Patents by Inventor Max M. Osborne

Max M. Osborne 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: 11305859
    Abstract: A method for forming a composite structure includes the steps of: forming a fiber-reinforced polymer paste to a shape of a cavity of a dry fiber preform structure; heating said dry fiber preform structure having said fiber-reinforced polymer in said cavity to an infusion temperature; infusing resin into said dry fiber preform structure and around said fiber-reinforced polymer; and curing said resin-infused fiber preform structure and said fiber-reinforced polymer at a cure temperature higher than said infusion temperature.
    Type: Grant
    Filed: March 28, 2018
    Date of Patent: April 19, 2022
    Assignee: The Boeing Company
    Inventors: Weidong Song, Gerard J. Gallo, Gwen Marie Lanphere Gross, Jamie J. Langabeer, Jason J. McBain, Stephen L. Metschan, Jeffrey H. Olberg, Max M. Osborne, Richard V. Phillips, Paul D. Evans, Hugh A. Yap, Nicholas J. Zayas
  • Patent number: 10807324
    Abstract: A tool and its method of use direct a flow of liquid resin through a preform. The tool has a tool surface with a channel recessed into the tool surface to a bottom surface of the channel. A plate is positioned on the tool surface covering over the channel with the plate being supported by the tool in the channel spaced above the bottom surface of the channel and with the top surface of the plate positioned coplanar with the tool surface of the tool. A preform is positioned on the tool surface with the preform covering over the plate. A flow of liquid resin is supplied to the tool surface and a pressure differential communicating with the tool surface draws the flow of liquid resin into the channel, through the channel and through a plurality of perforations through the plate and into the preform.
    Type: Grant
    Filed: August 3, 2018
    Date of Patent: October 20, 2020
    Assignee: The Boeing Company
    Inventors: Paul D. Evans, Max M Osborne
  • Patent number: 10759124
    Abstract: A method of infusing liquid resin into a preform involves positioning a preform on a planar section of a tool surface and a trough section of the tool surface, where the planar section of the tool surface is positioned vertically above the trough section of the tool surface and with there being a plurality of grooves in the planar section of the tool surface and a bottom of the trough section of the tool surface. At least one of a fluid impervious sheet, a second tool and a vacuum bag is secured on the tool surface over the preform forming a sealed volume on the tool surface. A pressure differential and a flow of resin is supplied onto the tool surface and the liquid resin is infused into the preform by the pressure differential.
    Type: Grant
    Filed: November 21, 2017
    Date of Patent: September 1, 2020
    Assignee: The Boeing Company
    Inventors: Kaustubh Dongre, Paul Evans, Peter J. Lockett, Jason J. McBain, Max M. Osborne, Manning Scarfe
  • Patent number: 10730250
    Abstract: Caul plates and related methods are disclosed herein. An example caul plate for use in a composite laminate layup includes a first surface and a second surface opposite the first surface. The example caul plate includes protrusions extending from the first surface. The protrusions are disposed over a tool surface of the composite laminate layup. The protrusions are to define a gap between the first surface and the tool surface to limit a thickness of a preform disposed between the tool surface and the first surface when a pressure is exerted on the second surface.
    Type: Grant
    Filed: October 5, 2018
    Date of Patent: August 4, 2020
    Assignee: The Boeing Company
    Inventors: Max M. Osborne, Matthew Suter
  • Publication number: 20200108571
    Abstract: Caul plates and related methods are disclosed herein. An example caul plate for use in a composite laminate layup includes a first surface and a second surface opposite the first surface. The example caul plate includes protrusions extending from the first surface. The protrusions are disposed over a tool surface of the composite laminate layup. The protrusions are to define a gap between the first surface and the tool surface to limit a thickness of a preform disposed between the tool surface and the first surface when a pressure is exerted on the second surface.
    Type: Application
    Filed: October 5, 2018
    Publication date: April 9, 2020
    Inventors: Max M. Osborne, Matthew Suter
  • Publication number: 20190300141
    Abstract: A method for forming a composite structure includes the steps of: forming a fiber-reinforced polymer paste to a shape of a cavity of a dry fiber preform structure; heating said dry fiber preform structure having said fiber-reinforced polymer in said cavity to an infusion temperature; infusing resin into said dry fiber preform structure and around said fiber-reinforced polymer; and curing said resin-infused fiber preform structure and said fiber-reinforced polymer at a cure temperature higher than said infusion temperature.
