Patents by Inventor Thomas R. Cundiff

Thomas R. Cundiff 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: 8974212
    Abstract: Methods and systems for manufacturing fiber-reinforced resin parts are disclosed herein. In one embodiment, a method for manufacturing a fiber-reinforced resin part includes positioning a plurality of fibers on a mold surface of a female tool, and covering the fibers with a sealing layer. The method further includes pressing a portion of the covered fibers against an interior transition region (e.g., an internal radius) of the mold surface. While the portion of covered fibers is pressed against the interior transition region, air is removed from between the sealing layer and the mold surface to draw at least a partial vacuum between the sealing layer and the mold surface.
    Type: Grant
    Filed: October 9, 2009
    Date of Patent: March 10, 2015
    Assignee: The Boeing Company
    Inventors: Thomas R. Cundiff, Dennis J. Hanks, Jack A. Woods, Val G. Brustad, Andrew E. Modin
  • Patent number: 8944128
    Abstract: An apparatus for tensioning a preform may include a mandrel to receive a preform. The mandrel may have a first mandrel end and a second mandrel end. The preform may have a first preform end and a second preform end. The apparatus may include an anchoring groove disposed at the first mandrel end, and an anchoring device being configured and located to urge the first preform end towards the anchoring groove to secure the first preform end therebetween. The apparatus may include a tensioning groove disposed between the first mandrel end and the second mandrel end, and a tensioning device being configured and located to urge at least a portion of the preform into the tensioning groove.
    Type: Grant
    Filed: June 25, 2012
    Date of Patent: February 3, 2015
    Assignee: The Boeing Company
    Inventors: Michael L. Glain, David J. Kehrl, Andrew E. Modin, Scott A. Harris, Robert A. Coleman, Andrew Head, Steven C. Stenard, Thomas R. Cundiff, Joo Hyun Han, Timothy D. Aquino
  • Patent number: 8303757
    Abstract: An apparatus to prepare a preform for fabrication includes a mandrel, anchoring groove, anchoring device, tensioning groove, and tensioning device. The mandrel receives the preform. The mandrel has a first mandrel end and a second mandrel end. The preform has a first preform end and a second preform end. The anchoring groove is disposed at the first mandrel end. The anchoring device is configured and located to urge the first preform end towards the anchoring groove to secure the first preform end therebetween. The tensioning groove is disposed between the first mandrel end and the second mandrel end. The tensioning device is configured and located to urge a portion of the preform into the tensioning groove.
    Type: Grant
    Filed: December 4, 2006
    Date of Patent: November 6, 2012
    Assignee: The Boeing Company
    Inventors: Michael L. Glain, David J. Kehrl, Andrew E. Modin, Scott A. Harris, Robert A. Coleman, Andrew Head, Steven C. Stenard, Thomas R. Cundiff, Joo Hyun Han, Timothy D. Aquino
  • Publication number: 20120263818
    Abstract: An apparatus for tensioning a preform may include a mandrel to receive a preform. The mandrel may have a first mandrel end and a second mandrel end. The preform may have a first preform end and a second preform end. The apparatus may include an anchoring groove disposed at the first mandrel end, and an anchoring device being configured and located to urge the first preform end towards the anchoring groove to secure the first preform end therebetween. The apparatus may include a tensioning groove disposed between the first mandrel end and the second mandrel end, and a tensioning device being configured and located to urge at least a portion of the preform into the tensioning groove.
    Type: Application
    Filed: June 25, 2012
    Publication date: October 18, 2012
    Applicant: THE BOEING COMPANY
    Inventors: Michael L. GLAIN, David J. KEHRL, Andrew E. MODIN, Scott A. HARRIS, Robert A. COLEMAN, Andrew HEAD, Steven C. STENARD, Thomas R. CUNDIFF, Joo Hyun HAN, Timothy D. AQUINO
  • Publication number: 20100074979
    Abstract: Methods and systems for manufacturing fiber-reinforced resin parts are disclosed herein. In one embodiment, a method for manufacturing a fiber-reinforced resin part includes positioning a plurality of fibers on a mold surface of a female tool, and covering the fibers with a sealing layer. The method further includes pressing a portion of the covered fibers against an interior transition region (e.g., an internal radius) of the mold surface. While the portion of covered fibers is pressed against the interior transition region, air is removed from between the sealing layer and the mold surface to draw at least a partial vacuum between the sealing layer and the mold surface.
