Patents by Inventor Panagiotis E. George

Panagiotis E. George 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: 11383503
    Abstract: Disclosed herein is a composite sandwich panel that includes a first face portion with fully consolidated comingled first fibers and a first thermoplastic matrix. The composite sandwich panel also includes a second face portion with fully consolidated comingled second fibers and a second thermoplastic matrix. Additionally, the composite sandwich panel includes at least one core portion with partially consolidated comingled third fibers and a third thermoplastic matrix. The at least one core portion is interposed between the first and second face portions. The first thermoplastic matrix is melded with the third thermoplastic matrix and the second thermoplastic matrix is melded with the third thermoplastic. A density of the fibers across a thickness of the composite panel is non-uniform.
    Type: Grant
    Filed: December 17, 2019
    Date of Patent: July 12, 2022
    Assignee: The Boeing Company
    Inventors: Hardik Dalal, Panagiotis E. George, Kelsi M. Hurley, Ashley C. Tracey
  • Patent number: 11377535
    Abstract: Methods and compositions for depolymerizing the polymer component of fiber reinforced polymers to facilitate the recovery of free fibers.
    Type: Grant
    Filed: March 9, 2020
    Date of Patent: July 5, 2022
    Assignee: The Boeing Company
    Inventors: Adam F. Gross, John J. Vajo, Ashley M. Nelson, April R. Rodriguez, Hardik Dalal, Panagiotis E. George
  • Publication number: 20200207940
    Abstract: Methods and compositions for depolymerizing the polymer component of fiber reinforced polymers to facilitate the recovery of free fibers.
    Type: Application
    Filed: March 9, 2020
    Publication date: July 2, 2020
    Inventors: Adam F. Gross, John J. Vajo, Ashley M. Nelson, April R. Rodriguez, Hardik Dalal, Panagiotis E. George
  • Publication number: 20200122442
    Abstract: Disclosed herein is a composite sandwich panel that includes a first face portion with fully consolidated comingled first fibers and a first thermoplastic matrix. The composite sandwich panel also includes a second face portion with fully consolidated comingled second fibers and a second thermoplastic matrix. Additionally, the composite sandwich panel includes at least one core portion with partially consolidated comingled third fibers and a third thermoplastic matrix. The at least one core portion is interposed between the first and second face portions. The first thermoplastic matrix is melded with the third thermoplastic matrix and the second thermoplastic matrix is melded with the third thermoplastic. A density of the fibers across a thickness of the composite panel is non-uniform.
    Type: Application
    Filed: December 17, 2019
    Publication date: April 23, 2020
    Inventors: Hardik Dalal, Panagiotis E. George, Kelsi M. Hurley, Ashley C. Tracey
  • Patent number: 10611892
    Abstract: Methods and compositions for depolymerizing the polymer component of fiber reinforced polymers to facilitate the recovery of free fibers.
    Type: Grant
    Filed: April 7, 2017
    Date of Patent: April 7, 2020
    Assignee: The Boeing Company
    Inventors: Adam F. Gross, John J. Vajo, Ashley M. Nelson, April R. Rodriguez, Hardik Dalal, Panagiotis E. George
  • Patent number: 10543666
    Abstract: Disclosed herein is a composite sandwich panel that includes a first face portion with fully consolidated comingled first fibers and a first thermoplastic matrix. The composite sandwich panel also includes a second face portion with fully consolidated comingled second fibers and a second thermoplastic matrix. Additionally, the composite sandwich panel includes at least one core portion with partially consolidated comingled third fibers and a third thermoplastic matrix. The at least one core portion is interposed between the first and second face portions. The first thermoplastic matrix is melded with the third thermoplastic matrix and the second thermoplastic matrix is melded with the third thermoplastic. A density of the fibers across a thickness of the composite panel is non-uniform.
    Type: Grant
    Filed: June 29, 2015
    Date of Patent: January 28, 2020
    Assignee: The Boeing Company
    Inventors: Hardik Dalal, Panagiotis E. George, Kelsi M. Hurley, Ashley C. Tracey
  • Patent number: 10286577
    Abstract: A composite mandrel includes a generally elongated mandrel body comprising a resilient mandrel core and an elastomeric mandrel outer layer disposed outside the mandrel core. A method for fabricating a contoured stiffened composite panel is also disclosed.
