Patents by Inventor David Inston

David Inston 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: 9469067
    Abstract: An apparatus for fabricating a fiber reinforced thermoplastic composite structure is described. The apparatus comprises a localized heat source arranged to heat a portion of a stack of fiber reinforced thermoplastic material layers and an ultrasonic transducer arranged to locally introduce ultrasonic energy waves to the heated portion of the fiber reinforced thermoplastic material layers. The apparatus makes it possible to achieve ultrasonic consolidation of the layers occurs.
    Type: Grant
    Filed: April 29, 2014
    Date of Patent: October 18, 2016
    Assignee: AIRBUS OPERATIONS LTD
    Inventor: David Inston
  • Publication number: 20140230993
    Abstract: An apparatus for fabricating a fibre reinforced thermoplastic composite structure is described. The apparatus comprises a localised heat source arranged to heat a portion of a stack of fibre reinforced thermoplastic material layers and an ultrasonic transducer arranged to locally introduce ultrasonic energy waves to the heated portion of the fibre reinforced thermoplastic material layers. The apparatus makes it possible to achieve ultrasonic consolidation of the layers occurs.
    Type: Application
    Filed: April 29, 2014
    Publication date: August 21, 2014
    Applicant: AIRBUS OPERATIONS LTD.
    Inventor: David INSTON
  • Patent number: 8747585
    Abstract: A method of fabricating a fiber reinforced thermoplastic composite structure comprising: placing a first layer of fiber reinforced thermoplastic material on top of a second layer of fiber reinforced thermoplastic material; providing a local heating source and locally heating a portion of at least the upper layer of thermoplastic composite material; and providing an ultrasonic transducer and locally introducing ultrasonic energy waves to the heated portion of the thermoplastic material such that ultrasonic consolidation of the fiber reinforced thermoplastic occurs.
    Type: Grant
    Filed: June 22, 2009
    Date of Patent: June 10, 2014
    Assignee: Airbus Operations Ltd
    Inventor: David Inston
  • Patent number: 8420183
    Abstract: Disclosed is a method of manufacturing a composite sheet. The method comprises (a) irradiating a sheet of fibers and a matrix film at an irradiation zone with a plasma at substantially atmospheric pressure, and (b) impregnating the sheet of fibers with the matrix at an adhesion zone. The processes (a) and (b) are performed simultaneously, and the matrix film is irradiated with a plasma at said irradiation zone after being unwound from a roller and prior to entering said adhesion zone.
    Type: Grant
    Filed: August 1, 2012
    Date of Patent: April 16, 2013
    Assignee: Airbus Operations Limited
    Inventor: David Inston
  • Publication number: 20120292828
    Abstract: Disclosed is a method of manufacturing a composite sheet. The method comprises (a) irradiating a sheet of fibres and a matrix film at an irradiation zone with a plasma at substantially atmospheric pressure, and (b) impregnating the sheet of fibres with the matrix at an adhesion zone. The processes (a) and (b) are performed simultaneously, and the matrix film is irradiated with a plasma at said irradiation zone after being unwound from a roller and prior to entering said adhesion zone.
    Type: Application
    Filed: August 1, 2012
    Publication date: November 22, 2012
    Applicant: AIRBUS OPERATIONS LIMITED
    Inventor: David INSTON
  • Patent number: 8241711
    Abstract: Disclosed is a method of manufacturing a composite sheet. The method comprises (a) irradiating a sheet of fibers and a matrix film at an irradiation zone with a plasma at substantially atmospheric pressure, and (b) impregnating the sheet of fibers with the matrix at an adhesion zone. The processes (a) and (b) are performed simultaneously, and the matrix film is irradiated with a plasma at said irradiation zone after being unwound from a roller and prior to entering said adhesion zone.
    Type: Grant
    Filed: August 1, 2007
    Date of Patent: August 14, 2012
    Assignee: Airbus Operations Limited
    Inventor: David Inston
  • Publication number: 20110065888
    Abstract: A method of fabricating a fibre reinforced thermoplastic composite structure comprising: placing a first layer of fibre reinforced thermoplastic material on top of a second layer of fibre reinforced thermoplastic material; providing a local heating source and locally heating a portion of at least the upper layer of thermoplastic composite material; and providing an ultrasonic transducer and locally introducing ultrasonic energy waves to the heated portion of the thermoplastic material such that ultrasonic consolidation of the fibre reinforced thermoplastic occurs.
    Type: Application
    Filed: June 22, 2009
    Publication date: March 17, 2011
    Applicant: AIRBUS OPERATIONS LTD
    Inventor: David Inston
  • Publication number: 20090297726
    Abstract: A method of manufacturing a composite sheet, the method comprising: a. irradiating a sheet of fibres and/or a matrix at an irradiation zone with a plasma at substantially atmospheric pressure, and b. impregnating the sheet of fibres with the matrix at an adhesion zone; wherein processes a. and b. are performed simultaneously. A method of manufacturing a composite material, the method comprising: a. irradiating a matrix with a plasma, and b. coating a filler with the irradiated matrix.
    Type: Application
    Filed: August 1, 2007
    Publication date: December 3, 2009
    Applicant: AIRBUS UK LIMITED
    Inventor: David Inston