The Boeing Company

Dennis James Hanks

Jack Allen Woods

Andrew Elmer Modin

Hugh A Yap

Benjamin Jeffrey Stephenson

Thomas R Cundiff

William Stahl Hollensteiner

Gwen Marie Lanphere Gross

Scott K Frankenbery

Val G Brustad

Robert Dennis Hawkins

Timothy David Aquino

Gregory Robert Gleason

Michael L Glain

Kate J Felde

A system and method for manufacturing composite parts has been developed which offers the ability to produce composite parts in an infusion resin process without the use of expensive preforms or tools. In addition, the methods of manufacturing composite parts described herein offer the ability to produce composite parts having complex structures without the need for complex tooling. The method of manufacturing and systems described herein typically include printing a part skeleton using an additive manufacturing process followed by infusing the part skeleton with resin and curing the resin infused part skeleton to form the composite part.

Multi-planar fiber matrix tool-less preform for resin infusion

Systems and methods are provided for utilizing support tools for forming laminates. One embodiment is a system that includes a pair of dies that hold a multi-layer laminate over a gap, a male die that presses the laminate into the gap causing the laminate to change shape, and a support tool inserted into the gap beneath the laminate. The support tool includes a base that extends in a lengthwise direction, struts fixedly attached to the base that project upward from the base and are distributed along the lengthwise direction, and a cap that is slidably attached to the struts, and that covers the struts to form an upper surface of the support tool. Each of the struts rises from the base to the cap.

Support tools for forming laminates

A fiber preform is infused with two differing resin systems concurrently using stacked resin delivery assemblies located along one edge of the preform.

Concurrent infusion of dissimilar resins

An area of a structure is reworked from one side of the structure using resin infusion of a dry fiber patch. Entrapped air and excess resin is removed from the patch during the infusion process by inserting a vacuum device into the patch, and forcing the area resin through the vacuum device.

Method and apparatus for reworking structures

Methods and systems for manufacturing fiber-reinforced resin parts are disclosed herein. In one embodiment, a method for manufacturing a fiber-reinforced resin part includes positioning a plurality of fibers on a mold surface of a female tool, and covering the fibers with a sealing layer. The method further includes pressing a portion of the covered fibers against an interior transition region (e.g., an internal radius) of the mold surface. While the portion of covered fibers is pressed against the interior transition region, air is removed from between the sealing layer and the mold surface to draw at least a partial vacuum between the sealing layer and the mold surface.

Systems for manufacturing composite parts with female tools

An area of a structure is reworked using resin infusion of a fiber preform. A resin flow hole is formed through the structure from a first side of the structure to a second side of the structure. The fiber preform is placed on the first side of the structure and substantially saturated with resin by flowing resin into the preform and out through the resin flow hole to the second side of the structure.

Method and apparatus for reworking structures using resin infusion of fiber preforms

A composite item is fabricated in system that includes a layer of preform, supply of resin, mandrel, and bagging film. The layer of preform corresponds to the composite item. The supply of resin is sufficient to infuse the preform. The mandrel includes a preform receiving zone to receive the layer of preform and a resin receiving zone to receive the supply of resin. The resin receiving zone is adjacent to the preform receiving zone. The bagging film is operable to generate an envelope surrounding the preform receiving zone and the resin receiving zone.

Bulk resin infusion system apparatus and method

Methods and systems for manufacturing composite parts with female tools

The disclosure is directed to a process for producing resin infused composite parts having improved structural performance and improved surface appearance. The process comprises the steps of positioning a dry composite preform on a forming tool component, arranging resin exit lines in close proximity to the perform, placing a permeable release material on the perform, and placing a first piece of flow media over the release material. The process further comprises the steps of wrapping a resin distribution tube with a second piece of flow media, placing a vacuum bag layer over the forming tool component, preform, release material, first and second pieces of flow media and resin distribution tube, such that the resin distribution tube is retained in a pleat formed in the vacuum bag layer and such that a bagged preform is formed, and positioning the resin distribution tube above the bagged preform.

Tube induced deformity elimination process

By evacuating the resin feed tank to a pressure below atmospheric pressure, employing cyclic compaction, and controlling the net compaction pressure, we are better able to control a resin infusion process, particularly a vacuum assisted resin transfer molding process, and produce aerospace-grade fiber-reinforced resin composite having fiber volume fractions and tool-side surface finishes comparable to or exceeding those made using an autoclave.

Growing community of inventors

Enumclaw, WA, United States of America

Dennis James Hanks