Patents by Inventor Martin Flannery

Martin Flannery 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: 20160230274
    Abstract: A multilayer coating for a metallic surface of a component is provided. The multilayer coating includes a first coating having a metal nitride. The first coating at least partially overlaps the metallic surface. The multilayer coating also includes a second coating having a metal. The second coating at least partially overlaps the first coating. The multilayer coating further includes a third coating having a Diamond Like Carbon (DLC) material. The third coating at least partially overlaps the second coating. The first coating, the second coating, and the third coating differ from one another with respect to at least one of hardness, elasticity, corrosion resistance, and lubricity. The multilayer coating includes at least ten overlapping layers having successive layers of the first coating, the second coating, and the third coating in repeating sequence.
    Type: Application
    Filed: April 19, 2016
    Publication date: August 11, 2016
    Applicant: Caterpillar Inc.
    Inventors: Colm Martin Flannery, Steven Charles Taylor, Bao Feng, Lucy Victoria Berg, Joseph Ryan Sullivan
  • Patent number: 7270304
    Abstract: A positioning boom disposed between a space-based observatory platform and its instrument payload provides thermal and dynamic isolation as well as fine pointing and momentum control. The inventive system isolates a sensitive payload from a warm, dynamically noisy spacecraft, which includes a sunshield. Isolation is required in terms of dynamics and heat flow, both in terms of the absolute level and its variance (thermal isolation). The present invention provides intrinsic control over momentum buildup (which is due to the separation of the center of pressure from the center of mass). The space-based platform also provides a view (field of regard) to at least half the sky (in the anti-sun direction).
    Type: Grant
    Filed: October 13, 2004
    Date of Patent: September 18, 2007
    Assignee: Northrop Grumman Corporation
    Inventors: Dean R. Dailey, Charles F. Lillie, Martin Flannery, Jonathan W. Arenberg, Allen J. Bronowicki
  • Publication number: 20060076459
    Abstract: A positioning boom disposed between a space-based observatory platform and its instrument payload provides thermal and dynamic isolation as well as fine pointing and momentum control. The inventive system isolates a sensitive payload from a warm, dynamically noisy spacecraft, which includes a sunshield. Isolation is required in terms of dynamics and heat flow, both in terms of the absolute level and its variance (thermal isolation). The present invention provides intrinsic control over momentum buildup (which is due to the separation of the center of pressure from the center of mass). The space-based platform also provides a view (field of regard) to at least half the sky (in the anti-sun direction).
    Type: Application
    Filed: October 13, 2004
    Publication date: April 13, 2006
    Inventors: Dean Dailey, Charles Lillie, Martin Flannery, Jonathan Arenberg, Allen Bronowicki