Patents by Inventor Kenneth L. Brook
Kenneth L. Brook 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).
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Patent number: 10308344Abstract: 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: GrantFiled: May 11, 2017Date of Patent: June 4, 2019Assignee: The Boeing CompanyInventors: Lyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
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Publication number: 20170246830Abstract: 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: ApplicationFiled: May 11, 2017Publication date: August 31, 2017Applicant: The Boeing CompanyInventors: Lyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
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Patent number: 9676470Abstract: 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: GrantFiled: March 9, 2015Date of Patent: June 13, 2017Assignee: The Boeing CompanyInventors: Lyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
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Patent number: 9382014Abstract: The disclosure provides in one embodiment for a vent dam for use in a vent stringer in a fuel vent system. The vent dam is configured to mount to and within the vent stringer The vent dam has a contoured guiding surface for guiding fuel flow into and out of an interior of the vent stringer, wherein the vent dam, the vent stringer, and a tube attached to the vent stringer are in fluid communication with one or more fuel tanks. The vent dam further has one or more side flanges extending from the contoured guiding surface for providing attachment of the vent dam to one or more interior portions of the vent stringer, wherein the contoured guiding surface and the one or more side flanges are formed as one piece.Type: GrantFiled: February 28, 2015Date of Patent: July 5, 2016Assignee: The Boeing CompanyInventors: Kenneth L. Brook, Bonnie A. Keefe
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Patent number: 9138919Abstract: A collapsible bladder has flexible outer walls and at least one strut inside the enclosure. The strut is connected to the outer walls and controls the shape into which the enclosure may be collapsed.Type: GrantFiled: July 8, 2014Date of Patent: September 22, 2015Assignee: THE BOEING COMPANYInventors: John D. Morris, Michael A. Lee, Kenneth L. Brook
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Publication number: 20150239570Abstract: The disclosure provides in one embodiment for a vent dam for use in a vent stringer in a fuel vent system. The vent dam is configured to mount to and within the vent stringer The vent dam has a contoured guiding surface for guiding fuel flow into and out of an interior of the vent stringer, wherein the vent dam, the vent stringer, and a tube attached to the vent stringer are in fluid communication with one or more fuel tanks. The vent dam further has one or more side flanges extending from the contoured guiding surface for providing attachment of the vent dam to one or more interior portions of the vent stringer, wherein the contoured guiding surface and the one or more side flanges are formed as one piece.Type: ApplicationFiled: February 28, 2015Publication date: August 27, 2015Inventors: Kenneth L. Brook, Bonnie A. Keefe
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Publication number: 20150175250Abstract: 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: ApplicationFiled: March 9, 2015Publication date: June 25, 2015Inventors: Lyle R. Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth J. Duffie, Gregory B. Doty
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Patent number: 9061754Abstract: A structure may comprise a skin member and a hat stringer. The hat stringer may include a base portion and first and second webs extending outwardly from the base portion. The first and second webs may be formed of a wrap laminate having wrap plies and a cover laminate having cover plies. The first and second webs may be interconnected by a cap. The hat stringer and skin member may be co-cured.Type: GrantFiled: January 2, 2014Date of Patent: June 23, 2015Assignee: The Boeing CompanyInventors: Donald P. Matheson, Kenneth L. Brook
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Patent number: 9010689Abstract: The disclosure provides in one embodiment for a vent dam for use in a vent stringer in a fuel vent system. The vent dam comprises a contoured guiding surface for guiding fluid flow in a vent stringer. The vent dam further comprises one or more side flanges extending from the contoured guiding surface for providing attachment of the vent dam within the vent stringer.Type: GrantFiled: January 4, 2010Date of Patent: April 21, 2015Assignee: The Boeing CompanyInventors: Kenneth L. Brook, Bonnie Keefe
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Patent number: 8974886Abstract: 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: GrantFiled: April 25, 2012Date of Patent: March 10, 2015Assignee: The Boeing CompanyInventors: Lyle Ray Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth John DuffiƩ, Gregory B. Doty
