Patents by Inventor Timothy M. Davis

Timothy M. Davis 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: 20190170006
    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. A wave spring and/or a rope seal is disposed between the first and second seal sections biases the first and second seal sections away from one another.
    Type: Application
    Filed: February 1, 2019
    Publication date: June 6, 2019
    Inventors: Timothy M. Davis, Paul M. Lutjen
  • Publication number: 20190170007
    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section, a second seal section, and (in some embodiments) a third seal section. Two or three of the seal sections are uncoupled, which allows the uncoupled seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and third (or in some embodiments, the first and second) seal sections away from one another.
    Type: Application
    Filed: February 8, 2019
    Publication date: June 6, 2019
    Inventors: Timothy M. Davis, Paul M. Lutjen
  • Patent number: 10301956
    Abstract: A seal assembly extends along an axis and seals an axial (and/or radial) gap between a first component and a second component. The seal assembly includes a seal carrier and a seal element. The seal element extends axially (and/or radially) between a first portion and a second portion. The first portion of the seal element is slidingly arranged within a slot in an axial end (or a radial side) of the seal carrier. The second portion of the seal element is configured to axially (and/or radially) engage the second component.
    Type: Grant
    Filed: September 25, 2015
    Date of Patent: May 28, 2019
    Assignee: United Technologies Corporation
    Inventors: Paul M. Lutjen, Timothy M. Davis, Mark J. Rogers
  • Patent number: 10301961
    Abstract: An active clearance control system of a gas turbine engine includes a multiple of blade outer air seal assemblies and a sync ring with a multiple of graduation sets. Each of the graduation sets is associated with one of the multiple of blade outer air seal assemblies. An active clearance control system of a gas turbine engine includes a sync ring with a multiple of graduation sets. Each of the graduation sets includes a multiple of graduations to define an associated radial position for each of a respective multiple of blade outer air seal assemblies.
    Type: Grant
    Filed: July 23, 2014
    Date of Patent: May 28, 2019
    Assignee: United Technologies Corporation
    Inventors: Timothy M. Davis, Brian Duguay
  • Patent number: 10280799
    Abstract: A seal assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a seal arc segment that has a sealing portion and a first interface portion. The first interface portion defines circumferential mate faces. A support includes a mounting portion and a second interface portion. The mounting portion is configured to be fixedly attached to an engine static structure, and the second interface portion is radially inward of the first interface portion. At least one positioning member is dimensioned to abut the first and second interface portions such that the first and second interface portions are spaced apart by a predetermined distance in a radial direction.
    Type: Grant
    Filed: June 10, 2016
    Date of Patent: May 7, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventor: Timothy M. Davis
  • Patent number: 10280778
    Abstract: An assembly for a turbine engine includes a turbine engine first component, a turbine engine second component and a seal assembly. The first component includes a groove and a groove surface. The second component includes a tongue that extends into the groove to a tongue surface. The seal assembly at least partially seals a gap between the groove surface and the tongue surface. The seal assembly includes a rope seal and a clip that attaches the rope seal to the tongue. The rope seal is arranged within the groove between the groove surface and the tongue surface.
    Type: Grant
    Filed: February 24, 2014
    Date of Patent: May 7, 2019
    Assignee: United Technologies Corporation
    Inventors: Mark J. Rogers, Timothy M. Davis, Mark Broomer, Kevin W. White, Craig McGarrah, Carson A. Roy Thill
  • Patent number: 10260364
    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and second seal sections away from one another.
    Type: Grant
    Filed: March 9, 2015
    Date of Patent: April 16, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: Paul M. Lutjen, Jeremy Drake, Timothy M. Davis
  • Publication number: 20190107000
    Abstract: A seal for sealing a space defined between first and second components, the seal having: an annular member having a substantially U-shaped cross section along at least a portion thereof, the portion configured to provide a seal interface at each of the first and second components.
    Type: Application
    Filed: October 16, 2018
    Publication date: April 11, 2019
    Inventor: Timothy M. Davis
  • Patent number: 10240473
    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components.
    Type: Grant
    Filed: August 26, 2014
    Date of Patent: March 26, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventor: Timothy M. Davis
  • Publication number: 20190063248
    Abstract: A seal system may comprise a seal cavity defined, at least partially, by a first axial surface and a second axial surface. The second axial surface may be recessed with respect to the first axial surface. A brush seal may be disposed in the seal cavity. The brush seal may comprise a first bristle pack and a backing plate coupled to the first bristle pack. A first group of bristles of the first bristle pack may be radially inward of the first axial surface.
