Patents by Inventor Joe Heeter

Joe Heeter 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: 11293474
    Abstract: Systems and methods are provided for fabricating fasteners. One embodiment is an apparatus that includes a fastener. The fastener includes a head, a cylindrical shank that extends from the head and is dimensioned to engage in a fit with a corresponding hole, and a coating that is discontinuously speckled around a circumference of the shank and extends axially along the shank, leaving irregular portions of a surface of the shank exposed. The coating exhibits a higher lubricity than the surface, and the coating exhibits a higher dielectric withstand voltage than the surface.
    Type: Grant
    Filed: October 18, 2019
    Date of Patent: April 5, 2022
    Assignee: The Boeing Company
    Inventors: Tanni Sisco, Antonio Carlos Rufin, Richard B Tanner, Dale Winter, Jeffrey Alan Wilkerson, Joe Heeter
  • Publication number: 20200049187
    Abstract: Systems and methods are provided for fabricating fasteners. One embodiment is an apparatus that includes a fastener. The fastener includes a head, a cylindrical shank that extends from the head and is dimensioned to engage in a fit with a corresponding hole, and a coating that is discontinuously speckled around a circumference of the shank and extends axially along the shank, leaving irregular portions of a surface of the shank exposed. The coating exhibits a higher lubricity than the surface, and the coating exhibits a higher dielectric withstand voltage than the surface.
    Type: Application
    Filed: October 18, 2019
    Publication date: February 13, 2020
    Inventors: Tanni Sisco, Antonio Carlos Rufin, Richard B. Tanner, Dale Winter, Jeffrey Alan Wilkerson, Joe Heeter
  • Patent number: 10495130
    Abstract: Systems and methods are provided for fabricating fasteners. One embodiment is an apparatus that includes a fastener. The fastener includes a head, a cylindrical shank that extends from the head and is dimensioned to engage in a fit with a corresponding hole, and a coating that is discontinuously speckled around a circumference of the shank and extends axially along the shank, leaving irregular portions of a surface of the shank exposed. The coating exhibits a higher lubricity than the surface, and the coating exhibits a higher dielectric withstand voltage than the surface.
    Type: Grant
    Filed: November 11, 2016
    Date of Patent: December 3, 2019
    Assignee: The Boeing Company
    Inventors: Tanni Sisco, Antonio Carlos Rufin, Richard B. Tanner, Dale Winter, Jeffrey Alan Wilkerson, Joe Heeter
  • Publication number: 20180135683
    Abstract: Systems and methods are provided for fabricating fasteners. One embodiment is an apparatus that includes a fastener. The fastener includes a head, a cylindrical shank that extends from the head and is dimensioned to engage in a fit with a corresponding hole, and a coating that is discontinuously speckled around a circumference of the shank and extends axially along the shank, leaving irregular portions of a surface of the shank exposed. The coating exhibits a higher lubricity than the surface, and the coating exhibits a higher dielectric withstand voltage than the surface.
    Type: Application
    Filed: November 11, 2016
    Publication date: May 17, 2018
    Inventors: Tanni Sisco, Antonio Carlos Rufin, Richard B. Tanner, Dale Winter, Jeffrey Alan Wilkerson, Joe Heeter
  • Patent number: 9003650
    Abstract: A conductive sleeved fastener assembly includes an electrically-conductive fastener having a fastener head and a fastener shank extending from the fastener head and an electrically-conductive fastener sleeve receiving the fastener shank of the fastener and a fastener sleeve flange provided on the fastener sleeve and disposed in direct contact with the fastener head of the fastener. A method of preparing a conductive sleeved fastener for use is also disclosed.
    Type: Grant
    Filed: December 27, 2012
    Date of Patent: April 14, 2015
    Assignee: The Boeing Company
    Inventors: Thu A Nguyen, Michael G Parent, Russell Joe Heeter, Jeffrey A Wilkerson
  • Patent number: 8410784
    Abstract: A device senses a static charge resulting from the impingement of particles on a surface, such as an aircraft's outer skin. The device includes a sensor adapted to be installed on the surface and a corona guard for guarding against corona discharge from the sensor.
