Patents by Inventor Lee WAGSTAFF

Lee WAGSTAFF 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: 9533386
    Abstract: A method of removing a metal sleeve from a bore formed in one or more elements is disclosed. The sleeve may be a cold-expanded sleeve secured within the bore by an interference fit. The method includes removing material from the internal surface of the sleeve by a cutter along a line to a depth less than the thickness of the sleeve, and subsequently urging the sleeve from the bore.
    Type: Grant
    Filed: September 13, 2012
    Date of Patent: January 3, 2017
    Assignee: AIRBUS OPERATIONS LIMITED
    Inventors: Lee Wagstaff, Lee Bradbury, Gareth Towlson
  • Patent number: 9457458
    Abstract: The present invention provides a method for removing a fastener from a component, the fastener comprising an end portion exposed from the component, the end portion having a threaded section, the method comprising the following steps; providing a cap with a threaded opening, screwing the threaded opening of the cap onto the threaded section of the exposed end portion of the fastener, and securing a percussive tool to the cap, such that repeated impacts from the percussive tool are directed onto the exposed end portion of the fastener. The present invention also provides a cap for use in removing a fastener from a component, the cap comprising a threaded opening for screwing onto a threaded section of an exposed end portion of the fastener, and an attachment portion for securing a percussive tool to the cap.
    Type: Grant
    Filed: June 11, 2013
    Date of Patent: October 4, 2016
    Assignee: AIRBUS OPERATIONS LIMITED
    Inventors: Lee Wagstaff, Philip Lee Bradbury, Gareth Towlson
  • Patent number: 9335144
    Abstract: A plastic hand-held measuring device, can measure the depth of a hole or bore or the length of a fixing, having particular application with composite aircraft components. A hook or tang, at the end of an elongate portion, can engage with the far end of the bore allowing the depth ascertained from a first measurement scale. A first formation can engage with a fixing, allowing measurement of the length of the fixing from a second measurement scale. A plastic slide can abut against a portion of the component to be measured and indicate the distance on the measurement scale that corresponds to the length of the dimension being measured. The slide may be arranged to engage with successive indexed formations along the length of the device, so that it is inclined to remain in a position corresponding to an indexed formation.
    Type: Grant
    Filed: December 6, 2012
    Date of Patent: May 10, 2016
    Assignee: AIRBUS OPERATIONS LIMITED
    Inventors: Lee Wagstaff, Philip Lee Bradbury, Gareth Towlson
  • Publication number: 20130327189
    Abstract: The present invention provides a method for removing a fastener from a component, the fastener comprising an end portion exposed from the component, the end portion having a threaded section, the method comprising the following steps; providing a cap with a threaded opening, screwing the threaded opening of the cap onto the threaded section of the exposed end portion of the fastener, and securing a percussive tool to the cap, such that repeated impacts from the percussive tool are directed onto the exposed end portion of the fastener. The present invention also provides a cap for use in removing a fastener from a component, the cap comprising a threaded opening for screwing onto a threaded section of an exposed end portion of the fastener, and an attachment portion for securing a percussive tool to the cap.
    Type: Application
    Filed: June 11, 2013
    Publication date: December 12, 2013
    Inventors: Lee WAGSTAFF, Philip Lee BRADBURY, Gareth TOWLSON
  • Publication number: 20130067746
    Abstract: A method of removing a metal sleeve from a bore formed in one or more elements is disclosed. The sleeve may be a cold-expanded sleeve secured within the bore by means of an interference fit. The method includes removing material from the internal surface of the sleeve by means of cutting along a line to a depth less than the thickness of the sleeve, and subsequently urging the sleeve from the bore.
    Type: Application
    Filed: September 13, 2012
    Publication date: March 21, 2013
    Applicant: AIRBUS OPERATIONS LIMITED
    Inventors: Lee WAGSTAFF, Lee BRADBURY, Gareth TOWLSON
  • Patent number: D687732
    Type: Grant
    Filed: June 11, 2012
    Date of Patent: August 13, 2013
    Assignee: Airbus Operations Limited
    Inventors: Lee Wagstaff, Lee Bradbury, Gareth Towlson
  • Patent number: D688147
    Type: Grant
    Filed: June 11, 2012
    Date of Patent: August 20, 2013
    Assignee: Airbus Operations Limited
    Inventors: Lee Wagstaff, Lee Bradbury, Gareth Towlson