Patents by Inventor Peter A. Coronado

Peter A. Coronado 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: 10587107
    Abstract: A dual protection inner seal washer employs a radially outward metallic portion having a dielectric coating and a radially inward polymeric portion engaging the metallic portion at an interface with an interference fit. The polymeric portion has at least one tapering compression surface to engage a surface of a structure proximate a hole and further has a fastener element contact surface to engage a mating surface on a fastener system element. Torqueing of the fastener element compresses the at least one compression surface inducing a predetermined pressure in the polymeric portion in a joint created by the fastener element and structure.
    Type: Grant
    Filed: September 25, 2017
    Date of Patent: March 10, 2020
    Assignee: The Boeing Company
    Inventors: Sean D. Morden, Peter A Coronado, Richard P. Whitlock, Haftom Y. Dessalegn, Julie M. Drexler
  • 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
  • Publication number: 20190097407
    Abstract: A dual protection inner seal washer employs a radially outward metallic portion having a dielectric coating and a radially inward polymeric portion engaging the metallic portion at an interface with an interference fit. The polymeric portion has at least one tapering compression surface to engage a surface of a structure proximate a hole and further has a fastener element contact surface to engage a mating surface on a fastener system element. Torqueing of the fastener element compresses the at least one compression surface inducing a predetermined pressure in the polymeric portion in a joint created by the fastener element and structure.
    Type: Application
    Filed: September 25, 2017
    Publication date: March 28, 2019
    Inventors: Sean D. Morden, Peter A. Coronado, Richard P. Whitlock, Haftom Y. Dessalegn, Julie M. Drexler
  • Patent number: 9908637
    Abstract: A fastener system for composite structure providing electromagnetic energy protection has a shank with a threaded portion on a first end of the shank terminating in a lead-in portion. A head is present on a second end of the shank. The shank is adapted for intimate conductive contact with an inner surface of an interference fit hole.
    Type: Grant
    Filed: May 23, 2014
    Date of Patent: March 6, 2018
    Assignee: The Boeing Company
    Inventors: Richard P. Whitlock, Peter A. Coronado, Omar J. Pacheco Agosto, Michael H. E. Ware
  • Patent number: 9802715
    Abstract: Fasteners are inserted into a stack of members and terminated with parts having at least one of a dry dielectric coating and a dry dielectric seal at select locations to protect against electromagnetic effects (EME).
    Type: Grant
    Filed: March 29, 2012
    Date of Patent: October 31, 2017
    Assignee: The Boeing Company
    Inventors: Richard P. Whitlock, Randall A. Rogers, Peter A. Coronado, Sean D. Morden
  • Publication number: 20170275019
    Abstract: Fasteners are inserted into a stack of members and terminated with parts having at least one of a dry dielectric coating and a dry dielectric seal at select locations to protect against electromagnetic effects (EME).
    Type: Application
    Filed: June 13, 2017
    Publication date: September 28, 2017
    Applicant: The Boeing Company
    Inventors: Richard P. Whitlock, Randall A. Rogers, Peter A. Coronado, Sean D. Morden
  • 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: 9611052
    Abstract: Fasteners are inserted into a stack of members and terminated with parts having at least one of a dry dielectric coating and an inner dry dielectric seal at select locations to protect against electromagnetic effects (EME).
    Type: Grant
    Filed: November 6, 2013
    Date of Patent: April 4, 2017
    Assignee: The Boeing Company
    Inventors: Richard P. Whitlock, Peter A. Coronado, Sean D. Morden, Randall A. Rogers
  • 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: 20150337885
    Abstract: A fastener system for composite structure providing electromagnetic energy protection has a shank with a threaded portion on a first end of the shank terminating in a lead-in portion. A head is present on a second end of the shank. The shank is adapted for intimate conductive contact with an inner surface of an interference fit hole.
    Type: Application
    Filed: May 23, 2014
    Publication date: November 26, 2015
    Applicant: The Boeing Company
    Inventors: Richard P. Whitlock, Peter A. Coronado, Omar J. Pacheco Agosto, Michael H. E. Ware
  • Patent number: 9169862
    Abstract: A fastener system for composite structure provides electromagnetic energy protection by incorporating a self-aligning head (SAH) fastener having a head with a spherical engaging surface and a shank extending from the head for insertion through a hole in a composite structure and a self-aligning self sealing (SASS) washer having a throat receiving the shank and a spherical mating surface interfacing with the spherical engaging surface of the head.
