Patents by Inventor Alexander M. Rubin

Alexander M. Rubin 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).

  • Publication number: 20150013894
    Abstract: A method and apparatus is presented. A method may comprise positioning a metallic bladder within a tool, the tool having a number of die liners that generate heat when exposed to a magnetic field; applying the magnetic field to the number of die liners to heat the metallic bladder; and pressurizing the metallic bladder.
    Type: Application
    Filed: July 7, 2014
    Publication date: January 15, 2015
    Inventors: Marc Rollo Matsen, Alexander M. Rubin, Randall Dow Wilkerson, Carey E. Wilkinson, James Rodney Fox, Charles R. Prebil, Gregory James Schoepen Hickman, Jeffery Lee Marcoe
  • Publication number: 20140314894
    Abstract: A device changes the shape of a die used to compression mold a part. The device includes a sleeve placed between the die and a charge to be molded. The sleeve has an inner face generally conforming to a face of the die, and a outer face for molding a part.
    Type: Application
    Filed: February 17, 2014
    Publication date: October 23, 2014
    Applicant: The Boeing Company
    Inventors: Charles R. Prebil, James R. Fox, Alexander M. Rubin, Randall D. Wilkerson
  • Patent number: 8691137
    Abstract: A device changes the shape of a die used to compression mold a part. The device includes a sleeve placed between the die and a charge to be molded. The sleeve has an inner face generally conforming to a face of the die, and a outer face for molding a part.
    Type: Grant
    Filed: March 4, 2009
    Date of Patent: April 8, 2014
    Assignee: The Boeing Company
    Inventors: Charles R. Prebil, James R. Fox, Alexander M. Rubin, Randall D. Wilkerson
  • Publication number: 20140014274
    Abstract: Thermoplastic laminates are fabricated in a continuous compression molding production line. A lay-up of laminate plies is placed in a recess on a carrying tool, and the tool is moved through successive forming operations on the line, including preforming and consolidation operations. The tool is separated from the fully formed part at the end of the line and may be reused. Use of the carrying tool reduces material scrap.
    Type: Application
    Filed: July 3, 2013
    Publication date: January 16, 2014
    Inventors: Randall D. Wilkerson, James R. Fox, Alexander M. Rubin
  • Patent number: 8545201
    Abstract: A system for forming a composite structure comprises an electromagnetic press including an upper die, a lower die and an electromagnet. The lower die may be mounted in spaced relation to the upper die for receiving a composite layup therebetween. The electromagnet is energizable such that the upper and lower dies apply a compressive force to the composite layup.
    Type: Grant
    Filed: August 16, 2012
    Date of Patent: October 1, 2013
    Assignee: The Boeing Company
    Inventors: Michael M. Vander Wel, Alexander M. Rubin
  • Patent number: 8491745
    Abstract: Thermoplastic laminates are fabricated in a continuous compression molding production line. A lay-up of laminate plies is placed in a recess on a carrying tool, and the tool is moved through successive forming operations on the line, including preforming and consolidation operations. The tool is separated from the fully formed part at the end of the line and may be reused. Use of the carrying tool reduces material scrap.
    Type: Grant
    Filed: February 3, 2007
    Date of Patent: July 23, 2013
    Assignee: The Boeing Company
    Inventors: Randall D. Wilkerson, James R. Fox, Alexander M. Rubin
  • Patent number: 8425708
    Abstract: Thermoplastic composite laminate parts with tailored and varying thickness and/or curved sections are manufactured in a continuous process. Automated equipment or hand lay-up is used to collate parts or components into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. Some or all of the plies may be continuously fed from spools of single or multiply ply material. Ply consolidation tooling contains all necessary part features and is coordinated to the customized multiple ply stacks to form a single integrated thermoplastic composite laminate potentially having areas of differing thickness from the multiple ply stacks.