    Type: Grant
    Filed: May 2, 2016
    Date of Patent: May 14, 2019
    Assignee: The Boeing Company
    Inventors: Brian G. Robins, Daniel M. Rotter, Todd J. Washburn, Panagiotis E. George
  • Publication number: 20180291174
    Abstract: Methods and compositions for depolymerizing the polymer component of fiber reinforced polymers to facilitate the recovery of free fibers.
    Type: Application
    Filed: April 7, 2017
    Publication date: October 11, 2018
    Inventors: Adam F. Gross, John J. Vajo, Ashley M. Nelson, April R. Rodriguez, Hardik Dalal, Panagiotis E. George
  • Publication number: 20160375661
    Abstract: Disclosed herein is a composite sandwich panel that includes a first face portion with fully consolidated comingled first fibers and a first thermoplastic matrix. The composite sandwich panel also includes a second face portion with fully consolidated comingled second fibers and a second thermoplastic matrix. Additionally, the composite sandwich panel includes at least one core portion with partially consolidated comingled third fibers and a third thermoplastic matrix. The at least one core portion is interposed between the first and second face portions. The first thermoplastic matrix is melded with the third thermoplastic matrix and the second thermoplastic matrix is melded with the third thermoplastic. A density of the fibers across a thickness of the composite panel is non-uniform.
    Type: Application
    Filed: June 29, 2015
    Publication date: December 29, 2016
    Inventors: Hardik Dalal, Panagiotis E. George, Kelsi M. Hurley, Ashley C. Tracey
  • Publication number: 20160243730
    Abstract: A composite mandrel includes a generally elongated mandrel body comprising a resilient mandrel core and an elastomeric mandrel outer layer disposed outside the mandrel core. A method for fabricating a contoured stiffened composite panel is also disclosed.
    Type: Application
    Filed: May 2, 2016
    Publication date: August 25, 2016
    Inventors: Brian G. Robins, Daniel M. Rotter, Todd J. Washburn, Panagiotis E. George
  • Patent number: 9327467
    Abstract: A composite mandrel includes a generally elongated mandrel body comprising a resilient mandrel core and an elastomeric mandrel outer layer disposed outside the mandrel core. A method for fabricating a contoured stiffened composite panel is also disclosed.
    Type: Grant
    Filed: July 10, 2008
    Date of Patent: May 3, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Brian G. Robins, Daniel M. Rotter, Todd J. Washburn, Panagiotis E. George
  • Publication number: 20140083155
    Abstract: A method for consolidating a preform made of composite material. The preform and a compliant metal alloy sheet are placed between less compliant matched confronting forming/molding surfaces with the preform being sandwiched between the metal alloy sheet and a matched confronting surface. The matched confronting surfaces and compliant metal alloy sheet are heated until the preform reaches at least its consolidation temperature. During heating, force is applied so that the matched confronting surfaces exert sufficient compressive force on the preform and metal alloy sheet to cause the composite material to consolidate at the consolidation temperature. The metal alloy sheet has a tensile yield point in a range of 25-300 psi at the consolidation temperature at a strain rate of about 1% to 10% strain per minute.
    Type: Application
    Filed: September 24, 2012
    Publication date: March 27, 2014
    Applicant: THE BOEING COMPANY
    Inventors: Marc R. Matsen, Erika L. Carter, Panagiotis E. George
  • Patent number: 8044354
    Abstract: In one embodiment, a method of classifying a polymer containing surface is provided including collecting one or more spectra of infrared energy reflected from the surface over a spectrum of wavelengths; performing multivariate processing at one or more wavelengths; comparing results of the multivariate processing with one or more predetermined material classification models derived from model material infrared energy spectra collected from one or more model material surfaces, the one or more model material surfaces each having a known polymer material composition; and, sorting the polymer containing surface into the proper class based on a similarity of the results of the multivariate processing at one or more wavelengths with the predetermined material classification models.
