Patents by Inventor Edward E. Feikert

Edward E. Feikert 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: 10072694
    Abstract: A fastener insertion system, for use with an assembly stack-up, includes a fastener and an end effector. The end effector includes a drill bit for drilling a hole through the stack-up, a probe for determining a stack-up parameter, and a fastener feed head for installing the fastener into the hole and applying rotational torque to complete fastener installation. The fastener insertion system also includes a processing device and an angle sensor communicatively coupled to the processing device and to the end effector. The processing device is programmed to measure, with the rotation angle sensor, the angular displacement required to complete fastener installation and to transmit a signal representative of the measured angular displacement from the angle sensor to the processing device. The processing device is also programmed to compare the measurement of angular displacement required to complete fastener installation to a range of angular displacement indicative of correct fastener installation.
    Type: Grant
    Filed: April 13, 2015
    Date of Patent: September 11, 2018
    Assignee: The Boeing Company
    Inventors: Mark A. Woods, John A. Davies, Jr., Edward E. Feikert, John E. Inman, Elizabeth Denise Blahut, Jeffry G. Bickford
  • Publication number: 20150211566
    Abstract: A fastener insertion system, for use with an assembly stack-up, includes a fastener and an end effector. The end effector includes a drill bit for drilling a hole through the stack-up, a probe for determining a stack-up parameter, and a fastener feed head for installing the fastener into the hole and applying rotational torque to complete fastener installation. The fastener insertion system also includes a processing device and an angle sensor communicatively coupled to the processing device and to the end effector. The processing device is programmed to measure, with the rotation angle sensor, the angular displacement required to complete fastener installation and to transmit a signal representative of the measured angular displacement from the angle sensor to the processing device. The processing device is also programmed to compare the measurement of angular displacement required to complete fastener installation to a range of angular displacement indicative of correct fastener installation.
    Type: Application
    Filed: April 13, 2015
    Publication date: July 30, 2015
    Inventors: Mark A. Woods, John A. Davies, JR., Edward E. Feikert, John E. Inman, Elizabeth Denise Blahut, Jeffry G. Bickford
  • Patent number: 9032602
    Abstract: A method for assembling a structure is described. The method includes locating a position in an assembly stack-up where a one-sided fastener is to be installed, drilling a hole through the assembly stack-up at the position, countersinking the hole to a specified depth, operating a calibrated probe to determine at least parameter associated with one or more of the hole and the stack-up proximate the hole, inserting the one-sided fastener into the hole, applying a rotational torque to the one-sided fastener to complete installation of the one-sided fastener, and comparing a measurement of angular displacement required to complete installation of the one-sided fastener to a range of angular displacement indicative of correct installation of the fastener.
    Type: Grant
    Filed: July 15, 2011
    Date of Patent: May 19, 2015
    Assignee: The Boeing Company
    Inventors: Mark A. Woods, John A. Davies, Jr., Edward E. Feikert, John E. Inman, Elizabeth Denise Blahut, Jeffry G. Bickford
  • Publication number: 20130014368
    Abstract: A method for assembling a structure is described. The method includes locating a position in an assembly stack-up where a one-sided fastener is to be installed, drilling a hole through the assembly stack-up at the position, countersinking the hole to a specified depth, operating a calibrated probe to determine at least parameter associated with one or more of the hole and the stack-up proximate the hole, inserting the one-sided fastener into the hole, applying a rotational torque to the one-sided fastener to complete installation of the one-sided fastener, and comparing a measurement of angular displacement required to complete installation of the one-sided fastener to a range of angular displacement indicative of correct installation of the fastener.
    Type: Application
    Filed: July 15, 2011
    Publication date: January 17, 2013
    Inventors: Mark A. Woods, John A. Davies, JR., Edward E. Feikert, John E. Inman, Elizabeth Denise Blahut, Jeffry G. Bickford
  • Patent number: 8275479
    Abstract: A method and apparatus for performing an operation on a workpiece. Image information may be received from a camera system at a controller in which the camera system and the controller may be associated with a housing. The workpiece with a number of inconsistencies and a tool system may be moved relative to each other under a control of the controller in which the tool system may be associated with the housing. A number of operations may be performed on the number of inconsistencies on the workpiece holes using the image information under the control of the controller.
    Type: Grant
    Filed: October 21, 2009
    Date of Patent: September 25, 2012
    Assignee: The Boeing Company
    Inventors: Philip L. Freeman, Edward E. Feikert, John E. Inman
  • Publication number: 20120201999
    Abstract: A method for joining a composite structure and a metallic structure is described. The method includes aligning the composite structure and the metallic structure, drilling a hole through the aligned structures creating an aligned hole, and inserting an interference fit fastener through the aligned hole such that the interference fit fastener engages a cylindrical wall in the composite structure formed by the drilling of the hole.
    Type: Application
    Filed: February 8, 2011
    Publication date: August 9, 2012
    Inventors: Mark A. Woods, John E. Inman, Edward E. Feikert, Julie R. Jones, Elizabeth D. Blahut
  • Patent number: 7292029
    Abstract: A method for detecting substructure includes the steps of: nondestructively scanning an assembly using a substructure scanning system including a precision motion carriage and a nondestructive scanning sensor, positioning the assembly under the substructure scanning system, positioning the scanning sensor on the outer skin, moving the scanning sensor over the outer skin with the precision motion carriage, locating the substructure through the outer skin, and controlling an assembly process using the location of the substructure. By using the method of the present invention substructure features may be located through an outer skin with sufficient accuracy to control assembly operations and to meet engineering tolerances. The method for precisely detecting substructure using precision eddy current scanning may be used for, but is not limited to, the location of substructure features, such as edges of flanges, machined steps, or tooling holes, covered by outer mold line skins of an aircraft airframe.
    Type: Grant
    Filed: October 28, 2004
    Date of Patent: November 6, 2007
    Assignee: The Boeing Company
    Inventors: Edward E. Feikert, Nancy Wood, Eugene A. Myers