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: 10400808Abstract: 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: GrantFiled: March 10, 2016Date of Patent: September 3, 2019Assignee: The Boeing CompanyInventors: Blake Alexander Simpson, Mark A. Woods, John E. Inman
-
Patent number: 10294976Abstract: 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: GrantFiled: February 4, 2017Date of Patent: May 21, 2019Assignee: The Boeing CompanyInventors: Jeffry G. Bickford, Mark A. Woods, Peter A. Coronado, Richard Whitlock
-
Patent number: 10072694Abstract: 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: GrantFiled: April 13, 2015Date of Patent: September 11, 2018Assignee: The Boeing CompanyInventors: Mark A. Woods, John A. Davies, Jr., Edward E. Feikert, John E. Inman, Elizabeth Denise Blahut, Jeffry G. Bickford
-
Publication number: 20170261023Abstract: 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: ApplicationFiled: March 10, 2016Publication date: September 14, 2017Inventors: Blake Alexander Simpson, Mark A. Woods, John E. Inman
-
Publication number: 20170146045Abstract: 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: ApplicationFiled: February 4, 2017Publication date: May 25, 2017Inventors: Jeffry G. Bickford, Mark A. Woods, Peter A. Coronado, Richard Whitlock
-
Patent number: 9644659Abstract: 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: GrantFiled: March 17, 2014Date of Patent: May 9, 2017Assignee: The Boeing CompanyInventors: Mark A. Woods, John A. Davies, Gregory J. Shish, Kwok Tung Chan, Eric M. Avakian, Dan Day, Omar J. Pacheo Agosto
-
Patent number: 9593706Abstract: 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: GrantFiled: November 11, 2012Date of Patent: March 14, 2017Assignee: The Boeing CompanyInventors: Jeffry G. Bickford, Mark A. Woods, Peter A. Coronado, Richard Whitlock
-
Patent number: 9291187Abstract: 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: GrantFiled: May 20, 2013Date of Patent: March 22, 2016Assignee: The Boeing CompanyInventors: Richard P. Whitlock, Peter A. Coronado, Sean D. Morden, Julie M. Drexler, Randall A. Rogers, Mark A. Woods, Thomas J. Lowe
-
Publication number: 20150260217Abstract: 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: ApplicationFiled: March 17, 2014Publication date: September 17, 2015Applicant: The Boeing CompanyInventors: Mark A. Woods, John A. Davies, Gregory J. Shish, Kwok Tung Chan, Eric M. Avakian, Dan Day, Omar J. Pacheo Agosto
-
Publication number: 20150211566Abstract: 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: ApplicationFiled: April 13, 2015Publication date: July 30, 2015Inventors: Mark A. Woods, John A. Davies, JR., Edward E. Feikert, John E. Inman, Elizabeth Denise Blahut, Jeffry G. Bickford
-
Patent number: 9032602Abstract: 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: GrantFiled: July 15, 2011Date of Patent: May 19, 2015Assignee: The Boeing CompanyInventors: Mark A. Woods, John A. Davies, Jr., Edward E. Feikert, John E. Inman, Elizabeth Denise Blahut, Jeffry G. Bickford
-
Publication number: 20140338179Abstract: 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: ApplicationFiled: May 20, 2013Publication date: November 20, 2014Applicant: The Boeing CompanyInventors: Richard P. Whitlock, Peter A. Coronado, Sean D. Morden, Julie M. Drexler, Randall A. Rogers, Mark A. Woods, Thomas J. Lowe
-
Publication number: 20130014368Abstract: 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: ApplicationFiled: July 15, 2011Publication date: January 17, 2013Inventors: Mark A. Woods, John A. Davies, JR., Edward E. Feikert, John E. Inman, Elizabeth Denise Blahut, Jeffry G. Bickford
-
Publication number: 20120201999Abstract: 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: ApplicationFiled: February 8, 2011Publication date: August 9, 2012Inventors: Mark A. Woods, John E. Inman, Edward E. Feikert, Julie R. Jones, Elizabeth D. Blahut
-
Publication number: 20080201291Abstract: 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: ApplicationFiled: February 16, 2007Publication date: August 21, 2008Inventors: John W. Fussner, Mark A. Woods
-
Publication number: 20080186161Abstract: 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: ApplicationFiled: February 2, 2007Publication date: August 7, 2008Inventors: John W. Fussner, Mark A. Woods
-
Patent number: 7260998Abstract: 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: GrantFiled: March 18, 2005Date of Patent: August 28, 2007Assignee: The Boeing CompanyInventors: Stella B. Madden, Thomas J. Lowe, Mark A. Woods
-
Patent number: 6742377Abstract: 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: GrantFiled: June 13, 2002Date of Patent: June 1, 2004Assignee: The Boeing CompanyInventors: Mark A. Woods, Jeffrey A. Wilkerson
-
Patent number: 6698268Abstract: 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: GrantFiled: March 18, 2002Date of Patent: March 2, 2004Assignee: The Boeing CompanyInventors: Mark A. Woods, Jeffrey A. Wilkerson
-
Publication number: 20030172706Abstract: 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: ApplicationFiled: March 18, 2002Publication date: September 18, 2003Applicant: The Boeing CompanyInventors: Mark A. Woods, Jeffrey A. Wilkerson