Patents by Inventor Jem Rongong

Jem Rongong 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: 7794210
    Abstract: A turbomachine blade comprising a root portion and an aerofoil portion, the aerofoil portion having a leading edge, a trailing edge, a concave metal wall portion extending from the leading edge to the trailing edge and a convex metal wall portion extending from the leading edge to the trailing edge, the concave metal wall portion and the convex metal wall portion forming a continuous integral metal wall, the aerofoil portion having a hollow interior defined by at least one internal surface, the hollow interior of the aerofoil portion being at least partially filled with a vibration damping material that is separated from the metal wall portions by a thermally insulating material.
    Type: Grant
    Filed: July 27, 2007
    Date of Patent: September 14, 2010
    Assignee: Rolls-Royce plc
    Inventors: Daniel Clark, Richard C Harvey, Jem A Rongong
  • Publication number: 20080025845
    Abstract: A turbomachine blade comprising a root portion and an aerofoil portion, the aerofoil portion having a leading edge, a trailing edge, a concave metal wall portion extending from the leading edge to the trailing edge and a convex metal wall portion extending from the leading edge to the trailing edge, the concave metal wall portion and the convex metal wall portion forming a continuous integral metal wall, the aerofoil portion having a hollow interior defined by at least one internal surface, the hollow interior of the aerofoil portion being at least partially filled with a vibration damping material that is separated from the metal wall portions by a thermally insulating material.
    Type: Application
    Filed: July 27, 2007
    Publication date: January 31, 2008
    Inventors: Daniel Clark, Richard C. Harvey, Jem A. Rongong
  • Patent number: 7311500
    Abstract: A turbomachine blade comprising a root portion and an aerofoil portion, the aerofoil portion having a leading edge, a trailing edge, a concave metal wall portion extending from the leading edge to the trailing edge and a convex metal wall portion extending from the leading edge to the trailing edge. The concave metal wall portion and the convex metal wall portion form a continuous integral metal wall. The aerofoil portion has a hollow interior defined by at least one internal surface and the hollow interior of the aerofoil portion is at least partially filled with a vibration damping and stiffening system that comprises a vibration damping material. The vibration damping material is bonded to the at least one internal surface and the vibration damping and stiffening system comprises a variation of material properties between the wall portions.
    Type: Grant
    Filed: July 1, 2003
    Date of Patent: December 25, 2007
    Assignee: Rolls-Royce plc
    Inventors: Jem A Rongong, Geoffrey R Tomlinson
  • Publication number: 20060180420
    Abstract: A particle vibration damper includes a container which locates a plurality of steel particles. A copper winding is provided around the container to induce a magnetic field therein to increase the inter-particle pressure. By adjusting the voltage across the winding the amplitude of peak damping ability can be varied to match the vibration amplitude being damped.
    Type: Application
    Filed: April 13, 2006
    Publication date: August 17, 2006
    Inventors: Jem Rongong, Thomas Cecil, David Webster
  • Patent number: 6688439
    Abstract: A vibration damping system (8) wherein the system (8) comprises a magnetism generating medium (12) and a magnetism energy dissipating medium (16) whereby, in use, vibration of the magnetism generating medium (12) generates a magnetic field, the magnetism generating medium (12) and the magnetism energy dissipating medium (16) being so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium (16) thereby damping the vibrations of the magnetism generating medium (12).
    Type: Grant
    Filed: August 13, 2001
    Date of Patent: February 10, 2004
    Assignee: Rolls-Royce plc
    Inventors: Bishakh Bhattacharya, Jem Rongong, Geoffrey R Tomlinson
  • Publication number: 20040018091
    Abstract: A turbomachine blade comprising a root portion and an aerofoil portion, the aerofoil portion having a leading edge, a trailing edge, a concave metal wall portion extending from the leading edge to the trailing edge and a convex metal wall portion extending from the leading edge to the trailing edge. The concave metal wall portion and the convex metal wall portion form a continuous integral metal wall. The aerofoil portion has a hollow interior defined by at least one internal surface and the hollow interior of the aerofoil portion is at least partially filled with a vibration damping and stiffening system that comprises a vibration damping material. The vibration damping material is bonded to the at least one internal surface and the vibration damping and stiffening system comprises a variation of material properties between the wall portions.
    Type: Application
    Filed: July 1, 2003
    Publication date: January 29, 2004
    Inventors: Jem A. Rongong, Geoffrey R. Tomlinson
  • Publication number: 20030213660
    Abstract: A vibration damping system 8 wherein the system 8 comprises a magnetism generating medium 12 and a magnetism energy dissipating medium 16 whereby, in use, vibration of the magnetism generating medium 12 generates a magnetic field, the magnetism generating medium 12 and the magnetism energy dissipating medium 16 being so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium 16 thereby damping the vibrations of the magnetism generating medium 12.
    Type: Application
    Filed: August 13, 2001
    Publication date: November 20, 2003
    Inventors: Bishakh Bhattacharya, Jem Rongong, Geoffrey R. Tomlinson