Patents by Inventor Mark A. Woods

Mark A. Woods 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: 10400808
    Abstract: A one-sided fastener assembly for use in coupling an assembly stack-up includes a sleeve comprising an outer cylindrical surface and an inner tapered surface oriented at a first angle with respect to the outer surface. The inner tapered defines an opening extending through the sleeve. The fastener assembly also includes a core extending along an axis and configured for insertion into the opening. The core includes an outer tapered surface oriented at a second angle with respect to the axis configured for engagement with the sleeve inner tapered surface such that insertion of the core into the sleeve causes radial expansion of the sleeve creating an interference fit with the assembly stack-up to complete installation of the one-sided fastener assembly.
    Type: Grant
    Filed: March 10, 2016
    Date of Patent: September 3, 2019
    Assignee: The Boeing Company
    Inventors: Blake Alexander Simpson, Mark A. Woods, John E. Inman
  • Patent number: 10294976
    Abstract: A two-piece, one-sided-installation fastener system may have an internally-threaded sleeve having a shank and a sleeve head. The fastener system may include an externally-threaded core bolt having a frangible driving provision and a core bolt head.
    Type: Grant
    Filed: February 4, 2017
    Date of Patent: May 21, 2019
    Assignee: The Boeing Company
    Inventors: Jeffry G. Bickford, Mark A. Woods, Peter A. Coronado, Richard Whitlock
  • 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: 20170261023
    Abstract: A one-sided fastener assembly for use in coupling an assembly stack-up includes a sleeve comprising an outer cylindrical surface and an inner tapered surface oriented at a first angle with respect to the outer surface. The inner tapered defines an opening extending through the sleeve. The fastener assembly also includes a core extending along an axis and configured for insertion into the opening. The core includes an outer tapered surface oriented at a second angle with respect to the axis configured for engagement with the sleeve inner tapered surface such that insertion of the core into the sleeve causes radial expansion of the sleeve creating an interference fit with the assembly stack-up to complete installation of the one-sided fastener assembly.
    Type: Application
    Filed: March 10, 2016
    Publication date: September 14, 2017
    Inventors: Blake Alexander Simpson, Mark A. Woods, John E. Inman
  • Publication number: 20170146045
    Abstract: A two-piece, one-sided-installation fastener system may have an internally-threaded sleeve having a shank and a sleeve head. The fastener system may include an externally-threaded core bolt having a frangible driving provision and a core bolt head.
    Type: Application
    Filed: February 4, 2017
    Publication date: May 25, 2017
    Inventors: Jeffry G. Bickford, Mark A. Woods, Peter A. Coronado, Richard Whitlock
  • Patent number: 9644659
    Abstract: A joint fastening system employs a lock bolt having a pull stem and locking threads inserted through a bore in a joint having fay sealant between layers. A collar is received over the pull stem to engage the threads, the collar producing tension on the threads to generate clamp force sufficient for fay sealant squeeze out.
    Type: Grant
    Filed: March 17, 2014
    Date of Patent: May 9, 2017
    Assignee: The Boeing Company
    Inventors: Mark A. Woods, John A. Davies, Gregory J. Shish, Kwok Tung Chan, Eric M. Avakian, Dan Day, Omar J. Pacheo Agosto
  • Patent number: 9593706
    Abstract: A two-piece, one-sided-installation fastener system may have an internally-threaded sleeve having a shank and a sleeve head. The fastener system may include an externally-threaded core bolt having a frangible driving provision and a core bolt head.
    Type: Grant
    Filed: November 11, 2012
    Date of Patent: March 14, 2017
    Assignee: The Boeing Company
    Inventors: Jeffry G. Bickford, Mark A. Woods, Peter A. Coronado, Richard Whitlock
  • Patent number: 9291187
    Abstract: A fastener system for composite structure providing electromagnetic energy (EME) protection incorporates a fastener having a head with an engagement surface and a shank having a threaded end. A nut is received on the threaded end of the fastener, with the nut also having an engagement surface. At least one of the head engagement surface and the nut engagement surface incorporates a reduced area portion for engagement of a first mating surface or second mating surface, respectively.
    Type: Grant
    Filed: May 20, 2013
    Date of Patent: March 22, 2016
    Assignee: The Boeing Company
    Inventors: Richard P. Whitlock, Peter A. Coronado, Sean D. Morden, Julie M. Drexler, Randall A. Rogers, Mark A. Woods, Thomas J. Lowe
  • Publication number: 20150260217
    Abstract: A joint fastening system employs a lock bolt having a pull stem and locking threads inserted through a bore in a joint having fay sealant between layers. A collar is received over the pull stem to engage the threads, the collar producing tension on the threads to generate clamp force sufficient for fay sealant squeeze out.