    Type: Grant
    Filed: November 12, 2009
    Date of Patent: April 2, 2013
    Assignee: The Boeing Company
    Inventors: Arlene M Brown, Grant J Erickson, Joe Heeter, Robert Steinle, Kari L Stromsland, Winson Taam
  • Patent number: 8382413
    Abstract: A conductive sleeved fastener assembly includes an electrically-conductive fastener having a fastener head and a fastener shank extending from the fastener head and an electrically-conductive fastener sleeve receiving the fastener shank of the fastener and a fastener sleeve flange provided on the fastener sleeve and disposed in direct contact with the fastener head of the fastener. A method of preparing a conductive sleeved fastener for use is also disclosed.
    Type: Grant
    Filed: November 17, 2008
    Date of Patent: February 26, 2013
    Assignee: The Boeing Company
    Inventors: Thu A. Nguyen, Michael G. Parent, Joe Heeter, Jeffrey A. Wilkerson
  • Publication number: 20100124472
    Abstract: A conductive sleeved fastener assembly includes an electrically-conductive fastener having a fastener head and a fastener shank extending from the fastener head and an electrically-conductive fastener sleeve receiving the fastener shank of the fastener and a fastener sleeve flange provided on the fastener sleeve and disposed in direct contact with the fastener head of the fastener. A method of preparing a conductive sleeved fastener for use is also disclosed.
    Type: Application
    Filed: November 17, 2008
    Publication date: May 20, 2010
    Inventors: Thu A. Nguyen, Michael G. Parent, Joe Heeter, Jeffrey A. Wilkerson
  • Patent number: 7596997
    Abstract: A precipitation static sensor includes a bottom flexible dielectric layer (e.g., a layer of urethane tape) configured to be attached to a wing or other external surface of an aircraft, a flexible conductive layer (e.g., a layer of aluminum tape) formed over a portion of the first flexible dielectric layer, and a conductor (such as a twisted-pair wire) coupled to the flexible conductive layer. A top flexible dielectric layer is formed over a portion of the bottom dielectric layer and a portion of the flexible conductive layer, thus forming an exposed detector region. In accordance with a further embodiment, multiple such precipitation static sensors are used and coupled to a meter device (e.g., a picoammeter), which may also be coupled to a data acquisition and display for providing a visual indication of the charge accumulated by the precipitation static sensors.
    Type: Grant
    Filed: May 15, 2008
    Date of Patent: October 6, 2009
    Assignee: The Boeing Company
    Inventors: Arlene M. Brown, Grant J. Erickson, Joe Heeter, David W. Kwolek, Robert Steinle, Kari L. Stromsland
  • Publication number: 20080246490
    Abstract: A precipitation static sensor includes a bottom flexible dielectric layer (e.g., a layer of urethane tape) configured to be attached to a wing or other external surface of an aircraft, a flexible conductive layer (e.g., a layer of aluminum tape) formed over a portion of the first flexible dielectric layer, and a conductor (such as a twisted-pair wire) coupled to the flexible conductive layer. A top flexible dielectric layer is formed over a portion of the bottom dielectric layer and a portion of the flexible conductive layer, thus forming an exposed detector region. In accordance with a further embodiment, multiple such precipitation static sensors are used and coupled to a meter device (e.g., a picoammeter), which may also be coupled to a data acquisition and display for providing a visual indication of the charge accumulated by the precipitation static sensors.
    Type: Application
    Filed: May 15, 2008
    Publication date: October 9, 2008
    Inventors: Arlene M. Brown, Grant J. Erickson, Joe Heeter, David W. Kwolek, Robert Steinle, Kari L. Stromsland
  • Patent number: 7373814
    Abstract: A precipitation static sensor includes a bottom flexible dielectric layer (e.g., a layer of urethane tape) configured to be attached to a wing or other external surface of an aircraft, a flexible conductive layer (e.g., a layer of aluminum tape) formed over a portion of the first flexible dielectric layer, and a conductor (such as a twisted-pair wire) coupled to the flexible conductive layer. A top flexible dielectric layer is formed over a portion of the bottom dielectric layer and a portion of the flexible conductive layer, thus forming an exposed detector region. In accordance with a further embodiment, multiple such precipitation static sensors are used and coupled to a meter device (e.g., a picoammeter), which may also be coupled to a data acquisition and display for providing a visual indication of the charge accumulated by the precipitation static sensors.
    Type: Grant
    Filed: December 22, 2006
    Date of Patent: May 20, 2008
    Assignee: The Boeing Company
    Inventors: Arlene M. Brown, Grant J. Erickson, Joe Heeter, David W. Kwolek, Robert Steinle, Kari L. Stromsland