Patents by Inventor Dan Gustafsson

Dan Gustafsson 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: 11356429
    Abstract: There is provided a method and system for securely coupling and transferring data between devices. In a preferred embodiment, the devices may comprise two devices, a transferring device and a receiving device, and both devices are mobile devices. Embodiments of the present invention allow the wireless transfer of data such as contacts, photo images, video files, or other data from one device to another device, without need for special hardware or cabling.
    Type: Grant
    Filed: July 23, 2014
    Date of Patent: June 7, 2022
    Assignee: BLANCCO TECHNOLOGY GROUP IP OY
    Inventors: William Fitzgerald, Dan Gustafsson, Donal O'Shaughnessy, Peter Bermingham
  • Patent number: 9822652
    Abstract: A supporting structure for a gas turbine engine comprises an inner ring, an outer ring, and a plurality of circumferentially spaced, load carrying radial elements connecting the inner and outer rings, said radial elements being configured to transfer loads between the inner ring and the outer ring, wherein a gas channel for a primary axial gas flow is defined between the inner and outer rings, wherein the supporting structure has an inlet side for primary gas flow entrance and an outlet side for primary gas outflow, wherein the radial elements have an airfoil shape with a leading edge directed towards the inlet side, a trailing edge directed towards the outlet side, and two opposite sides connecting the leading edge and the trailing edge, and wherein at least a first of said radial elements is connected to an adjacent part of the supporting structure via a weld joint that extends across the leading edge and circumferentially at least partly around the first radial element.
    Type: Grant
    Filed: July 3, 2012
    Date of Patent: November 21, 2017
    Assignee: GKN Aerospace Sweden AB
    Inventors: Roger Sjoqvist, Hakan Jakobsson, Dan Gustafsson
  • Publication number: 20150176420
    Abstract: A supporting structure for a gas turbine engine comprises an inner ring, an outer ring, and a plurality of circumferentially spaced, load carrying radial elements connecting the inner and outer rings, said radial elements being configured to transfer loads between the inner ring and the outer ring, wherein a gas channel for a primary axial gas flow is defined between the inner and outer rings, wherein the supporting structure has an inlet side for primary gas flow entrance and an outlet side for primary gas outflow, wherein the radial elements have an airfoil shape with a leading edge directed towards the inlet side, a trailing edge directed towards the outlet side, and two opposite sides connecting the leading edge and the trailing edge, and wherein at least a first of said radial elements is connected to an adjacent part of the supporting structure via a weld joint that extends across the leading edge and circumferentially at least partly around the first radial element
    Type: Application
    Filed: July 3, 2012
    Publication date: June 25, 2015
    Inventors: Roger Sjoqvist, Hakan Jakobsson, Dan Gustafsson
  • Publication number: 20150082410
    Abstract: There is provided a method and system for securely coupling and transferring data between devices. In a preferred embodiment, the devices may comprise two devices, a transferring device and a receiving device, and both devices are mobile devices. Embodiments of the present invention allow the wireless transfer of data such as contacts, photo images, video files, or other data from one device to another device, without need for special hardware or cabling.
    Type: Application
    Filed: July 23, 2014
    Publication date: March 19, 2015
    Applicant: YOUGETITBACK LIMITED
    Inventors: William Fitzgerald, Dan Gustafsson, Donal O'Shaughnessy, Peter Bermingham
  • Publication number: 20110262277
    Abstract: A gas turbine composite workpiece, such as a workpiece forming a part of a gas turbine casing, is provided. The workpiece includes at least two components joined by at least one weld seam. In order to reduce thermal stresses of the workpiece during operation, the weld seam is interrupted by at least one aperture. In order to reduce the exchange of gases between the workpiece's sides, the workpiece may be equipped with an arrangement for preventing gas flow through the aperture.
    Type: Application
    Filed: December 18, 2008
    Publication date: October 27, 2011
    Applicant: VOLVO AERO CORPORATION
    Inventors: Roger Sjöqvist, Dan Gustafsson, Hasse Lindell