The Boeing Company

Theboeing Company

Manning James Scarfe

Peter J Lockett

Keith Edward Baddock

Peter Lucas Heintz

Martin Alexander Szarski

Andrew K Glynn

Max Marley Osborne

David A Pook

Andrew Klimovski

Ashleigh Raoul Nesbit

Paul David Evans

Luke Fletcher

Peter N Steele

Jason J McBain

Richard James Bain

Dominic Wierzbicki

Kaustubh Dongre

A molding system and methods of forming a structure are presented. The molding system is configured to sequentially form features of a structure. The molding system comprises a first tool comprising a number of features configured to completely form a first set of radii of a structure and a number of partial forming features configured to partially form a second set of radii of the structure, and a second tool comprising a number of completion features configured to complete shaping of the second set of radii.

Molding system and methods for forming structures

A molding system and methods of forming a structure are presented. A molding system is configured to form a composite structure. The molding system comprises a first tool comprising a first vacuum groove, a first trough having a first edge configured to form a first bend of the composite structure, and a first molding surface; and a second tool comprising a second vacuum groove, a second trough having a second edge configured to form a second bend of the composite structure, and a second molding surface.

Systems and methods are provided for securing laminates to mandrels. One embodiment is a method for facilitating layup of preforms, the method including selecting a mandrel that includes at least one receptacle, disposing a first vacuum bag atop the mandrel that covers the receptacle, selecting a Ply Location Template (PLT) that includes a securement element, aligning a portion of the securement element with the receptacle, pressing the portion of the securement element downward into the first vacuum bag and driving the portion of the securement element into the receptacle, and abutting a preform against the PLT.

Ply location templates for double diaphragm vacuum bagging systems

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.

Apparatus and method for manufacturing liquid molded composites using a discrete network of tool surface resin distribution grooves

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.

Manufacture of a resin infused one-piece composite truss structure

A method for drawing a flexible sleeve over an elongated mandrel includes placing a ring within a lumen of the sleeve. A first end of the sleeve is fixed against movement relative to a first end of the mandrel. A first end portion of the sleeve is inverted over a first end portion of the mandrel so as to define a circumferential cuff in the sleeve, and the ring is positioned concentrically within the circumferential cuff. Using, e.g., a magnet, the ring is then urged longitudinally along the mandrel and toward an opposite, second end thereof, such that the sleeve is inverted over at least an outer surface of the mandrel.

Automated braided sleeve placement and tensioning

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.

Growing community of inventors

Ascot Vale, Australia

Manning James Scarfe