    Type: Application
    Filed: October 9, 2009
    Publication date: March 25, 2010
    Applicant: The Boeing Company
    Inventors: Thomas R. Cundiff, Dennis J. Hanks, Jack A. Woods, Val G. Brustad, Andrew E. Modin
  • Patent number: 7622066
    Abstract: Methods and systems for manufacturing fiber-reinforced resin parts are disclosed herein. In one embodiment, a method for manufacturing a fiber-reinforced resin part includes positioning a plurality of fibers on a mold surface of a female tool, and covering the fibers with a sealing layer. The method further includes pressing a portion of the covered fibers against an interior transition region (e.g., an internal radius) of the mold surface. While the portion of covered fibers is pressed against the interior transition region, air is removed from between the sealing layer and the mold surface to draw at least a partial vacuum between the sealing layer and the mold surface.
    Type: Grant
    Filed: July 26, 2004
    Date of Patent: November 24, 2009
    Assignee: The Boeing Company
    Inventors: Val G. Brustad, Thomas R. Cundiff, Dennis J. Hanks, Jack A. Woods, Andrew E. Modin
  • Publication number: 20080283177
    Abstract: An apparatus to prepare a preform for fabrication includes a mandrel, anchoring groove, anchoring device, tensioning groove, and tensioning device. The mandrel receives the preform. The mandrel has a first mandrel end and a second mandrel end. The preform has a first preform end and a second preform end. The anchoring groove is disposed at the first mandrel end. The anchoring device is configured and located to urge the first preform end towards the anchoring groove to secure the first preform end therebetween. The tensioning groove is disposed between the first mandrel end and the second mandrel end. The tensioning device is configured and located to urge a portion of the preform into the tensioning groove.
    Type: Application
    Filed: December 4, 2006
    Publication date: November 20, 2008
    Inventors: Michael L. Glain, David J. Kehrl, Andrew E. Modin, Scott A. Harris, Robert A. Coleman, Andrew Head, Steven C. Stenard, Thomas R. Cundiff, Joo Hyun Han, Timothy D. Aquino
  • Patent number: 7147895
    Abstract: A wind tunnel blade (30) connected to a base (32) and held in position by a two-piece cuff (34). The wind tunnel blade (30) is formed in a resin transfer molding process in which central, fore, and aft foam core sections (70, 72, 74) are placed together to form the wind tunnel blade (30). Radius fillers (120) are used to fill the gaps between the outer edge of the foam core sections. The radius fillers (120) used in the wind tunnel blade (30) are formed by a braided sleeve (122) surrounding a number of unidirectional tows (124). A tip (68) is formed separately from the rest of the wind tunnel blade (30) and is glued to the top thereof. Stacked layers of braided fibers (100) are used to reinforce the central core section (70).
    Type: Grant
    Filed: January 15, 2004
    Date of Patent: December 12, 2006
    Assignee: The Boeing Company
    Inventors: Thomas R. Cundiff, Henry H. Bennett, Brad G. Lund, Robert S. Renz, Donald E. Wright
  • Patent number: 6872340
    Abstract: A wind tunnel blade (30) connected to a base (32) and held in position by a two-piece cuff (34). The wind tunnel blade (30) is formed in a resin transfer molding process in which central, fore, and aft foam core sections (70, 72, 74) are placed together to form the wind tunnel blade (30). Radius fillers (120) are used to fill the gaps between the outer edge of the foam core sections. The radius fillers (120) used in the wind tunnel blade (30) are formed by a braided sleeve (122) surrounding a number of unidirectional tows (124). A tip (68) is formed separately from the rest of the wind tunnel blade (30) and is glued to the top thereof. Stacked layers of braided fibers (100) are used to reinforce the central core section (70).
    Type: Grant
    Filed: May 30, 2003
    Date of Patent: March 29, 2005
    Assignee: The Boeing Company
    Inventors: Thomas R. Cundiff, Henry H. Bennett, Brad G. Lund, Robert S. Renz, Donald E. Wright
  • Patent number: 6811733
    Abstract: A method for forming a plurality of composite parts via resin transfer molding in a single molding cycle. The method includes the steps of using a mold having first and second mold members that cooperate to house a plurality of shims and placing a plurality of preform workpiece into the mold cavity such that at least one of the shims is disposed between each of an adjacent pair of the preform workpieces. A liquid resin is then injected into the mold cavity and subsequently cured to thereby form a cured workpiece matrix that is composed of a plurality of semi-finished composite parts and at least one shim separating the plurality of semi-finished composite parts from one another.
