Patents by Inventor Bradley J. Burie

Bradley J. Burie 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: 8733110
    Abstract: A method and system for an integrated ejector valve assembly is provided. The integrated ejector valve assembly includes a first valve assembly configured to control a flow of relatively lower pressure fluid from a first inlet port, a second valve assembly configured to control a flow of relatively higher pressure fluid from a second inlet port, a first actuation chamber configured to close the first valve assembly, a second actuation chamber configured to close the second valve assembly, and a third actuation chamber configured to open the second valve assembly.
    Type: Grant
    Filed: August 14, 2012
    Date of Patent: May 27, 2014
    Assignee: GE Aviation Systems, LLC
    Inventors: Kent Weber, Athanasios Kyriazopoulos, Peter C. Hightower, Bradley J. Burie
  • Publication number: 20120304663
    Abstract: A method and system for an integrated ejector valve assembly is provided. The integrated ejector valve assembly includes a first valve assembly configured to control a flow of relatively lower pressure fluid from a first inlet port, a second valve assembly configured to control a flow of relatively higher pressure fluid from a second inlet port, a first actuation chamber configured to close the first valve assembly, a second actuation chamber configured to close the second valve assembly, and a third actuation chamber configured to open the second valve assembly.
    Type: Application
    Filed: August 14, 2012
    Publication date: December 6, 2012
    Inventors: Kent Weber, Athanasios Kyriazopoulos, Peter C. Hightower, Bradley J. Burie
  • Patent number: 8267122
    Abstract: A method and system for an integrated ejector valve assembly is provided. The integrated ejector valve assembly includes a first valve assembly configured to control a flow of relatively lower pressure fluid from a first inlet port, a second valve assembly configured to control a flow of relatively higher pressure fluid from a second inlet port, a first actuation chamber configured to close the first valve assembly, a second actuation chamber configured to close the second valve assembly, and a third actuation chamber configured to open the second valve assembly.
    Type: Grant
    Filed: June 30, 2009
    Date of Patent: September 18, 2012
    Assignee: GE Aviation Systems LLC
    Inventors: Kent Weber, Athanasios Kyriazopoulos, Peter C. Hightower, Bradley J. Burie
  • Publication number: 20100326089
    Abstract: A method and system for an integrated ejector valve assembly is provided. The integrated ejector valve assembly includes a first valve assembly configured to control a flow of relatively lower pressure fluid from a first inlet port, a second valve assembly configured to control a flow of relatively higher pressure fluid from a second inlet port, a first actuation chamber configured to close the first valve assembly, a second actuation chamber configured to close the second valve assembly, and a third actuation chamber configured to open the second valve assembly.
    Type: Application
    Filed: June 30, 2009
    Publication date: December 30, 2010
    Inventors: Kent Weber, Athanasios Kyriazopoulos, Peter C. Hightower, Bradley J. Burie
  • Patent number: D463301
    Type: Grant
    Filed: January 30, 2002
    Date of Patent: September 24, 2002
    Inventors: William M. Martz, Bradley J. Burie