Patents by Inventor Catalin T. Vrinceanu

Catalin T. Vrinceanu 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: 10508669
    Abstract: A method and apparatus for reworking a composite structure. A fastener is cooled from a first temperature to a second temperature at which a diameter of a post of the fastener is reduced by a desired amount. The post of the fastener is placed into a channel in a bushing such that a desired interference fit occurs when the fastener is at the first temperature. The bushing with the fastener is positioned in a hole in the composite structure. A gap is present between an outer surface of the bushing and an inner surface of the hole. A gap is also present between an end of the bushing and a second structure.
    Type: Grant
    Filed: November 21, 2016
    Date of Patent: December 17, 2019
    Assignee: The Boeing Company
    Inventors: David Jonathan Gordon, Catalin T. Vrinceanu
  • Publication number: 20170074302
    Abstract: A method and apparatus for reworking a composite structure. A fastener is cooled from a first temperature to a second temperature at which a diameter of a post of the fastener is reduced by a desired amount. The post of the fastener is placed into a channel in a bushing such that a desired interference fit occurs when the fastener is at the first temperature. The bushing with the fastener is positioned in a hole in the composite structure. A gap is present between an outer surface of the bushing and an inner surface of the hole. A gap is also present between an end of the bushing and a second structure.
    Type: Application
    Filed: November 21, 2016
    Publication date: March 16, 2017
    Inventors: David Jonathan Gordon, Catalin T. Vrinceanu
  • Patent number: 9498855
    Abstract: A method and apparatus for reworking a composite structure. A fastener is cooled from a first temperature to a second temperature at which a diameter of a post of the fastener is reduced by a desired amount. The post of the fastener is placed into a channel in a bushing such that a desired interference fit occurs when the fastener is at the first temperature. The bushing with the fastener is positioned in a hole in the composite structure. A gap is present between an outer surface of the bushing and an inner surface of the hole. A gap is also present between an end of the bushing and a second structure.
    Type: Grant
    Filed: April 2, 2014
    Date of Patent: November 22, 2016
    Assignee: THE BOEING COMPANY
    Inventors: David Jonathan Gordon, Catalin T. Vrinceanu
  • Publication number: 20150283655
    Abstract: A method and apparatus for reworking a composite structure. A fastener is cooled from a first temperature to a second temperature at which a diameter of a post of the fastener is reduced by a desired amount. The post of the fastener is placed into a channel in a bushing such that a desired interference fit occurs when the fastener is at the first temperature. The bushing with the fastener is positioned in a hole in the composite structure. A gap is present between an outer surface of the bushing and an inner surface of the hole. A gap is also present between an end of the bushing and a second structure.
    Type: Application
    Filed: April 2, 2014
    Publication date: October 8, 2015
    Applicant: The Boeing Company
    Inventors: David Jonathan Gordon, Catalin T. Vrinceanu