Patents by Inventor Steven F. Hanson
Steven F. Hanson 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: 8702417Abstract: Tooling aids for applying pressure in laminating, and methods for their use, are described herein. In one embodiment, a caul for applying pressure in laminating includes a base portion positioned between first and second corner portions. The base portion can have a curved shape when it is in a relaxed state, but it moves to a flatter shape when subjected to pressure during lamination. Movement of the base portion to the flatter shape causes the first and second corner portions to move outwardly and away from the base portion. In this manner, the caul can be used to compact laminating materials into corner regions of a corresponding female mold surface.Type: GrantFiled: April 20, 2011Date of Patent: April 22, 2014Assignee: The Boeing CompanyInventor: Steven F. Hanson
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Patent number: 8394310Abstract: An inflatable compaction tool for consolidating a composite material inside a faceted hollow or tubular mold for a composite part is made from an elastic material. The compaction tool includes relatively flat wall segments conjoined by corner segments that define a sealed chamber. The wall segments curve away from the mold surface toward the midpoint of each wall segment, so that as a pressurized fluid is introduced into the compaction tool, a component of the force exerted on the tool interior surface is transmitted through the wall segments toward the corner segments. Thus, during initial inflation, the corner segments are forced toward the corner regions of the mold before the wall segments contact the composite material, firmly compressing the composite material into the corner regions of the mold before the friction of the wall segments against the composite material inhibits expansion of the corner segments into the mold corner regions.Type: GrantFiled: October 15, 2010Date of Patent: March 12, 2013Assignee: The Boeing CompanyInventors: Steven F. Hanson, Amitabh Vyas
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Patent number: 8158051Abstract: An intermediate sealing element and method for unsealing a vacuum membrane from one tool surface and transferring it to another tool surface without damaging the vacuum membrane. The intermediate sealing element forms a continuous path around the periphery of a vacuum membrane and is sealed directly to one or more vacuum membranes and a tool surface using any means known in the art to create an airtight seal between two surfaces. The intermediate sealing element is able to withstand high temperatures and high pressure without altering its structural characteristics. Because of its durability, the intermediate sealing element can be removed from the tool surface without tearing or elongating, subsequently allowing the vacuum membranes to be detached from the tool surface without tearing or elongating.Type: GrantFiled: May 7, 2008Date of Patent: April 17, 2012Assignee: Spirit AeroSystems, Inc.Inventors: Steven F. Hanson, Jeffrey W. Priest, Carl R. Fiegenbaum, Kelvin D. Nguyen
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Publication number: 20110195230Abstract: Tooling aids for applying pressure in laminating, and methods for their use, are described herein. In one embodiment, a caul for applying pressure in laminating includes a base portion positioned between first and second corner portions. The base portion can have a curved shape when it is in a relaxed state, but it moves to a flatter shape when subjected to pressure during lamination. Movement of the base portion to the flatter shape causes the first and second corner portions to move outwardly and away from the base portion. In this manner, the caul can be used to compact laminating materials into corner regions of a corresponding female mold surface.Type: ApplicationFiled: April 20, 2011Publication date: August 11, 2011Applicant: THE BOEING COMPANYInventor: Steven F. Hanson
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Patent number: 7951318Abstract: Tooling aids for applying pressure in laminating, and methods for their use, are described herein. In one embodiment, a caul for applying pressure in laminating includes a base portion positioned between first and second corner portions. The base portion can have a curved shape when it is in a relaxed state, but it moves to a flatter shape when subjected to pressure during lamination. Movement of the base portion to the flatter shape causes the first and second corner portions to move outwardly and away from the base portion. In this manner, the caul can be used to compact laminating materials into corner regions of a corresponding female mold surface.Type: GrantFiled: October 29, 2007Date of Patent: May 31, 2011Assignee: The Boeing CompanyInventor: Steven F. Hanson
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Publication number: 20110027405Abstract: An inflatable compaction tool for consolidating a composite material inside a faceted hollow or tubular mold for a composite part is made from an elastic material. The compaction tool includes relatively flat wall segments conjoined by corner segments that define a sealed chamber. The wall segments curve away from the mold surface toward the midpoint of each wall segment, so that as a pressurized fluid is introduced into the compaction tool, a component of the force exerted on the tool interior surface is transmitted through the wall segments toward the corner segments. Thus, during initial inflation, the corner segments are forced toward the corner regions of the mold before the wall segments contact the composite material, firmly compressing the composite material into the corner regions of the mold before the friction of the wall segments against the composite material inhibits expansion of the corner segments into the mold corner regions.Type: ApplicationFiled: October 15, 2010Publication date: February 3, 2011Applicant: THE BOEING COMPANYInventors: Steven F. Hanson, Amitabh Vyas
