Patents by Inventor Brian J. Humke

Brian J. Humke 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: 6138896
    Abstract: First and second superalloy workpieces are inertia welded together by rotating the first workpiece to an initial contact speed greater than about 750 surface feet per minute, and frictionally engaging under a weld load the first and second workpieces to effect an inertia weld therebetween.
    Type: Grant
    Filed: October 5, 1998
    Date of Patent: October 31, 2000
    Assignee: General Electric Company
    Inventors: Adrian M. Ablett, Charles W. Carrier, Brian J. Humke, Steven A. Strang
  • Patent number: 5486086
    Abstract: A blade containment system is disclosed which includes an annular casing positioned radially outward of the blades and in surrounding relationship therewith, the annular casing including a plurality of ribs on the outer radial surface thereof, wherein the ribs limit the propagation of cracks and holes formed in the annular casing.
    Type: Grant
    Filed: January 4, 1994
    Date of Patent: January 23, 1996
    Assignee: General Electric Company
    Inventors: Donald L. Bellia, Christopher C. Glynn, Brian J. Humke
  • Patent number: 5431532
    Abstract: A blade containment system is disclosed which includes an annular casing positioned radially outward of the blades and in surrounding relationship therewith, the annular casing including a plurality of composite tapes bonded to the outer or inner radial surfaces thereof, wherein the composite tapes limit the propagation of cracks and holes formed in the annular casing.
    Type: Grant
    Filed: May 20, 1994
    Date of Patent: July 11, 1995
    Assignee: General Electric Company
    Inventors: Brian J. Humke, Robert P. Czachor, Donald L. Bellia, Eric E. Baehre, Christopher C. Glynn
  • Patent number: 5165850
    Abstract: A compressor discharge flowpath for a gas turbine engine includes flowpath outer and inner walls joined to a plurality of circumferentially spaced flowpath dividers extending therebetween. An inner support extends from the inner wall and is joined to a turbine nozzle, and an outer support extends from the outer wall and is joined to an engine casing. The outer support preferably includes a plurality of circumferentially spaced beams being sized and configured for carrying both axial force and torque transmitted therethrough from the turbine nozzle to the casing while allowing the beams to bend radially for accommodating differential thermal movement between the casing and the outer wall.
    Type: Grant
    Filed: July 15, 1991
    Date of Patent: November 24, 1992
    Assignee: General Electric Company
    Inventors: Brian J. Humke, Donald L. Bellia, Eric E. Baehre, Michael L. Barron, Thomas G. Wakeman