Patents by Inventor Jeremy Banik

Jeremy Banik 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: 10236590
    Abstract: A foldable segmented structure includes a substantially center portion and a plurality of strut assemblies radially disposed around the center portion. Each strut assembly includes an inner and outer strut. The inner strut includes a first end portion rotatably coupled at the center portion and a second end portion rotatably coupled to the outer strut at an intermediate portion of the strut assembly. The intermediate portion is spaced apart from the center portion. At least one shell segment is disposed on at least one of the inner and outer strut. Each inner strut is configured to rotatably articulate about the first end portion in a first angular direction. Each outer strut is configured to rotatably articulate about the second end portion in a second angular direction opposite to the first angular direction to form an axially extending structure from the center portion to the intermediate portion in a stowed configuration.
    Type: Grant
    Filed: December 21, 2016
    Date of Patent: March 19, 2019
    Assignee: The United States of America, as Represented by the Secretary of the Air Force
    Inventors: Joseph N. Footdale, Jeremy Banik, Jeremiah Sanders
  • Patent number: 10119266
    Abstract: A sparse-isogrid columnar lattice structure including rigid ring frames connected by a mirrored symmetric double helix pattern comprised of first shell hinge elements in a first helical pattern and second shell hinge elements in a second helical pattern oriented in an opposite direction to the first helical pattern and congruent thereto. The helical axes of the first and second helical patterns intersect the respective centers of the ring frames. The first and second shell hinge elements are configured to stow in a stored energy state when the ring frames are collapsed toward one another along the helical axis, and the first and second shell hinge elements are configured to release the stored energy to deploy to a restored state and extend the ring frames apart from each other along the helical axis when deployed to form a stable rigid axial column in a restored state.
    Type: Grant
    Filed: December 22, 2016
    Date of Patent: November 6, 2018
    Assignee: The Government of the United States of America as Represented by the Secretary of the Air Force
    Inventors: Sungeun K. Jeon, Jeremy Banik, Michael Peterson
  • Patent number: 7895795
    Abstract: An elastic space-deployable boom of carbon fiber reinforced plastic or other resilient material having an open substantially triangular cross-section when deployed and stowed with a flattened cross-section about a circular hub.
    Type: Grant
    Filed: October 22, 2007
    Date of Patent: March 1, 2011
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Thomas W. Murphey, Jeremy Banik