Patents by Inventor Lisa C. Carlson

Lisa C. Carlson 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: 11919261
    Abstract: There is provided an automated removal apparatus for selectively removing one or more trimmed portions of a laminated ply in a ply-by-ply fabrication process. The automated removal apparatus includes a rotatable reel having a plurality of retractable vacuum panels attached around the rotatable reel. Each retractable vacuum panel has one or more retractable vacuum pad assemblies, and each retractable vacuum pad assembly has a vacuum pad with a vacuum port and a self-sealing valve. The automated removal apparatus further includes actuator assemblies attached to the plurality of retractable vacuum panels, friction reducing elements attached around the rotatable reel, a drive assembly attached to the rotatable reel, and a pneumatic system attached to the rotatable reel and including a valve manifold operable to control an air flow to the actuator assemblies and to one or more vacuum generators to generate a vacuum flow.
    Type: Grant
    Filed: June 2, 2021
    Date of Patent: March 5, 2024
    Assignee: The Boeing Company
    Inventors: Jonathan Y. Ahn, Chace Wilcoxson, Lisa C. Carlson, Gregory R. Klempel, Austin T. McAnelly, Deborah A. Fisher, Scott E. Krajca
  • Patent number: 11426971
    Abstract: A composite structure including a composite body having an outer surface, wherein the composite body is elongated along a span axis, and a detection layer connected to the outer surface of the composite body, the detection layer including a plurality of strips, wherein each strip comprises a plurality of glass fibers embedded in a matrix material, is elongated along a detection axis, the detection axis being substantially aligned with the span axis, and is spaced a non-zero distance apart from adjacent strips such that a discontinuity is defined between adjacent strips.
    Type: Grant
    Filed: October 31, 2018
    Date of Patent: August 30, 2022
    Assignee: The Boeing Company
    Inventors: Hyukbong Kwon, Khanh Mai Pham, Lisa C. Carlson, Garrett C. Hanson
  • Publication number: 20210394466
    Abstract: There is provided an automated removal apparatus for selectively removing one or more trimmed portions of a laminated ply in a ply-by-ply fabrication process. The automated removal apparatus includes a rotatable reel having a plurality of retractable vacuum panels attached around the rotatable reel. Each retractable vacuum panel has one or more retractable vacuum pad assemblies, and each retractable vacuum pad assembly has a vacuum pad with a vacuum port and a self-sealing valve. The automated removal apparatus further includes actuator assemblies attached to the plurality of retractable vacuum panels, friction reducing elements attached around the rotatable reel, a drive assembly attached to the rotatable reel, and a pneumatic system attached to the rotatable reel and including a valve manifold operable to control an air flow to the actuator assemblies and to one or more vacuum generators to generate a vacuum flow.
    Type: Application
    Filed: June 2, 2021
    Publication date: December 23, 2021
    Inventors: Jonathan Y. Ahn, Chace Wilcoxson, Lisa C . Carlson, Gregory R. Klempel, Austin T. McAnelly, Deborah A. Fisher, Scott E. Krajca
  • Patent number: 11059242
    Abstract: An apparatus is provided for forming a pleat of a vacuum bag into position over a stringer of an uncured skin panel. The apparatus comprises a leading shoe and a trailing shoe that cooperates with the leading shoe to form the pleat of the vacuum bag. The apparatus also comprises at least one roller assembly for compacting the formed pleat into position over the stringer.
    Type: Grant
    Filed: March 30, 2018
    Date of Patent: July 13, 2021
    Assignee: The Boeing Company
    Inventors: Steven J. McAllister, Lisa C Carlson, Garrett C. Hanson, Kanna M. Pham
  • Patent number: 10814568
    Abstract: An example method for forming a flat composite charge into a composite blade stiffener includes cutting a flat composite charge along a cut line into a first piece and a second piece having an angle, positioning the first piece and the second piece of the flat composite charge on a forming mandrel about a tooling plunger, activating the tooling plunger to drive the first piece and the second piece into a cavity of the forming mandrel resulting in the first piece and the second piece folding at the cut line, withdrawing the tooling plunger from the cavity of the forming mandrel, compressing the forming mandrel to apply a lateral pressure to the first piece and the second piece folded into the cavity, and applying a vertical pressure to a first flange and a second flange of the first piece and the second piece, respectively, to form the composite blade stiffener.
    Type: Grant
    Filed: July 15, 2019
    Date of Patent: October 27, 2020
    Assignee: The Boeing Company
    Inventors: Lisa C. Carlson, Kanna M. Pham, Joseph L. Sweetin, Garrett C. Hanson, Jake A. Reeves, Chilip Chan, Kiet Nguyen
  • Publication number: 20190337242
    Abstract: An example method for forming a flat composite charge into a composite blade stiffener includes cutting a flat composite charge along a cut line into a first piece and a second piece having an angle, positioning the first piece and the second piece of the flat composite charge on a forming mandrel about a tooling plunger, activating the tooling plunger to drive the first piece and the second piece into a cavity of the forming mandrel resulting in the first piece and the second piece folding at the cut line, withdrawing the tooling plunger from the cavity of the forming mandrel, compressing the forming mandrel to apply a lateral pressure to the first piece and the second piece folded into the cavity, and applying a vertical pressure to a first flange and a second flange of the first piece and the second piece, respectively, to form the composite blade stiffener.
