Patents by Inventor Bruce Gordy

Bruce Gordy 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: 10746246
    Abstract: A preform for a carbon-carbon composite including a plurality of fibrous layers stacked and needled-punched together to form the preform in the shape of an annulus having an inner radial section and an outer radial section. Each fibrous layer includes a respective plurality of fabric segments comprising at least one of carbon fibers or carbon-precursor fibers. At least one fibrous layer includes a first fabric segment forming at least a portion the inner radial section, the first fabric segment defining a first segment bisector and a first fiber orientation angle, and a second fabric segment forming at least a portion the outer radial section, the second fabric segment defining a second segment bisector and a second fiber orientation angle, where the first and second segment bisectors are radially aligned and the first fiber orientation angle is different than the second fiber orientation angle.
    Type: Grant
    Filed: August 27, 2018
    Date of Patent: August 18, 2020
    Assignee: Honeywell International Inc.
    Inventors: Slawomir T. Fryska, Bruce Gordy
  • Publication number: 20200061964
    Abstract: A preform for a carbon-carbon composite including a plurality of fibrous layers stacked and needled-punched together to form the preform in the shape of an annulus having an inner radial section and an outer radial section. Each fibrous layer includes a respective plurality of fabric segments comprising at least one of carbon fibers or carbon-precursor fibers. At least one fibrous layer includes a first fabric segment forming at least a portion the inner radial section, the first fabric segment defining a first segment bisector and a first fiber orientation angle, and a second fabric segment forming at least a portion the outer radial section, the second fabric segment defining a second segment bisector and a second fiber orientation angle, where the first and second segment bisectors are radially aligned and the first fiber orientation angle is different than the second fiber orientation angle.
    Type: Application
    Filed: August 27, 2018
    Publication date: February 27, 2020
    Inventors: Slawomir T. Fryska, Bruce Gordy
  • Publication number: 20200063812
    Abstract: A preform for a carbon-carbon composite including a plurality of fibrous layers superposed and needled-punched together. Each fibrous layer of the plurality of fibrous layers includes web fibers and tow fibers that each include at least one of carbon fibers or carbon-precursor fibers. The plurality of fibrous layers includes a first, a second, and a third fibrous layer, the third fibrous layer positioned between the first and the second fibrous layers. The third fibrous layer includes at least one of a ratio of web fibers to tow fibers that is less than a ratio of web fibers to tow fibers of the first fibrous layer, an areal weight that is greater than an areal weight of the first fibrous layer, or a pre-needled thickness that is greater than a pre-needled thickness the first fibrous layer.
    Type: Application
    Filed: August 27, 2018
    Publication date: February 27, 2020
    Inventors: Slawomir T. Fryska, Bruce Gordy