    Type: Grant
    Filed: April 6, 2007
    Date of Patent: April 23, 2013
    Assignee: The Boeing Company
    Inventors: Alexander M. Rubin, James R. Fox, Randall D. Wilkerson
  • Patent number: 8333858
    Abstract: A fabrication method of forming curved thermoplastic composite laminate parts with tailored and varying thickness in a continuous process. Automated equipment or hand lay-up are used to collate parts or components into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. Ply consolidation tooling contains all necessary part features and is coordinated to the customized multiple ply stacks to form a single integrated thermoplastic composite laminate potentially having areas of differing thickness from the multiple ply stacks.
    Type: Grant
    Filed: October 20, 2006
    Date of Patent: December 18, 2012
    Assignee: The Boeing Company
    Inventors: Alexander M. Rubin, James R. Fox, Randall D. Wilkerson
  • Publication number: 20120305197
    Abstract: A system for forming a composite structure comprises an electromagnetic press including an upper die, a lower die and an electromagnet. The lower die may be mounted in spaced relation to the upper die for receiving a composite layup therebetween. The electromagnet is energizable such that the upper and lower dies apply a compressive force to the composite layup.
    Type: Application
    Filed: August 16, 2012
    Publication date: December 6, 2012
    Applicant: THE BOEING COMPANY
    Inventors: Michael M. Vander Wel, Alexander M. Rubin
  • Patent number: 8268226
    Abstract: A system for forming a composite structure comprises an electromagnetic press including an upper die, a lower die and an electromagnet. The lower die may be mounted in spaced relation to the upper die for receiving a composite layup therebetween. The electromagnet is energizable such that the upper and lower dies apply a compressive force to the composite layup.
    Type: Grant
    Filed: July 7, 2009
    Date of Patent: September 18, 2012
    Assignee: The Boeing Company
    Inventors: Michael M. Vander Wel, Alexander M. Rubin
  • Publication number: 20110206906
    Abstract: An elongate thermoplastic composite member is fabricated by a continuous molding process. A pre-consolidated thermoplastic laminate is softened by heating it to a temperature below its melting layup, and is fed substantially continuously through multiple sets of tool dies. The tool dies incrementally mold portions of softened laminate over a mandrel to form the laminate into a shape having a closed cross section.
    Type: Application
    Filed: February 24, 2010
    Publication date: August 25, 2011
    Inventors: Alexander M. Rubin, James R. Fox, Randall D. Wilkerson
  • Patent number: 7871553
    Abstract: A process for forming curved thermoplastic composite material. According to an illustrative embodiment, the process includes providing a length of straight thermoplastic material; pre-forming the length of straight thermoplastic material into a selected cross-sectional configuration; pressing the length of the straight thermoplastic material; and imparting a curved shape to the length of straight thermoplastic material by providing a curved section and passing the length of straight thermoplastic material through the curved section of a process assembly.
    Type: Grant
    Filed: September 21, 2007
    Date of Patent: January 18, 2011
    Assignee: The Boeing Company
    Inventors: Randall D. Wilkerson, Alexander M. Rubin, James R. Fox
  • Publication number: 20110006460
    Abstract: A system for forming a composite structure comprises an electromagnetic press including an upper die, a lower die and an electromagnet. The lower die may be mounted in spaced relation to the upper die for receiving a composite layup therebetween. The electromagnet is energizable such that the upper and lower dies apply a compressive force to the composite layup.
    Type: Application
    Filed: July 7, 2009
    Publication date: January 13, 2011
    Applicant: The Boeing Company
    Inventors: Michael M. Vander Wel, Alexander M. Rubin
  • Publication number: 20100319841
    Abstract: A fabrication method of forming a thermoplastic composite laminate material with tailored and varying thickness in a continuous process. This process utilizes automated equipment or hand lay-up to collate parts or components into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. The consolidation tooling contains all necessary part features and is coordinated to the customized multiple ply stacks to form a single integrated thermoplastic composite laminate potentially having areas of differing thickness from these multiple ply stacks.