    Type: Application
    Filed: July 15, 2019
    Publication date: November 7, 2019
    Inventors: Lisa C. Carlson, Kanna M. Pham, Joseph L. Sweetin, Garrett C. Hanson, Jake A. Reeves, Chilip Chan, Kiet Nguyen
  • Publication number: 20190299544
    Abstract: An apparatus is provided for forming a pleat of a vacuum bag into position over a stringer of an uncured skin panel. The apparatus comprises a leading shoe and a trailing shoe that cooperates with the leading shoe to form the pleat of the vacuum bag. The apparatus also comprises at least one roller assembly for compacting the formed pleat into position over the stringer.
    Type: Application
    Filed: March 30, 2018
    Publication date: October 3, 2019
    Applicant: The Boeing Company
    Inventors: Steven J. McAllister, Lisa C Carlson, Garrett C. Hanson, Kanna M. Pham
  • Publication number: 20190061310
    Abstract: A composite structure including a composite body having an outer surface and including a web portion having a proximal portion and a distal portion, and a base portion connected to the proximal portion of the web portion, wherein the composite body is elongated along a span axis, and a detection layer connected to the outer surface of the composite body at the distal portion of the web portion of the composite body, the detection layer including a plurality of glass fibers embedded in a first matrix material, wherein the composite body includes a plurality of carbon fibers embedded in a second matrix material, and wherein the outer surface of the composite body subjacent the detection layer is substantially free of exposed carbon fibers of the plurality of carbon fibers.
    Type: Application
    Filed: October 31, 2018
    Publication date: February 28, 2019
    Applicant: The Boeing Company
    Inventors: Hyukbong Kwon, Khanh Mai Pham, Lisa C. Carlson, Garrett C. Hanson
  • Publication number: 20190061309
    Abstract: A composite structure including a composite body having an outer surface, wherein the composite body is elongated along a span axis, and a detection layer connected to the outer surface of the composite body, the detection layer including a plurality of strips, wherein each strip comprises a plurality of glass fibers embedded in a matrix material, is elongated along a detection axis, the detection axis being substantially aligned with the span axis, and is spaced a non-zero distance apart from adjacent strips such that a discontinuity is defined between adjacent strips.
    Type: Application
    Filed: October 31, 2018
    Publication date: February 28, 2019
    Applicant: The Boeing Company
    Inventors: Hyukbong Kwon, Khanh Mai Pham, Lisa C. Carlson, Garrett C. Hanson
  • Patent number: 10071506
    Abstract: A vacuum bagging system may include a layer assembly defining a fluid flow channel. The layer assembly may include a contact layer mounted to a composite part positionable within an outer mold line (OML) tool. The contact layer may have a contact layer width defined by opposing contact layer side edges. The layer assembly may further include an inner layer mounted to the contact layer and having inner layer side edges located between the contact layer side edges. The fluid flow channel may extend along at least a portion of the composite part to at least one part end. The vacuum bagging system may include an internal vacuum bag positionable against the inner layer. An inner mold line (IML) tool may support the internal vacuum bag. The contact layer width may be less than an IML tool width.
    Type: Grant
    Filed: October 29, 2015
    Date of Patent: September 11, 2018
    Assignee: The Boeing Company
    Inventors: Brett I. Lyons, Lisa C. Carlson, Stanley W. Stawski, Robert B. Miller, Matt Wallen, Jens Rossfeldt
  • Publication number: 20160046041
    Abstract: A vacuum bagging system may include a layer assembly defining a fluid flow channel. The layer assembly may include a contact layer mounted to a composite part positionable within an outer mold line (OML) tool. The contact layer may have a contact layer width defined by opposing contact layer side edges. The layer assembly may further include an inner layer mounted to the contact layer and having inner layer side edges located between the contact layer side edges. The fluid flow channel may extend along at least a portion of the composite part to at least one part end. The vacuum bagging system may include an internal vacuum bag positionable against the inner layer. An inner mold line (IML) tool may support the internal vacuum bag. The contact layer width may be less than an IML tool width.
    Type: Application
    Filed: October 29, 2015
    Publication date: February 18, 2016
    Inventors: Brett I. Lyons, Lisa C. Carlson, Stanley W. Stawski, Robert B. Miller, Matt Wallen, Jens Rossfeldt
  • Patent number: 9199419
    Abstract: A vacuum bagging system may include a layer assembly defining a fluid flow channel. The layer assembly may include a contact layer mounted to a composite part positionable within an outer mold line (OML) tool. The contact layer may have a contact layer width defined by opposing contact layer side edges. The layer assembly may further include an inner layer mounted to the contact layer and having inner layer side edges located between the contact layer side edges. The fluid flow channel may extend along at least a portion of the composite part to at least one part end. The vacuum bagging system may include an internal vacuum bag positionable against the inner layer. An inner mold line (IML) tool may support the internal vacuum bag. The contact layer width may be less than an IML tool width.
    Type: Grant
    Filed: October 31, 2012
    Date of Patent: December 1, 2015
    Assignee: The Boeing Company
    Inventors: Brett I. Lyons, Lisa C. Carlson, Stanley W. Stawski, Robert B. Miller, Matt Wallen, Jens Rossfeldt