    Type: Grant
    Filed: November 13, 2001
    Date of Patent: November 2, 2004
    Assignee: The Boeing Company
    Inventors: Karl M. Nelson, Thomas R. Cundiff, Scott A. Miller
  • Publication number: 20040150130
    Abstract: A wind tunnel blade (30) connected to a base (32) and held in position by a two-piece cuff (34). The wind tunnel blade (30) is formed in a resin transfer molding process in which central, fore, and aft foam core sections (70, 72, 74) are placed together to form the wind tunnel blade (30). Radius fillers (120) are used to fill the gaps between the outer edge of the foam core sections. The radius fillers (120) used in the wind tunnel blade (30) are formed by a braided sleeve (122) surrounding a number of unidirectional tows (124). A tip (68) is formed separately from the rest of the wind tunnel blade (30) and is glued to the top thereof. Stacked layers of braided fibers (100) are used to reinforce the central core section (70).
    Type: Application
    Filed: January 15, 2004
    Publication date: August 5, 2004
    Applicant: The Boeing Company
    Inventors: Thomas R. Cundiff, Henry H. Bennett, Brad G. Lund, Robert S. Renz, Donald E. Wright
  • Publication number: 20040018265
    Abstract: A liquid molding pressure control apparatus is provided that includes a housing and a piston assembly movably disposed within the housing. The piston assembly includes a shaft and first and second pistons engaged with the shaft. The housing is configured to receive a pressurized fluid adjacent the first piston and to receive a starting material adjacent the second piston. The first and second pistons are sized such that the starting material received within the housing exits the housing at a pressure greater than the pressure of the pressurized fluid received within the housing. Accordingly, the liquid molding control apparatus may be used to increase the pressure within the mold cavity after mold cavity has been provided with the starting material. Alternatively, the liquid molding control apparatus may be used to substantially maintain pressure within a mold cavity after the mold cavity has been provided with the starting material.
    Type: Application
    Filed: July 24, 2002
    Publication date: January 29, 2004
    Inventors: Scott A. Miller, Thomas R. Cundiff
  • Publication number: 20030183067
    Abstract: A wind tunnel blade (30) connected to a base (32) and held in position by a two-piece cuff (34). The wind tunnel blade (30) is formed in a resin transfer molding process in which central, fore, and alt foam core sections (70, 72, 74) are placed together to form the wind tunnel blade (30). Radius fillers (120) are used to fill the gaps between the outer edge of the foam core sections. The radius fillers (120) used in the wind tunnel blade (30) are formed by a braided sleeve (122) surrounding a number of unidirectional tows (124). A tip (68) is formed separately from the rest of the wind tunnel blade (30) and is glued to the top thereof. Stacked layers of braided fibers (100) are used to reinforce the central core section (70).
    Type: Application
    Filed: May 30, 2003
    Publication date: October 2, 2003
    Applicant: The Boeing Company
    Inventors: Thomas R. Cundiff, Henry H. Bennett, Brad G. Lund, Robert S. Renz, Donald E. Wright
  • Patent number: 6589618
    Abstract: A wind tunnel blade (30) connected to a base (32) and held in position by a two-piece cuff (34). The wind tunnel blade (30) is formed in a resin transfer molding process in which central, fore, and aft foam core sections (70, 72, 74) are placed together to form the wind tunnel blade (30). Radius fillers (120) are used to fill the gaps between the outer edge of the foam core sections. The radius fillers (120) used in the wind tunnel blade (30) are formed by a braided sleeve (122) surrounding a number of unidirectional tows (124). A tip (68) is formed separately from the rest of the wind tunnel blade (30) and is glued to the top thereof. Stacked layers of braided fibers (100) are used to reinforce the central core section (70).
    Type: Grant
    Filed: April 4, 2001
    Date of Patent: July 8, 2003
    Assignee: The Boeing Company
    Inventors: Thomas R. Cundiff, Henry H. Bennett, Brad G. Lund, Robert S. Renz, Donald E. Wright
  • Publication number: 20030090025
    Abstract: A method for forming a plurality of composite parts via resin transfer molding in a single molding cycle. The method includes the steps of using a mold having first and second mold members that cooperate to house a plurality of shims and placing a plurality of preform workpieces into the mold cavity such that at least one of the shims is disposed between each of an adjacent pair of the preform workpieces. A liquid resin is then injected into the mold cavity and subsequently cured to thereby form a cured workpiece matrix that is composed of a plurality of semi-finished composite parts and at least one shim separating the plurality of semi-finished composite parts from one another.
