Patents by Inventor Aaron C. Caba

Aaron C. Caba 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).

  • CTE compensation for wafer-level and chip-scale packages and assemblies
    Patent number: 10847469
    Abstract: A microelectronic structure having CTE compensation for use in wafer-level and chip-scale packages, comprising a plurality of substrate tiles each having a generally planar upper surface, the upper surfaces of the tiles disposed within a common plane to provide a generally planar grid of the tiles, each respective pair of adjacent tiles having a gap disposed therebetween.
    Type: Grant
    Filed: July 17, 2017
    Date of Patent: November 24, 2020
    Assignee: CUBIC CORPORATION
    Inventors: Kenneth J. Vanhille, Aaron C. Caba, Masud Beroz, Jared W. Jordan, Timothy A. Smith, Anatoliy O. Boryssenko, Steven E. Huettner
  • CTE COMPENSATION FOR WAFER-LEVEL AND CHIP-SCALE PACKAGES AND ASSEMBLIES
    Publication number: 20170330836
    Abstract: CTE compensation for wafer-level and chip-scale packages and assemblies.
    Type: Application
    Filed: July 17, 2017
    Publication date: November 16, 2017
    Inventors: Kenneth J. Vanhille, Aaron C. Caba, Masud Beroz, Jared W. Jordan, Timothy A. Smith, Anatoliy O. Boryssenko, Steven E. Huettner
  • Rocket nozzle assembly
    Patent number: 8952304
    Abstract: In one example, a rocket nozzle assembly is disclosed that has stowed and deployed positions, and includes a casing including an outer wall and an inner surface, at least a portion of the inner surface defining a diverging region, wherein the casing defines a plurality of fin slots, and wherein each of the plurality of fin slots extend through the outer wall of the casing and the inner surface of the casing, and wherein the diverging region defines a bell-shaped contour. The assembly further includes a plurality of fins pivotally engaged to the casing, wherein in the stowed position, each of the plurality of fins extends into the diverging region through a respective one of the fin slots, and wherein in the deployed position, each of the plurality of fins extend outwardly from the casing.
    Type: Grant
    Filed: July 14, 2011
    Date of Patent: February 10, 2015
    Assignee: Alliant Techsystems, Inc.
    Inventors: Joseph O. Bellotte, Thomas F. Farabaugh, Aaron C. Caba
  • ROCKET NOZZLE ASSEMBLY
    Publication number: 20140291441
    Abstract: In one example, a rocket nozzle assembly is disclosed that has stowed and deployed positions, and includes a casing including an outer wall and an inner surface, at least a portion of the inner surface defining a diverging region, wherein the casing defines a plurality of fin slots, and wherein each of the plurality of fin slots extend through the outer wall of the casing and the inner surface of the casing, and wherein the diverging region defines a bell-shaped contour. The assembly further includes a plurality of fins pivotally engaged to the casing, wherein in the stowed position, each of the plurality of fins extends into the diverging region through a respective one of the fin slots, and wherein in the deployed position, each of the plurality of fins extend outwardly from the casing.
    Type: Application
    Filed: July 14, 2011
    Publication date: October 2, 2014
    Applicant: ALLIANT TECHSYSTEMS INC.
    Inventors: Joseph O. Bellotte, Thomas F. Farabaugh, Aaron C. Caba