    Type: Application
    Filed: August 26, 2010
    Publication date: December 23, 2010
    Applicant: THE BOEING COMPANY
    Inventors: ALEXANDER M. RUBIN, JAMES R. FOX, RANDALL D. WILKERSON
  • Patent number: 7807005
    Abstract: A fabrication method of forming a thermoplastic composite laminate material with tailored and varying thickness in a continuous process. This process utilizes automated equipment or hand lay-up to collate parts or components into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. The consolidation tooling contains all necessary part features and is coordinated to the customized multiple ply stacks to form a single integrated thermoplastic composite laminate potentially having areas of differing thickness from these multiple ply stacks.
    Type: Grant
    Filed: February 2, 2006
    Date of Patent: October 5, 2010
    Assignee: The Boeing Company
    Inventors: Alexander M. Rubin, James R. Fox, Randall D. Wilkerson
  • Publication number: 20100225016
    Abstract: A device changes the shape of a die used to compression mold a part. The device includes a sleeve placed between the die and a charge to be molded. The sleeve has an inner face generally conforming to a face of the die, and a outer face for molding a part.
    Type: Application
    Filed: March 4, 2009
    Publication date: September 9, 2010
    Inventors: Charles R. Prebil, James R. Fox, Alexander M. Rubin, Randall D. Wilkerson
  • Publication number: 20090078362
    Abstract: A process for forming curved thermoplastic composite material. According to an illustrative embodiment, the process includes providing a length of straight thermoplastic material; pre-forming the length of straight thermoplastic material into a selected cross-sectional configuration; pressing the length of the straight thermoplastic material; and imparting a curved shape to the length of straight thermoplastic material by providing a curved section and passing the length of straight thermoplastic material through the curved section of a process assembly.
    Type: Application
    Filed: September 21, 2007
    Publication date: March 26, 2009
    Inventors: Randall D. Wilkerson, Alexander M. Rubin, James R. Fox
  • Publication number: 20080185756
    Abstract: Thermoplastic laminates are fabricated in a continuous compression molding production line. A lay-up of laminate plies is placed in a recess on a carrying tool, and the tool is moved through successive forming operations on the line, including preforming and consolidation operations. The tool is separated from the fully formed part at the end of the line and may be reused. Use of the carrying tool reduces material scrap.
    Type: Application
    Filed: February 3, 2007
    Publication date: August 7, 2008
    Inventors: Randall D. Wilkerson, James R. Fox, Alexander M. Rubin
  • Publication number: 20070175573
    Abstract: Thermoplastic composite parts having integrated metal fittings are manufactured using a continuous compression molding process. Automated equipment or hand lay-up are used to collate composite material plies and metal fittings into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. Multiple lay-ups may be cut from each stack. The lay-ups are placed in tooling containing part features and are continuously fed through a performing station where the lay-ups are preformed into the approximate shape of the finished part. Following pre-forming, the tooling is moved incrementally through a consolidation station where a compression press presses successive sections of the tooling to form a single integrated thermoplastic composite laminate part having integrated metal fittings, which may include areas of differing thickness.
    Type: Application
    Filed: January 29, 2007
    Publication date: August 2, 2007
    Inventors: James R. Fox, Randall D. Wilkerson, Alexander M. Rubin
  • Publication number: 20070175575
    Abstract: A fabrication method of forming curved thermoplastic composite laminate parts with tailored and varying thickness in a continuous process. Automated equipment or hand lay-up are used to collate parts or components into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. Ply consolidation tooling contains all necessary part features and is coordinated to the customized multiple ply stacks to form a single integrated thermoplastic composite laminate potentially having areas of differing thickness from the multiple ply stacks.
    Type: Application
    Filed: October 20, 2006
    Publication date: August 2, 2007
    Inventors: Alexander M. Rubin, James R. Fox, Randall D. Wilkerson