Patents Represented by Attorney, Agent or Law Firm Scott, Addis Senniger, Powers, Leavitt & Roedel
  • Turbine airfoil with separately formed tip and method for manufacture and repair thereof
    Patent number: 6558119
    Abstract: An airfoil for a gas turbine engine, the airfoil having a core body with an airfoil body, an integral partial height squealer tip, and an integral tip cap between the airfoil body and the integral partial height squealer tip; and a squealer tip extension bonded to the partial height squealer tip. A method for manufacture and repair of an airfoil.
    Type: Grant
    Filed: May 29, 2001
    Date of Patent: May 6, 2003
    Assignee: General Electric Company
    Inventors: Ching-Pang Lee, Jonathan James Stow, John Peter Heyward, John Howard Starkweather, Lawrence Joseph Roedl, Joseph Howell Bowden, Jr.