    Type: Grant
    Filed: February 19, 2013
    Date of Patent: October 27, 2015
    Assignee: The Boeing Company
    Inventors: Richard P. Whitlock, Peter A. Coronado, Sean D. Morden, Randall A. Rogers, Julie M. Drexler, John R. Porter, Jeffry G. Bickford
  • Patent number: 9108363
    Abstract: A method for directing electrical current to prevent sparking from the interaction between a composite structure and lightning or static electrical charge, the method including the steps of forming a hole in a composite structure; and positioning a bushing into the hole to create an interference fit between the bushing and the composite structure, wherein the bushing is formed of a material that has a coefficient of thermal expansion close to the coefficient of thermal expansion of the composite structure and the bushing provides an electrical path between a fastener disposed in the bushing and the composite structure.
    Type: Grant
    Filed: October 6, 2011
    Date of Patent: August 18, 2015
    Assignee: THE BOEING COMPANY
    Inventors: Matthew Anthony Dilligan, James P. Irwin, Christopher Newbolt, Peter A. Coronado, Benjamin A. Johnson
  • 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: 20140055906
    Abstract: Fasteners are inserted into a stack of members and terminated with parts having at least one of a dry dielectric coating and an inner dry dielectric seal at select locations to protect against electromagnetic effects (EME).
    Type: Application
    Filed: November 6, 2013
    Publication date: February 27, 2014
    Applicant: THE BOEING COMPANY
    Inventors: Richard P. Whitlock, Peter A. Coronado, Sean D. Morden, Randall A. Rogers
  • Publication number: 20130259604
    Abstract: Fasteners are inserted into a stack of members and terminated with parts having at least one of a dry dielectric coating and a dry dielectric seal at select locations to protect against electromagnetic effects (EME).
    Type: Application
    Filed: March 29, 2012
    Publication date: October 3, 2013
    Applicant: THE BOEING COMPANY
    Inventors: Richard P. Whitlock, Randall A. Rogers, Peter A. Coronado, Sean D. Morden
  • Publication number: 20130087380
    Abstract: A method for directing electrical current to prevent sparking from the interaction between a composite structure and lightning or static electrical charge, the method including the steps of forming a hole in a composite structure; and positioning a bushing into the hole to create an interference fit between the bushing and the composite structure, wherein the bushing is formed of a material that has a coefficient of thermal expansion close to the coefficient of thermal expansion of the composite structure and the bushing provides an electrical path between a fastener disposed in the bushing and the composite structure.
    Type: Application
    Filed: October 6, 2011
    Publication date: April 11, 2013
    Applicant: THE BOEING COMPANY
    Inventors: Matthew Anthony Dilligan, James P. Irwin, Christopher Newbolt, Peter A. Coronado, Benjamin A. Johnson
  • Publication number: 20130075150
    Abstract: A system includes a composite structure and a bushing. The composite structure includes an opening defined therethrough. The bushing includes a cylindrical body sized to be secured within the opening in an interference fit to facilitate providing electromagnetic effects protection in the composite structure. The cylindrical body is fabricated from a conductive material.
    Type: Application
    Filed: September 27, 2011
    Publication date: March 28, 2013
    Inventors: Christopher L. Newbolt, Rebecca Elizabeth Ludwig (nee Ahern), James P. Irwin, Peter A. Coronado, Benjamin A. Johnson
  • Publication number: 20130061423
    Abstract: A bushing assembly includes a washer that includes an opening defined therethrough. A cylindrical body includes a first end that is sized to be inserted within the washer opening and an opposite second end. The cylindrical body is fabricated from a smart material that is configured to selectively expand when at least a portion of the body is positioned within the washer opening.
    Type: Application
    Filed: September 12, 2011
    Publication date: March 14, 2013
    Inventors: Rebecca Elizabeth Ahern, Christopher L. Newbolt, James P. Irwin, Peter A. Coronado, Benjamin A. Johnson
  • Patent number: 7936550
    Abstract: A fastening assembly for a composite structure including a washer sealing the assembly for internal lightning strike protection. The washer includes one or more concentric ribs that are dielectric rings on both sides. When used (e.g., with a nut and bolt) internal to a structure, especially a composite structure, the washer seals the fastener hole (i.e., that the bolt passes through) and contains any sparking and hot gasses that may arise in the fastener hole from entering the structure.
    Type: Grant
    Filed: July 12, 2010
    Date of Patent: May 3, 2011
    Assignee: The Boeing Company
    Inventors: Justin H. Morrill, Peter A. Coronado, Daniel J. Kovach