    Type: Application
    Filed: March 17, 2014
    Publication date: September 17, 2015
    Applicant: The Boeing Company
    Inventors: Mark A. Woods, John A. Davies, Gregory J. Shish, Kwok Tung Chan, Eric M. Avakian, Dan Day, Omar J. Pacheo Agosto
  • 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: 20140338179
    Abstract: A fastener system for composite structure providing electromagnetic energy (EME) protection incorporates a fastener having a head with an engagement surface and a shank having a threaded end. A nut is received on the threaded end of the fastener, with the nut also having an engagement surface. At least one of the head engagement surface and the nut engagement surface incorporates a reduced area portion for engagement of a first mating surface or second mating surface, respectively.
    Type: Application
    Filed: May 20, 2013
    Publication date: November 20, 2014
    Applicant: The Boeing Company
    Inventors: Richard P. Whitlock, Peter A. Coronado, Sean D. Morden, Julie M. Drexler, Randall A. Rogers, Mark A. Woods, Thomas J. Lowe
  • 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
  • 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
  • Publication number: 20080201291
    Abstract: The present invention provides a distinct advance in the state of the art. The personnel accounting system for efficiently accounting of individuals after or or during an event, such as a natural disaster or during an emergency, preferably is a computer-aided system that operates to provide an improved communication system whereby individuals can be identified, tracked, monitored in real time using a central processing and communication system and collectively stores and manages information pertinent to individuals affected by the event.
    Type: Application
    Filed: February 16, 2007
    Publication date: August 21, 2008
    Inventors: John W. Fussner, Mark A. Woods
  • Publication number: 20080186161
    Abstract: A system and method for tracking, locating, and guiding personnel at a location, preferably is a computer-aided system that operates to provide a communication system whereby individuals can be tracked and guided and can communicate with a central processing and communication system as well as other individuals within the system. In a preferred embodiment of the invention, the system comprises deployable sensor arrays.
    Type: Application
    Filed: February 2, 2007
    Publication date: August 7, 2008
    Inventors: John W. Fussner, Mark A. Woods
  • Patent number: 7260998
    Abstract: Apparatuses and methods for structurally testing fasteners are described herein. A fastener test apparatus configured in accordance with one aspect of the invention includes a first support member configured to support a head portion of a fastener, and a second support member configured to support a locking feature on a shaft portion of the fastener. The test apparatus can also include a force measurement device configured to be operably sandwiched between the first support member and the second support member. The force measurement device can be used to measure fastener preload. The test apparatus can further include first and second fixtures for performing an ultimate tensile test of the fastener. In this regard, the first fixture can be configured to exert a first force against the first support member in a first direction, and the second fixture can be configured to exert a second force against the second support member in a second direction opposite the first direction.
    Type: Grant
    Filed: March 18, 2005
    Date of Patent: August 28, 2007
    Assignee: The Boeing Company
    Inventors: Stella B. Madden, Thomas J. Lowe, Mark A. Woods
  • Patent number: 6742377
    Abstract: A passive-adaptive indentor is provided for cold working a material that includes a material surface and a depth extending in a direction that is perpendicular to a direction of the material surface. The passive-adaptive indentor has a first member that includes a first working end that is configured to create a first residual stress field that extends to a predetermined depth in the material. The passive-adaptive indentor also has a second member that includes a second working end that is configured to create a second residual stress field that extends to a generally fixed second depth of the material regardless of the depth to which the first residual stress field extends. A method of using a passive-adaptive indentor for cold working a material is also presented.
    Type: Grant
    Filed: June 13, 2002
    Date of Patent: June 1, 2004
    Assignee: The Boeing Company
    Inventors: Mark A. Woods, Jeffrey A. Wilkerson
  • Patent number: 6698268
    Abstract: A passive-adaptive indentor is provided for cold working a material that includes a material surface and a depth extending in a direction that is perpendicular to a direction of the material surface. The passive-adaptive indentor has a first member that includes a first working end that is configured to create a first residual stress field that extends to a predetermined depth in the material. The passive-adaptive indentor also has a second member that includes a second working end that is configured to create a second residual stress field that extends to a generally fixed second depth of the material regardless of the depth to which the first residual stress field extends. A method of using a passive-adaptive indentor for cold working a material is also presented.
    Type: Grant
    Filed: March 18, 2002
    Date of Patent: March 2, 2004
    Assignee: The Boeing Company
    Inventors: Mark A. Woods, Jeffrey A. Wilkerson
  • Publication number: 20030172706
    Abstract: A passive-adaptive indentor is provided for cold working a material that includes a material surface and a depth extending in a direction that is perpendicular to a direction of the material surface. The passive-adaptive indentor has a first member that includes a first working end that is configured to create a first residual stress field that extends to a predetermined depth in the material. The passive-adaptive indentor also has a second member that includes a second working end that is configured to create a second residual stress field that extends to a generally fixed second depth of the material regardless of the depth to which the first residual stress field extends. A method of using a passive-adaptive indentor for cold working a material is also presented.
    Type: Application
    Filed: March 18, 2002
    Publication date: September 18, 2003
    Applicant: The Boeing Company
    Inventors: Mark A. Woods, Jeffrey A. Wilkerson