    Type: Application
    Filed: August 28, 2017
    Publication date: February 28, 2019
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Mark J. Rogers, Timothy M. Davis
  • Patent number: 10208613
    Abstract: The present disclosure relates generally to a seal between two circumferential components. The seal comprises a plurality of seal segments disposed adjacent one another by a retaining ring that is at least partially disposed within a cavity formed within each of the plurality of seal segments.
    Type: Grant
    Filed: August 19, 2015
    Date of Patent: February 19, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: Timothy M Davis, Mark J. Rogers
  • Patent number: 10202863
    Abstract: An annular ring for sealing a flow includes an inner ring and a tab. The tab extends radially and is configured to restrict axial movement of the seal.
    Type: Grant
    Filed: May 23, 2016
    Date of Patent: February 12, 2019
    Assignee: United Technologies Corporation
    Inventors: Timothy M. Davis, Mark F. Zelesky, Michael G. McCaffrey
  • Patent number: 10202862
    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section, a second seal section, and (in some embodiments) a third seal section. Two or three of the seal sections are uncoupled, which allows the uncoupled seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and third (or in some embodiments, the first and second) seal sections away from one another.
    Type: Grant
    Filed: April 8, 2015
    Date of Patent: February 12, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: Timothy M. Davis, Paul M. Lutjen
  • Patent number: 10196912
    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. A wave spring and/or a rope seal is disposed between the first and second seal sections biases the first and second seal sections away from one another.
    Type: Grant
    Filed: August 20, 2015
    Date of Patent: February 5, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: Timothy M Davis, Paul M Lutjen
  • Publication number: 20190032786
    Abstract: A brush seal includes a bristle pack disposed between a top plate and a back plate. A sliding backing plate is disposed between the bristle pack and the back plate. The bristle pack includes a first bristle set that extends across a seal gap between a first engine component and a second engine component to prevent leakage across the seal gap and a second bristle set that exerts a force on the sliding backing plate. The sliding backing plate supports at least a portion of the first bristles and extends across the seal cavity to contact the second component. The force exerted on the sliding backing plate drives the sliding backing plate into contact with the second component.
    Type: Application
    Filed: July 31, 2017
    Publication date: January 31, 2019
    Inventors: Timothy M. Davis, Jose R. Paulino, Mark J. Rogers
  • Publication number: 20190024801
    Abstract: A seal structure may comprise a cavity defined at least partially by an axial surface and a radial surface. A brush seal may be disposed in the cavity. The brush seal may comprise a bristle pack and a backing plate coupled to the bristle pack. A first surface of the backing plate may contact the axial surface, and a second surface of the backing plate may contact the radial surface.
    Type: Application
    Filed: July 19, 2017
    Publication date: January 24, 2019
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Timothy M. Davis, Mark J. Rogers, Jeffrey M. Wittman, James R. Plante
  • Patent number: 10167957
    Abstract: A metal gasket bellows seal includes a first ply comprised of a first material having a first yield strength. The metal gasket bellows seal also includes a second ply positioned adjacent to the first ply and comprised of a second material having a second yield strength that is less than the first yield strength.
    Type: Grant
    Filed: May 31, 2016
    Date of Patent: January 1, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: Timothy M. Davis, Terence P. Tyler, Jr., Jose R. Paulino, Paul M. Lutjen
  • Patent number: 10167730
    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section including one or more first slots formed therein, a second seal section including one or more second slots formed therein and one or more frustoconical rings disposed in respective ones of the slots, such that the first and second seal sections and the frustoconical rings move relative to one another during relative movement between the two components. A wave spring disposed between the first and second seal sections biases the first and second seal sections away from one another.
    Type: Grant
    Filed: August 20, 2015
    Date of Patent: January 1, 2019
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: Timothy M. Davis, Paul M. Lutjen, Mark J. Rogers
  • Patent number: 10145308
    Abstract: A seal assembly for a gas turbine engine includes an engine static structure. First and second members fluidly separate cavities from one another. A seal assembly is captured by the engine structure. The seal assembly includes a carrier and a seal that engages the first member. The second member is captured by the carrier.
    Type: Grant
    Filed: February 2, 2015
    Date of Patent: December 4, 2018
    Assignee: United Technologies Corporation
    Inventors: Carson A. Roy Thill, Mark Broomer, Timothy M. Davis, Craig R. McGarrah, Mark J. Rogers, Russell E. Keene, Anthony B. Swift
  • Patent number: 10113437
    Abstract: The present disclosure relates generally to a seal between two components. The seal includes a plurality of seal sections including convolutions therein that are inter-engaged with one another to form flexible and resilient seals.
    Type: Grant
    Filed: August 19, 2015
    Date of Patent: October 30, 2018
    Assignee: UNITED TECHNOLOGIES CORPORATION
    Inventors: Timothy M Davis, Michael S Stevens