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Publication number: 20140322382Abstract: A collapsible bladder has flexible outer walls and at least one strut inside the enclosure. The strut is connected to the outer walls and controls the shape into which the enclosure may be collapsed.Type: ApplicationFiled: July 8, 2014Publication date: October 30, 2014Inventors: John D. Morris, Michael A. Lee, Kenneth L. Brook
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Patent number: 8800953Abstract: A collapsible bladder has flexible outer walls and at least one strut inside the enclosure. The strut is connected to the outer walls and controls the shape into which the enclosure may be collapsed.Type: GrantFiled: September 25, 2012Date of Patent: August 12, 2014Assignee: The Boeing CompanyInventors: John D. Morris, Michael A. Lee, Kenneth L. Brook
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Patent number: 8746618Abstract: A stringer comprises a base portion and first and second webs extending outwardly from the base portion. The orientation of at least one of the first and second webs may transition from a first angle to a second angle within an angle transition zone.Type: GrantFiled: October 30, 2011Date of Patent: June 10, 2014Assignee: The Boeing CompanyInventors: Kenneth L. Brook, Niraj Patel, John D. Morris, Michael A. Lee
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Patent number: 8714485Abstract: A structure may comprise a skin member and a hat stringer. The hat stringer may include a base portion and first and second webs extending outwardly from the base portion. Each one of the first and second webs may be comprised of a wrap laminate having wrap plies and a cover laminate having cover plies. The first and second webs may be interconnected by a cap. The hat stringer and skin member may be co-cured.Type: GrantFiled: December 15, 2009Date of Patent: May 6, 2014Assignee: The Boeing CompanyInventors: Donald P. Matheson, Kenneth L. Brook
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Publication number: 20140120318Abstract: A structure may comprise a skin member and a hat stringer. The hat stringer may include a base portion and first and second webs extending outwardly from the base portion. The first and second webs may be formed of a wrap laminate having wrap plies and a cover laminate having cover plies. The first and second webs may be interconnected by a cap. The hat stringer and skin member may be co-cured.Type: ApplicationFiled: January 2, 2014Publication date: May 1, 2014Applicant: THE BOEING COMPANYInventors: Donald P. Matheson, Kenneth L. Brook
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Publication number: 20130287995Abstract: 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: ApplicationFiled: April 25, 2012Publication date: October 31, 2013Inventors: Lyle Ray Deobald, Kenneth L. Brook, Timothy D. Jackson, Kenneth John DuffiƩ, Gregory B. Doty
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Patent number: 8293051Abstract: A collapsible bladder has flexible outer walls and at least one strut inside the enclosure. The strut is connected to the outer walls and controls the shape into which the enclosure may be collapsed.Type: GrantFiled: December 10, 2008Date of Patent: October 23, 2012Assignee: The Boeing CompanyInventors: John D. Morris, Michael A. Lee, Kenneth L. Brook
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Publication number: 20120045609Abstract: A stringer comprises a base portion and first and second webs extending outwardly from the base portion. The orientation of at least one of the first and second webs may transition from a first angle to a second angle within an angle transition zone.Type: ApplicationFiled: October 30, 2011Publication date: February 23, 2012Applicant: THE BOEING COMPANYInventors: Kenneth L. Brook, Niraj Patel, John D. Morris, Michael A. Lee
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Patent number: 8074694Abstract: A stringer comprises a base portion and first and second webs extending outwardly from the base portion. The orientation of at least one of the first and second webs may transition from a first angle to a second angle within an angle transition zone.Type: GrantFiled: May 28, 2009Date of Patent: December 13, 2011Assignee: The Boeing CompanyInventors: Kenneth L. Brook, Niraj Patel, John D. Morris, Michael A. Lee
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Publication number: 20110139932Abstract: A structure may comprise a skin member and a hat stringer. The hat stringer may include a base portion and first and second webs extending outwardly from the base portion. Each one of the first and second webs may be comprised of a wrap laminate having wrap plies and a cover laminate having cover plies. The first and second webs may be interconnected by a cap. The hat stringer and skin member may be co-cured.Type: ApplicationFiled: December 15, 2009Publication date: June 16, 2011Applicant: THE BOEING COMPANYInventors: Donald P. Matheson, Kenneth L. Brook