Patents by Inventor David Bombara

David Bombara 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: 7527479
    Abstract: A mechanical coupling for coupling a ceramic disc member to a metallic shaft includes a first wedge clamp and a second wedge clamp. A fastener engages a threaded end of a tie-bolt to sandwich the ceramic disc between the wedge clamps. An axial spring is positioned between the fastener and the second wedge clamp to apply an axial preload along the longitudinal axis. Another coupling utilizes a rotor shaft end of a metallic rotor shaft as one wedge clamp. Still another coupling includes a solid ceramic rotor disc with a multiple of tie-bolts radially displaced from the longitudinal axis to exert the preload on the solid ceramic rotor disc.
    Type: Grant
    Filed: September 8, 2005
    Date of Patent: May 5, 2009
    Assignee: Hamilton Sundstrand Corporation
    Inventors: Jun Shi, David Bombara, Kevin E. Green, Connic Bird, John Holowczak
  • Publication number: 20070237646
    Abstract: A mechanical coupling for coupling a ceramic disc member to a metallic shaft includes a first wedge clamp and a second wedge clamp. A fastener engages a threaded end of a tie-bolt to sandwich the ceramic disc between the wedge clamps. An axial spring is positioned between the fastener and the second wedge clamp to apply an axial preload along the longitudinal axis. Another coupling utilizes a rotor shaft end of a metallic rotor shaft as one wedge clamp. Still another coupling includes a solid ceramic rotor disc with a multiple of tie-bolts radially displaced from the longitudinal axis to exert the preload on the solid ceramic rotor disc.
    Type: Application
    Filed: September 8, 2005
    Publication date: October 11, 2007
    Inventors: Jun Shi, David Bombara, Kevin Green, Connic Bird, John Holowczak
  • Publication number: 20060242965
    Abstract: A combustion system for an engine, such as a gas turbine engine is provided. The combustion system has a ceramic component, such as ceramic combustor liner, and at least one metal support component, such as a metal ring or a plurality of metal cones, for providing radial and axial support to the ceramic component. The at least one metal support component includes a structure, such as axial slots or radial slots, for minimizing stress and for increasing compliance of the metal support component with respect to the ceramic component.
    Type: Application
    Filed: April 27, 2005
    Publication date: November 2, 2006
    Inventors: Jun Shi, Jason Lawrence, David Bombara, Richard Tuthill, Jeffrey Melman