    Type: Application
    Filed: November 13, 2001
    Publication date: May 15, 2003
    Inventors: Karl M. Nelson, Thomas R. Cundiff, Scott A. Miller
  • Patent number: 6561478
    Abstract: The present invention relates to a seal pin indexed precisely in a resin transfer molding die to assure the desired resin-to-fiber ratio in the mold part, and, thereby, to produce reliably and consistently a part of minimum weight with adequate strength. The index/resin seal pin of the present invention for RTM mold dies is novel in that it provides the seal (via replaceable O-rings) on the threaded stem of the pin to prevent low viscosity resin from invading the threads, bolts pins, or other elements of the internal mandrel. The pin allows the entire inner mandrel to be enclosed and sealed within the mold cavity, simplifying the sealing system. The invention also relates to a method for using the seal pin in a resin transfer molding process.
    Type: Grant
    Filed: October 8, 2001
    Date of Patent: May 13, 2003
    Assignee: The Boeing Company
    Inventors: Thomas R. Cundiff, Scott A. Miller, Donald L. Conaway
  • Patent number: 6560843
    Abstract: The present invention relates to an index/seal pin indexed precisely in a resin transfer molding die to assure the desired resin-to-fiber ratio in the mold part, and, thereby, to produce reliably and consistently a part of minimum weight with adequate strength. The index/seal pin seals via replaceable O-rings on the threaded stem of the pin to prevent low viscosity resin from exiting a mold cavity and invading the threads, bolts, pins, or other elements of the internal mandrel. The pin also assures accurate positioning of a mandrel in the die cavity while it allows the entire inner mandrel to be enclosed and sealed within the mold cavity, simplifying the sealing system.
    Type: Grant
    Filed: October 8, 2001
    Date of Patent: May 13, 2003
    Assignee: The Boeing Company
    Inventors: Thomas R. Cundiff, Scott A. Miller, Donald L. Conaway
  • Publication number: 20020027310
    Abstract: The present invention relates to a seal pin indexed precisely in a resin transfer molding die to assure the desired resin-to-fiber ratio in the mold part, and, thereby, to produce reliably and consistently a part of minimum weight with adequate strength. The index/resin seal pin of the present invention for RTM mold dies is novel in that it provides the seal (via replaceable O-rings) on the threaded stem of the pin to prevent low viscosity resin from invading the threads, bolts pins, or other elements of the internal mandrel. The pin allows the entire inner mandrel to be enclosed and sealed within the mold cavity, simplifying the sealing system. The invention also relates to a method for using the seal pin in a resin transfer molding process.
    Type: Application
    Filed: October 8, 2001
    Publication date: March 7, 2002
    Inventors: Thomas R. Cundiff, Scott A. Miller, Donald L. Conaway
  • Publication number: 20020015754
    Abstract: The present invention relates to a seal pin indexed precisely in a resin transfer molding die to assure the desired resin-to-fiber ratio in the mold part, and, thereby, to produce reliably and consistently a part of minimum weight with adequate strength. The index/resin seal pin of the present invention for RTM mold dies is novel in that it provides the seal (via replaceable O-rings) on the threaded stem of the pin to prevent low viscosity resin from invading the threads, bolts pins, or other elements of the internal mandrel. The pin allows the entire inner mandrel to be enclosed and sealed within the mold cavity, simplifying the sealing system. The invention also relates to a method for using the seal pin in a resin transfer molding process.
    Type: Application
    Filed: October 8, 2001
    Publication date: February 7, 2002
    Inventors: Thomas R. Cundiff, Scott A. Miller, Donald L. Conaway
  • Publication number: 20020004115
    Abstract: A wind tunnel blade (30) connected to a base (32) and held in position by a two-piece cuff (34). The wind tunnel blade (30) is formed in a resin transfer molding process in which central, fore, and aft foam core sections (70, 72, 74) are placed together to form the wind tunnel blade (30). Radius fillers (120) are used to fill the gaps between the outer edge of the foam core sections. The radius fillers (120) used in the wind tunnel blade (30) are formed by a braided sleeve (122) surrounding a number of unidirectional tows (124). A tip (68) is formed separately from the rest of the wind tunnel blade (30) and is glued to the top thereof Stacked layers of braided fibers (100) are used to reinforce the central core section (70).
    Type: Application
    Filed: April 4, 2001
    Publication date: January 10, 2002
    Applicant: The Boeing Company
    Inventors: Thomas R.. Cundiff, Henry H. Bennett, Brad G. Lund, Robert S. Renz, Donald E. Wright