Patents by Inventor Manning J. Scarfe

Manning J. Scarfe 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: 20250018663
    Abstract: A curing tool assembly includes a curing tool and a compaction pressure chamber. The curing tool includes a tool surface to receive a dry fabric layup. The compaction pressure chamber overlays the dry fabric layup. The compaction pressure chamber receives a pressurized fluid from a compressed fluid source during resin infusion of the dry fabric layup. The pressurized fluid received at a compaction pressure above a standard atmosphere. A method includes applying a resin pressure above a standard atmosphere to a liquid resin in a liquid resin source; and flowing the liquid resin to a dry fabric layup on a tool surface of a curing tool in response to the resin pressure. The dry fabric layup enclosed in a sealed volume. A compaction pressure above the resin pressure. The liquid resin is infused into the dry fabric layup in response to the resin pressure and the compaction pressure.
    Type: Application
    Filed: August 18, 2023
    Publication date: January 16, 2025
    Applicant: The Boeing Company
    Inventor: Manning J. Scarfe
  • Patent number: 10272619
    Abstract: A composite truss structure may have a first facesheet, a second facesheet, and a plurality of truss elements joined with the first facesheet and the second facesheet at nodes to form a one-piece structure. The composite truss structure may be formed by a method comprising preparing a dry fabric mold by: 1) placing a first dry fabric layer on a tool, 2) placing a first layer of fabric-loaded mandrels on the first dry fabric layer, 3) placing a second layer of the fabric-loaded mandrels on the first layer of fabric-loaded mandrels, and 4) placing a second dry fabric layer over the fabric-loaded mandrels. The method may further comprise infusing the dry fabric mold with a resin, and curing the resin to provide the nonflexible composite truss structure.
    Type: Grant
    Filed: May 19, 2014
    Date of Patent: April 30, 2019
    Assignee: The Boeing Company
    Inventors: Peter J. Lockett, Manning J. Scarfe, Andrew K. Glynn, David A. Pook
  • Patent number: 10086534
    Abstract: A multifunctional mandrel end cap for the fabrication of composite parts having an end cap core operatively connected to a mandrel and substantially sealed using a bonding agent or end cap sheath. The end cap sheath substantially encloses the end cap core and seals engage perimeter sealing features of the end cap core. The end cap core has a passageway fluidly connecting the mandrel with a vacuum source. The vacuum source is engageable by a vacuum conduit having one or more vacuum conduit perimeter sealing features.
    Type: Grant
    Filed: October 17, 2014
    Date of Patent: October 2, 2018
    Assignee: The Boeing Company
    Inventors: Peter J. Lockett, Manning J. Scarfe
  • Publication number: 20160107338
    Abstract: A multifunctional mandrel end cap for the fabrication of composite parts having an end cap core operatively connected to a mandrel and substantially sealed using a bonding agent or end cap sheath. The end cap sheath substantially encloses the end cap core and seals engage perimeter sealing features of the end cap core. The end cap core has a passageway fluidly connecting the mandrel with a vacuum source. The vacuum source is engageable by a vacuum conduit having one or more vacuum conduit perimeter sealing features.
    Type: Application
    Filed: October 17, 2014
    Publication date: April 21, 2016
    Inventors: Peter J. Lockett, Manning J. Scarfe
  • Publication number: 20150328845
    Abstract: A composite truss structure may have a first facesheet, a second facesheet, and a plurality of truss elements joined with the first facesheet and the second facesheet at nodes to form a one-piece structure. The composite truss structure may be formed by a method comprising preparing a dry fabric mold by: 1) placing a first dry fabric layer on a tool, 2) placing a first layer of fabric-loaded mandrels on the first dry fabric layer, 3) placing a second layer of the fabric-loaded mandrels on the first layer of fabric-loaded mandrels, and 4) placing a second dry fabric layer over the fabric-loaded mandrels. The method may further comprise infusing the dry fabric mold with a resin, and curing the resin to provide the nonflexible composite truss structure.
    Type: Application
    Filed: May 19, 2014
    Publication date: November 19, 2015
    Applicant: The Boeing Company
    Inventors: Peter J. Lockett, Manning J. Scarfe, Andrew K. Glynn, David A. Pook