Patents by Inventor Timothy D. Jackson

Timothy D. Jackson 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: 11034100
    Abstract: A method and apparatus for forming a composite object. A first plurality of tows is laid up over a tool according to a first path. A second plurality of tows is laid up over the tool according to a second path. A first portion of the first plurality of tows runs non-parallel to a second portion of the second plurality of tows. First ends of the first portion of the first plurality of tows and second ends of the second portion of the second plurality of tows meet at a merge zone along the tool to form a ply of a composite laminate.
    Type: Grant
    Filed: June 20, 2018
    Date of Patent: June 15, 2021
    Assignee: The Boeing Company
    Inventors: Michael Kenneth-Que Louie, Jeron D. Moore, Gagandeep Saini, Luis A. Perla, Brice Aaron Johnson, Stewart James Ibbotson, Timothy D. Jackson, Robert G. Meyer, Robert Graham Albers
  • Publication number: 20190389150
    Abstract: A method and apparatus for forming a composite object. A first plurality of tows is laid up over a tool according to a first path. A second plurality of tows is laid up over the tool according to a second path. A first portion of the first plurality of tows runs non-parallel to a second portion of the second plurality of tows. First ends of the first portion of the first plurality of tows and second ends of the second portion of the second plurality of tows meet at a merge zone along the tool to form a ply of a composite laminate.
    Type: Application
    Filed: June 20, 2018
    Publication date: December 26, 2019
    Inventors: Michael Kenneth-Que Louie, Jeron D. Moore, Gagandeep Saini, Luis A. Perla, Brice Aaron Johnson, Stewart James Ibbotson, Timothy D. Jackson, Robert G. Meyer, Robert Graham Albers
  • Patent number: 10308344
    Abstract: The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.
    Type: Grant
    Filed: May 11, 2017
    Date of Patent: June 4, 2019
    Assignee: The Boeing Company
    Inventors: Lyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
  • Publication number: 20170246830
    Abstract: The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.
    Type: Application
    Filed: May 11, 2017
    Publication date: August 31, 2017
    Applicant: The Boeing Company
    Inventors: Lyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
  • Patent number: 9676470
    Abstract: The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.
    Type: Grant
    Filed: March 9, 2015
    Date of Patent: June 13, 2017
    Assignee: The Boeing Company
    Inventors: Lyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
  • Publication number: 20150175250
    Abstract: The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.
    Type: Application
    Filed: March 9, 2015
    Publication date: June 25, 2015
    Inventors: Lyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
  • Patent number: 8974886
    Abstract: The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.
    Type: Grant
    Filed: April 25, 2012
    Date of Patent: March 10, 2015
    Assignee: The Boeing Company
    Inventors: Lyle Ray Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth John DuffiƩ, Gregory B. Doty
  • Publication number: 20130287995
    Abstract: The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.
    Type: Application
    Filed: April 25, 2012
    Publication date: October 31, 2013
    Inventors: Lyle Ray Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth John DuffiƩ, Gregory B. Doty