff is inserted through the wall so that the biasing member imparts a predetermined biasing force between the bracket and the structural body. The slip joint allows relative sliding movement between the bracket and the structural body when a sliding force due to thermal expansion or contraction is greater than the biasing force.
    Type: Grant
    Filed: June 30, 2010
    Date of Patent: August 20, 2013
    Assignee: Unison Industries, LLC
    Inventors: John Hand, Bernard A. Luschek, Lonnie R. Stewart, Michael J. Gilloon, Walter A. Hundley, Jr., Jerry W. Myers, Dennis A. McQueen, Michael Peoples
  • Publication number: 20110146944
    Abstract: A mounting assembly for a heat exchanger for a gas turbine engine. The heat exchanger assembly includes a plurality of arcuate manifolds each supporting an array of fins extending from a radial inner surface. A plurality of circumferentially extending spaced weld tabs is integrally formed on the radial outer surface. A bracket assembly is utilized to attach the heat exchanger to a structural member of a gas turbine engine assembly, e.g., a fan case, in such a manner as to maximize the surface area available for fin placement, and to not interfere with the cooling circuits within the manifold. The mounting system provides adequate stiffness for high cycle fatigue loads (i.e., vibrations) and allows relative slippage between the heat exchanger and the fan case to accommodate thermal expansion and contraction to address low cycle fatigue loads.
    Type: Application
    Filed: June 30, 2010
    Publication date: June 23, 2011
    Inventors: John Hand, Bernard A. Luschek, Lonnie R. Stewart, Michael J. Gilloon, Walter A. Hundley, JR., Jerry W. Myers, Dennis A. McQueen, Michael Peoples
  • Publication number: 20110146051
    Abstract: A method of assembling a heat exchanger in a gas turbine engine assembly is provided. The method includes providing a structural body including a wall having an elongated slot, providing a heat exchanger operably associated with a bracket, and providing a slip joint for coupling the bracket to the structural body. The slip joint includes a standoff, an elongated member, and a biasing member disposed about the elongated member. The standoff is inserted through the wall so that the biasing member imparts a predetermined biasing force between the bracket and the structural body. The slip joint allows relative sliding movement between the bracket and the structural body when a sliding force due to thermal expansion or contraction is greater than the biasing force.
    Type: Application
    Filed: June 30, 2010
    Publication date: June 23, 2011
    Inventors: John Hand, Bernard A. Luschek, Lonnie R. Stewart, Michael J. Gilloon, Walter A. Hundley, JR., Jerry W. Myers, Dennis A. McQueen, Michael Peoples