Patents by Inventor Julian B. Santiago Prowald

Julian B. Santiago Prowald 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: 9660351
    Abstract: A multi-faceted deployable antenna frame including a six-bar linkage structure in a lateral facet of the antenna frame, the six-bar linkage structure being convertible from a folded state into a deployed state and having two first bars and four second bars, each bar being coupled to two others by a hinge to form a closed loop, where in the deployed state, the six-bar linkage structure has a quadrilateral shape.
    Type: Grant
    Filed: October 1, 2012
    Date of Patent: May 23, 2017
    Assignee: European Space Agency
    Inventors: Elguja Medzmariashvili, Nodar Tsignadze, Nikoloz Medzmariashvili, Leri Datashvili, Alexander Ihle, Julian B. Santiago Prowald, Cornelis Van't Klooster
  • Publication number: 20150288072
    Abstract: A multi-faceted deployable antenna frame including a six-bar linkage structure in a lateral facet of the antenna frame, the six-bar linkage structure being convertible from a folded state into a deployed state and having two first bars and four second bars, each bar being coupled to two others by a hinge to form a closed loop, where in the deployed state, the six-bar linkage structure has a quadrilateral shape.
    Type: Application
    Filed: October 1, 2012
    Publication date: October 8, 2015
    Inventors: Elguja Medzmariashvili, Nodar Tsignadze, Nikoloz Medzmariashvili, Leri Datashvili, Alexander Ihle, Julian B. Santiago Prowald, Cornelis Van't Klooster
  • Patent number: 9153860
    Abstract: A mechanical support ring structure for supporting a deployable space reflector antenna. The mechanical support ring structure is convertible from a folded state into a deployed state and includes a ring-shaped pantograph having a plurality of circumferentially arranged pantograph sections which are deployable for converting the mechanical support ring structure from the folded state into the deployed state, and a plurality of circumferentially arranged support rods, each pantograph section being arranged between a respective pair of support rods, wherein each pantograph section includes one or more pairs of pantograph rods which intersect crosswise with each other at a respective crossing position.
    Type: Grant
    Filed: March 15, 2012
    Date of Patent: October 6, 2015
    Assignee: EUROPEAN SPACE AGENCY
    Inventors: Shota Tserodze, Nodar Tsignadze, Elguja Medzmariashvili, Leri Datashvili, Julian B. Santiago Prowald
  • Publication number: 20150060605
    Abstract: A mechanical support ring structure for supporting a deployable space reflector antenna. The mechanical support ring structure is convertible from a folded state into a deployed state and includes a ring-shaped pantograph having a plurality of circumferentially arranged pantograph sections which are deployable for converting the mechanical support ring structure from the folded state into the deployed state, and a plurality of circumferentially arranged support rods, each pantograph section being arranged between a respective pair of support rods, wherein each pantograph section includes one or more pairs of pantograph rods which intersect crosswise with each other at a respective crossing position.
    Type: Application
    Filed: March 15, 2012
    Publication date: March 5, 2015
    Applicant: EUROPEAN SPACE AGENCY
    Inventors: Shota Tserodze, Nodar Tsignadze, Elguja Medzmariashvili, Leri Datashvili, Julian B. Santiago Prowald
  • Patent number: 8839585
    Abstract: Deployable support structures include a six-bar linkage structure as a lateral facet of a truncated pyramid. The six-bar linkage structure comprises six articulated struts, each coupled to two others by a revolute joint to form a closed loop. The six-bar linkage structure is convertible from a deployed state into a folded state and vice versa. In the deployed state of one embodiment, the six-bar linkage structure forms a trapezoid with two opposing first and second parallel sides formed by two struts arranged in series and coupled by a revolute joint at the center of the parallel sides. In the folded state, the two struts of each parallel side are pivoted around the joint so that opposing end portions of the struts are located side by side. Scalable and modular deployable structures can be made for space applications as well as civil constructions such as domes, roofs, housing, tents, and bridges.
    Type: Grant
    Filed: November 19, 2010
    Date of Patent: September 23, 2014
    Assignee: European Space Agency
    Inventors: Julian B. Santiago Prowald, Miguel Such Taboada
  • Publication number: 20130340373
    Abstract: Deployable support structures include a six-bar linkage structure as a lateral facet of a truncated pyramid. The six-bar linkage structure comprises six articulated struts, each coupled to two others by a revolute joint to form a closed loop. The six-bar linkage structure is convertible from a deployed state into a folded state and vice versa. In the deployed state of one embodiment, the six-bar linkage structure forms a trapezoid with two opposing first and second parallel sides formed by two struts arranged in series and coupled by a revolute joint at the center of the parallel sides. In the folded state, the two struts of each parallel side are pivoted around the joint so that opposing end portions of the struts are located side by side. Scalable and modular deployable structures can be made for space applications as well as civil constructions such as domes, roofs, housing, tents, and bridges.
    Type: Application
    Filed: November 19, 2010
    Publication date: December 26, 2013
    Inventors: Julian B. Santiago Prowald, Miguel Such Taboada