Patents by Inventor Edmond R. Coletta

Edmond R. Coletta 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: 6880743
    Abstract: The average strength of a pull plug weld is increased and weak bonding eliminated by providing a dual included angle at the top one third of the pull plug. Plugs using the included angle of the present invention had consistent high strength, no weak bonds and were substantially defect free. The dual angle of the pull plug body increases the heat and pressure of the weld in the region of the top one third of the plug. This allows the plug to form a tight high quality solid state bond. The dual angle was found to be successful in elimination of defects on both small and large plugs.
    Type: Grant
    Filed: October 8, 2002
    Date of Patent: April 19, 2005
    Assignee: Lockheed Martin Corporation
    Inventors: Edmond R. Coletta, Mark A. Cantrell
  • Patent number: 6460750
    Abstract: Friction Pull Plug Welding (FPPW) is a solid state repair process for defects up to one inch in length, only requiring single sided tooling (OSL) for usage on flight hardware. Experimental data has shown that the mass of plug heat sink remaining above the top of the plate surface after a weld is completed (the plug heat sink) affects the bonding at the plug top. A minimized heat sink ensures complete bonding of the plug to the plate at the plug top. However, with a minimal heat sink three major problems can arise, the entire plug could be pulled through the plate hole, the central portion of the plug could be separated along grain boundaries, or the plug top hat can be separated from the body. The Chamfered Heat Sink Pull Plug Design allows for complete bonding along the ISL interface through an outside diameter minimal mass heat sink, while maintaining enough central mass in the plug to prevent plug pull through, central separation, and plug top hat separation.
    Type: Grant
    Filed: May 2, 2000
    Date of Patent: October 8, 2002
    Inventors: Edmond R. Coletta, Mark A. Cantrell
  • Patent number: 6386419
    Abstract: Friction Pull Plug Welding is a solid state repair process for defects up to one inch in length, only requiring single sided tooling, or outside skin line (OSL), for preferred usage on flight hardware. The most prevalent defect associated with Friction Pull Plug Welding (FPPW) was a top side or inside skin line (ISL) lack of bonding. Bonding was not achieved at this location due to the reduction in both frictional heat and welding pressure between the plug and plate at the end of the weld. Thus, in order to eliminate the weld defects and increase the plug strength at the plug ‘top’ a small ‘hat’ section is added to the pull plug for added frictional heating and pressure.
    Type: Grant
    Filed: March 22, 2001
    Date of Patent: May 14, 2002
    Assignee: Lockhead Martin Corporation
    Inventors: Edmond R. Coletta, Mark A. Cantrell
  • Publication number: 20020027156
    Abstract: Friction Pull Plug Welding (FPPW) is a solid state repair process for defects up to one inch in length, only requiring single sided tooling (OSL) for usage on flight hardware. Early attempts with FPPW followed the matching plug/plate geometry precedence of the successful Friction Push Plug Welding program, however no defect free welds were achieved due to substantial plug necking and plug rotational stalling. The dual chamfered hole has eliminated plug rotational stalling, both upon initial plug/plate contact and during welding. Also, the necking of the heated plug metal under a tensile heating/forging load has been eliminated through the usage of the dual chamfered plate hole.
    Type: Application
    Filed: May 15, 2001
    Publication date: March 7, 2002
    Inventors: Edmond R. Coletta, Mark A. Cantrell
  • Publication number: 20010038027
    Abstract: Friction Pull Plug Welding is a solid state repair process for defects up to one inch in length, only requiring single sided tooling, or outside skin line (OSL), for preferred usage on flight hardware. The most prevalent defect associated with Friction Pull Plug Welding (FPPW) was a top side or inside skin line (ISL) lack of bonding. Bonding was not achieved at this location due to the reduction in both frictional heat and welding pressure between the plug and plate at the end of the weld. Thus, in order to eliminate the weld defects and increase the plug strength at the plug ‘top’ a small ‘hat’ section is added to the pull plug for added frictional heating and pressure.
    Type: Application
    Filed: March 22, 2001
    Publication date: November 8, 2001
    Inventors: Edmond R. Coletta, Mark A. Cantrell
  • Patent number: 6253987
    Abstract: Friction Pull Plug Welding is a solid state repair process for defects up to one inch in length, only requiring single sided tooling, or outside skin line (OSL), for preferred usage on flight hardware. The most prevalent defect associated with Friction Pull Plug Welding (FPPW) was a top side or inside skin line (ISL) lack of bonding. Bonding was not achieved at this location due to the reduction in both frictional heat and welding pressure between the plug and plate at the end of the weld. Thus, in order to eliminate the weld defects and increase the plug strength at the plug ‘top’ a small ‘hat’ section is added to the pull plug for added frictional heating and pressure.
    Type: Grant
    Filed: April 10, 2000
    Date of Patent: July 3, 2001
    Assignee: Lockheed Martin Corporation
    Inventors: Edmond R. Coletta, Mark A. Cantrell
  • Patent number: 6230958
    Abstract: Friction Pull Plug Welding (FPPW) is a solid state repair process for defects up to one inch in length, only requiring single sided tooling (OSL) for usage on flight hardware. Early attempts with FPPW followed the matching plug/plate geometry precedence of the successful Friction Push Plug Welding program, however no defect free welds were achieved due to substantial plug necking and plug rotational stalling. The dual chamfered hole has eliminated plug rotational stalling, both upon initial plug/plate contact and during welding. Also, the necking of the heated plug metal under a tensile heating/forging load has been eliminated through the usage of the dual chamfered plate hole.
    Type: Grant
    Filed: April 11, 2000
    Date of Patent: May 15, 2001
    Assignee: Lockheed Martin Corporation
    Inventors: Edmond R. Coletta, Mark A. Cantrell