    Type: Grant
    Filed: December 4, 2008
    Date of Patent: October 25, 2011
    Assignee: The Boeing Company
    Inventors: Gregory J. Werner, Paul H. Shelley, Panagiotis E. George
  • Publication number: 20100140476
    Abstract: In one embodiment, a method of classifying a polymer containing surface is provided including collecting one or more spectra of infrared energy reflected from the surface over a spectrum of wavelengths; performing multivariate processing at one or more wavelengths; comparing results of the multivariate processing with one or more predetermined material classification models derived from model material infrared energy spectra collected from one or more model material surfaces, the one or more model material surfaces each having a known polymer material composition; and, sorting the polymer containing surface into the proper class based on a similarity of the results of the multivariate processing at one or more wavelengths with the predetermined material classification models.
    Type: Application
    Filed: December 4, 2008
    Publication date: June 10, 2010
    Inventors: Gregory J. Werner, Paul H. Shelley, Panagiotis E. George
  • Publication number: 20100006739
    Abstract: A composite mandrel includes a generally elongated mandrel body comprising a resilient mandrel core and an elastomeric mandrel outer layer disposed outside the mandrel core. A method for fabricating a contoured stiffened composite panel is also disclosed.
    Type: Application
    Filed: July 10, 2008
    Publication date: January 14, 2010
    Inventors: Brian G. Robins, Daniel M. Rotter, Todd J. Washburn, Panagiotis E. George
  • Patent number: 7138031
    Abstract: An apparatus and method for retaining composite structures, such as composite honeycomb structures, during manufacture are provided. The composite structure is cured on a mandrel that defines a layup surface with a grip feature. The grip feature is configured to engage the composite structure during manufacture and retain the structure in a predetermined configuration. A film adhesive can be provided between the grip feature and a tiedown ply that extends from the composite structure.
    Type: Grant
    Filed: September 9, 2003
    Date of Patent: November 21, 2006
    Assignee: The Boeing Company
    Inventors: Dave G. Erickson, Panagiotis E. George, Ryan C. Mortensen, Stuart A. Smith
  • Patent number: 6709538
    Abstract: A laminated composite (multi-ply) radius filler includes a plurality of woven fabric reinforced plies cut to fill a radius gap (including, if appropriate, intentional overfill) to increase absolute strength, to increase specific strength, or to reduce cost by reducing cracking and distortion in the radius of a composite assembly. The present invention also describes the method of manufacture and method of use for such laminated composite radius filler.
    Type: Grant
    Filed: May 21, 2002
    Date of Patent: March 23, 2004
    Assignee: The Boeing Company
    Inventors: Panagiotis E. George, Kirk B. Kajita, Barry P. Van West
  • Patent number: 6689448
    Abstract: A laminated composite (multi-ply) radius filler includes a plurality of woven fabric reinforced plies cut to fill a radius gap (including, if appropriate, intentional overfill) to increase absolute strength, to increase specific strength, or to reduce cost by reducing cracking and distortion in the radius of a composite assembly. The present invention also describes the method of manufacture and method of use for such laminated composite radius filler.
    Type: Grant
    Filed: May 21, 2002
    Date of Patent: February 10, 2004
    Assignee: The Boeing Company
    Inventors: Panagiotis E. George, Kirk B. Kajita, Barry P. Van West
  • Patent number: 6562436
    Abstract: A laminated composite (multi-ply) radius filler includes a plurality of woven fabric reinforced plies cut to fill a radius gap (including, if appropriate, intentional overfill) to increase absolute strength, to increase specific strength, or to reduce cost by reducing cracking and distortion in the radius of a composite assembly. The present invention also describes the method of manufacture and method of use for such laminated composite radius filler.
    Type: Grant
    Filed: February 23, 2001
    Date of Patent: May 13, 2003
    Assignee: The Boeing Company
    Inventors: Panagiotis E. George, Kirk B. Kajita, Barry P. Van West
  • Publication number: 20030044570
    Abstract: A laminated composite (multi-ply) radius filler includes a plurality of woven fabric reinforced plies cut to fill a radius gap (including, if appropriate, intentional overfill) to increase absolute strength, to increase specific strength, or to reduce cost by reducing cracking and distortion in the radius of a composite assembly. The present invention also describes the method of manufacture and method of use for such laminated composite radius filler.
    Type: Application
    Filed: May 21, 2002
    Publication date: March 6, 2003
    Inventors: Panagiotis E. George, Kirk B. Kajita, Barry P. Van West