Patents by Inventor Antonio Rufin

Antonio Rufin 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: 8555481
    Abstract: According to a preferred embodiment, a multi-piece fastener with self-indexing nut is disclosed. The multi-piece fastener is designed for use in low clearance areas such as aircraft wing side-of-body joint locations. The multi-piece fastener comprises a stud comprising an elongated part extending between a first end face and a second end face, a threaded head fastener, a threaded tail fastener, and a wrenching feature. A self-indexing feature is provided on the stud and head fastener which allows automatic orientation of the head fastener with respect to the stud.
    Type: Grant
    Filed: March 5, 2012
    Date of Patent: October 15, 2013
    Assignee: The Boeing Company
    Inventors: John R. Porter, Antonio Rufin
  • Publication number: 20120144653
    Abstract: According to a preferred embodiment, a multi-piece fastener with self-indexing nut is disclosed. The multi-piece fastener is designed for use in low clearance areas such as aircraft wing side-of-body joint locations. The multi-piece fastener comprises a stud comprising an elongated part extending between a first end face and a second end face, a threaded head fastener, a threaded tail fastener, and a wrenching feature. A self-indexing feature is provided on the stud and head fastener which allows automatic orientation of the head fastener with respect to the stud.
    Type: Application
    Filed: March 5, 2012
    Publication date: June 14, 2012
    Applicant: The Boeing Company
    Inventors: John R. Porter, Antonio Rufin
  • Publication number: 20090136294
    Abstract: According to a preferred embodiment, a multi-piece fastener with self-indexing nut is disclosed. The multi-piece fastener is designed for use in low clearance areas such as aircraft wing side-of-body joint locations. The multi-piece fastener comprises a stud comprising an elongated part extending between a first end face and a second end face, a threaded head fastener, a threaded tail fastener, and a wrenching feature. A self-indexing feature is provided on the stud and head fastener which allows automatic orientation of the head fastener with respect to the stud.
    Type: Application
    Filed: January 26, 2009
    Publication date: May 28, 2009
    Applicant: THE BOEING COMPANY
    Inventors: John R. Porter, Antonio Rufin
  • Publication number: 20060075827
    Abstract: The minimum tensile elongation specification of a manufactured part, such as metal castings, forgings and premium mill products, is verified in-situ using a simple, inexpensive, nondestructive apparatus and method in which a through-hole is formed in the part to be tested. A disposable mandrel having a diameter adapted to expand the hole to the minimum elongation required in the part's specification is pressed into the hole. The presence of radial cracks in the part adjacent to the hole after the mandrel has been pressed in indicates that the part does not meet the specification, and the absence of such cracks indicates that it does. Since the test is performed on the part itself, the cost of the manufacture and testing of tensile test coupons is eliminated, and different areas of the part may be sampled easily, thereby enabling a closer, more thorough evaluation of part's material bulk properties.
    Type: Application
    Filed: October 7, 2004
    Publication date: April 13, 2006
    Inventor: Antonio Rufin