    Type: Application
    Filed: March 28, 2018
    Publication date: October 3, 2019
    Applicant: The Boeing Company
    Inventors: Weidong Song, Gerard J. Gallo, Gwen Marie Lanphere Gross, Jamie J. Langabeer, Jason J. McBain, Stephen L. Metschan, Jeffrey H. Olberg, Max M. Osborne, Richard V. Phillips, Paul D. Evans, Hugh A. Yap, Nicholas J. Zayas
  • Publication number: 20190152167
    Abstract: A tool and its method of use, where a plurality of grooves and/or a channel are formed into the tool surface of the tool. The grooves and/or channel distribute and deliver resin supplied to the tool surface throughout a dry fiber composite layup positioned on the tool surface in resin infusion and resin transfer molding. The grooves are formed in the tool surface extending to discrete areas on the tool surface to direct a flow of liquid resin to the discrete areas and infuse the dry fiber composite layup with the liquid resin at those discrete areas of the tool surface. When a channel is formed in the tool surface, a perforated plate extends over the channel to prevent fibers from the preform from being pulled from the preform and into the liquid resin flowing through the channel.
    Type: Application
    Filed: August 3, 2018
    Publication date: May 23, 2019
    Applicant: The Boeing Company
    Inventors: Paul E. Evans, Max M. Osborne
  • Publication number: 20190152170
    Abstract: A tool and its method of use, where a plurality of grooves are formed into the tool surface of the tool. The grooves have different cross-section dimensions, different lengths, different configurations and/or different patterns that function as tool surface resin distribution grooves. The grooves distribute and deliver resin supplied to the tool surface throughout a dry fiber composite layup positioned on the tool surface in resin infusion and resin transfer molding. The grooves are formed in the tool surface extending to discrete areas on the tool surface to direct a flow of liquid resin to the discrete areas and infuse the dry fiber composite layup with the liquid resin at those discrete areas of the tool surface.
    Type: Application
    Filed: November 21, 2017
    Publication date: May 23, 2019
    Applicant: The Boeing Company
    Inventors: Kaustubh Dongre, Paul Evans, Peter J. Lockett, Jason J. McBain, Max M. Osborne, Manning Scarfe
  • Patent number: 10059061
    Abstract: A system for manufacturing a composite structure includes a tool with a surface for supporting component elements of the composite structure. The surface is divided into a multi-dimensional array of thermal zones for in-process control of the temperature of a component element (e.g. resin) of the composite structure. The sensors sense a characteristic of the component element and provide sensor data, which is applied to a machine-learning algorithm configured to generate control data to achieve a defined quality goal. A controller then independently controls the thermal zones to locally heat, cool or maintain the temperature of the component element according to the control data to advance the component element or composite structure to the defined quality goal. This may be performed over a plurality of instances during which the machine-learning algorithm learns to increase advancement of the component element or composite structure to the defined quality goal.
    Type: Grant
    Filed: October 7, 2015
    Date of Patent: August 28, 2018
    Assignee: The Boeing Company
    Inventors: Lauren A. Burns, Max M. Osborne, Martin A. Szarski, Ronnie K. Ligeti, David Pook, Andrew K. Glynn
  • Publication number: 20170100894
    Abstract: A system for manufacturing a composite structure includes a tool with a surface for supporting component elements of the composite structure. The surface is divided into a multi-dimensional array of thermal zones for in-process control of the temperature of a component element (e.g. resin) of the composite structure. The sensors sense a characteristic of the component element and provide sensor data, which is applied to a machine-learning algorithm configured to generate control data to achieve a defined quality goal. A controller then independently controls the thermal zones to locally heat, cool or maintain the temperature of the component element according to the control data to advance the component element or composite structure to the defined quality goal. This may be performed over a plurality of instances during which the machine-learning algorithm learns to increase advancement of the component element or composite structure to the defined quality goal.
    Type: Application
    Filed: October 7, 2015
    Publication date: April 13, 2017
    Inventors: Lauren A. Burns, Max M. Osborne, Martin A. Szarski, Ronnie K. Ligeti, David Pook, Andrew K. Glynn