Patents by Inventor Jordan CARON

Jordan CARON 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: 11631146
    Abstract: In an example method, a communications platform generates a plurality of logical structures. The communication platform receives, from a first user, first content to be shared within a first logical structure of the plurality of logical structures. The communications platform determines one or more second users associated with the first logical structure, and transmits contents of the first logical structure including the first content to the one or more second users.
    Type: Grant
    Filed: November 13, 2020
    Date of Patent: April 18, 2023
    Assignee: Geneva Technologies, Inc.
    Inventors: Justin Hauser, Jordan Caron, David Lee, Daniel Cushing, Samuel Liebeskind, Matthew Handler, Austin Yu
  • Publication number: 20210217106
    Abstract: In an example method, a communications platform generates a plurality of logical structures. The communication platform receives, from a first user, first content to be shared within a first logical structure of the plurality of logical structures. The communications platform determines one or more second users associated with the first logical structure, and transmits contents of the first logical structure including the first content to the one or more second users.
    Type: Application
    Filed: November 13, 2020
    Publication date: July 15, 2021
    Inventors: Justin Hauser, Jordan Caron, David Lee, Daniel Cushing, Samuel Liebeskind, Matthew Handler, Austin Yu
  • Patent number: 10378385
    Abstract: A turbine ring assembly includes ring sectors made of ceramic matrix composite material forming a turbine ring, and a ring support structure having first and second annular flanges, each ring sector having tabs. The first tab includes an annular groove in which there is received an annular projection of the first flange. The second tab of each ring sector is connected to the ring support structure by a resilient retention element. The second tab includes an opening in which there is received a portion of a retention element secured to the second annular flange of the ring support structure. The retention element is made of a material having a coefficient of thermal expansion that is greater than the coefficient of thermal expansion of the ceramic matrix composite material of the ring sectors.
    Type: Grant
    Filed: December 12, 2016
    Date of Patent: August 13, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Thierry Tesson, Maxime Carlin, Jordan Caron
  • Publication number: 20180363506
    Abstract: A turbine ring assembly includes ring sectors made of ceramic matrix composite material forming a turbine ring, and a ring support structure having first and second annular flanges, each ring sector having tabs. The first tab includes an annular groove in which there is received an annular projection of the first flange. The second tab of each ring sector is connected to the ring support structure by a resilient retention element. The second tab includes an opening in which there is received a portion of a retention element secured to the second annular flange of the ring support structure. The retention element is made of a material having a coefficient of thermal expansion that is greater than the coefficient of thermal expansion of the ceramic matrix composite material of the ring sectors.
    Type: Application
    Filed: December 12, 2016
    Publication date: December 20, 2018
    Inventors: Thierry TESSON, Maxime CARLIN, Jordan CARON