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Patent number: 7824171Abstract: An inflatable compaction tool for consolidating a composite material inside a faceted hollow or tubular mold for a composite part is made from an elastic material. The compaction tool includes relatively flat wall segments conjoined by corner segments that define a sealed chamber. The wall segments curve away from the mold surface toward the midpoint of each wall segment, so that as a pressurized fluid is introduced into the compaction tool, a component of the force exerted on the tool interior surface is transmitted through the wall segments toward the corner segments. Thus, during initial inflation, the corner segments are forced toward the corner regions of the mold before the wall segments contact the composite material, firmly compressing the composite material into the corner regions of the mold before the friction of the wall segments against the composite material inhibits expansion of the corner segments into the mold corner regions.Type: GrantFiled: October 31, 2005Date of Patent: November 2, 2010Assignee: The Boeing CompanyInventors: Steven F. Hanson, Amitabh Vyas
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Patent number: 7648661Abstract: A system and method for making and using a reconfigurable composite part mandrel operable in the manufacture of composite parts. The system may comprise an assembly fixture, a generic mandrel, a reconfigurable simulated skin, a reconfigurable frame portion, and state-changing material operable to harden into a desired configuration for forming a particular composite part. The method of forming and using the reconfigurable composite part mandrel may comprise: inserting the simulated skin within the assembly fixture, inserting or assembling the frame portion within the assembly fixture; inserting the generic mandrel into the assembly fixture; filling a cavity between the generic mandrel and the assembly fixture with the state-changing mixture to encapsulate the frame portion; hardening the state-changing mixture; and removing the assembly fixture and the simulated skin.Type: GrantFiled: August 22, 2008Date of Patent: January 19, 2010Assignee: Spirit Aerosystems, Inc.Inventor: Steven F. Hanson
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Publication number: 20090278319Abstract: An intermediate sealing element and method for unsealing a vacuum membrane from one tool surface and transferring it to another tool surface without damaging the vacuum membrane. The intermediate sealing element forms a continuous path around the periphery of a vacuum membrane and is sealed directly to one or more vacuum membranes and a tool surface using any means known in the art to create an airtight seal between two surfaces. The intermediate sealing element is able to withstand high temperatures and high pressure without altering its structural characteristics. Because of its durability, the intermediate sealing element can be removed from the tool surface without tearing or elongating, subsequently allowing the vacuum membranes to be detached from the tool surface without tearing or elongating.Type: ApplicationFiled: May 7, 2008Publication date: November 12, 2009Applicant: Spirit AeroSystems, Inc.Inventors: Steven F. Hanson, Jeffrey W. Priest, Carl R. Fiegenbaum, Kelvin D. Nguyen
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Publication number: 20090051069Abstract: A system and method for making and using a reconfigurable composite part mandrel operable in the manufacture of composite parts. The system may comprise an assembly fixture, a generic mandrel, a reconfigurable simulated skin, a reconfigurable frame portion, and state-changing material operable to harden into a desired configuration for forming a particular composite part. The method of forming and using the reconfigurable composite part mandrel may comprise: inserting the simulated skin within the assembly fixture, inserting or assembling the frame portion within the assembly fixture; inserting the generic mandrel into the assembly fixture; filling a cavity between the generic mandrel and the assembly fixture with the state-changing mixture to encapsulate the frame portion; hardening the state-changing mixture; and removing the assembly fixture and the simulated skin.Type: ApplicationFiled: August 22, 2008Publication date: February 26, 2009Applicant: SPIRIT AEROSYSTEMS, INC.Inventor: Steven F. Hanson
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Patent number: 7306450Abstract: Tooling aids for applying pressure in laminating, and methods for their use, are described herein. In one embodiment, a caul for applying pressure in laminating includes a base portion positioned between first and second corner portions. The base portion can have a curved shape when it is in a relaxed state, but it moves to a flatter shape when subjected to pressure during lamination. Movement of the base portion to the flatter shape causes the first and second corner portions to move outwardly and away from the base portion. In this manner, the caul can be used to compact laminating materials into corner regions of a corresponding female mold surface.Type: GrantFiled: September 29, 2004Date of Patent: December 11, 2007Assignee: The Boeing CompanyInventor: Steven F. Hanson
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Patent number: 6291743Abstract: The invention involves production of transgenic plants containing DNA encoding AC1/C1 wildtype and mutant sequences that negatively interfere in trans with geminiviral replication during infection. The transgenic plants produced by the invention are resistant to viral infection.Type: GrantFiled: April 15, 1997Date of Patent: September 18, 2001Assignees: Seminis Vegetable Seeds, Inc., Wisconsin Alymni Research Foundation, Regents of the University of CaliforniaInventors: John T. Stout, Hang T. Luu, Steven F. Hanson, Douglas P. Maxwell, Paul G. Ahlquist, Robert L. Gilbertson
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Publication number: 20010011379Abstract: The invention involves production of transgenic plants containing DNA encoding AC1/C1 wildtype and mutant sequences that negatively interfere in trans with geminiviral replication during infection. The transgenic plants produced by the invention are resistant to viral infection.Type: ApplicationFiled: April 15, 1997Publication date: August 2, 2001Inventors: JOHN T. STOUT, HANG T. LUU, STEVEN F. HANSON, DOUGLAS P. MAXWELL, PAUL G. AHLQUIST, ROBERT L. GILBERTSON