The Boeing Company

Foster-miller, Inc.

General Electric Company

Jack Allen Woods

Andrew Elmer Modin

Wendy Wen-Ling Lin

Dennis James Hanks

Robert Dennis Hawkins

Thomas R Cundiff

Prameela Susarla

Robert Graham Albers

Joseph S Boyce

Val G Brustad

Timothy David Aquino

Xiaomei Fang

Daniel E Bullock

Gregory Robert Gleason

Michael L Glain

John Player

Victor Leemon

Margaret E Roylance

Kate J Felde

Dave A Evans

Fiber reinforced composite structures having curved stepped surfaces are fabricated by laying up plies of fiber reinforced material over a tool having a stepped tool feature. The plies are rotated about a fixed axis as they are laid up to substantially form a fixed axis rosette pattern. The plies are angularly oriented such that at least certain of the plies have fiber orientations other than 0, +45, &#x2212;45 and 90 degrees. Potential bridging of the fibers over the stepped tool features is reduced or eliminated by cutting slits in the plies in the area of the stepped features, so that the plies can be fully compacted.

Method of fabricating fiber reinforced composite structure having stepped surface

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

A method comprises laying up a fiber ply of reinforcing fibers and a metal foil layer in a full face-to-face relation. The fibers in the fiber ply are oriented in a single direction. The metal foil layer includes a plurality of metal foil strips separated by gaps. The metal foil layer has substantially the same length and width as the fiber ply. The method further comprises infusing resin into the layup, wherein the resin flows through the gaps and infuses into the fibers.

Laminated fiber metal composite

Fiber reinforced composite structure having stepped surface

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 method for fabricating a laminated composite body including a metal foil and a plurality of fiber plies. The method includes perforating a sheet of metal foil, stacking the perforated metal foil sheet and the plurality of fiber plies in face to face relation in a predetermined order and orientation, and infusing resin into the stacked sheet and plies so that resin flows through the perforations in the metal foil sheet and intersperses between the plurality of fiber plies to form the laminated composite body.

Method for fabricating a laminated fiber metal composite

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.

Controlled atmospheric pressure resin infusion process

A method of fabricating a fiber matrix composite structure including assembling a plurality of plies of fiber-reinforced polymer-matrix material on a mandrel; engaging an ultrasonic horn with the top surface of uppermost ply; and orienting the horn at an acute angle with respect to the top surface and energizing the horn to inducing a shear force in the plies to heat and consolidate the plies.

Method of fabricating a polymer-matrix fiber-reinforced composite and the product thereof

A method of fabricating a thermosetting matrix, fiber reinforced composite structure wherein a stack of fiber reinforced thermosetting material plies are assembled; an ultrasonic horn is engaged with a top surface of the upper most ply, oriented at an acute angle with respect to the top surface, and energized to induce a shear wave in the plies to heat the plies. The horn is moved along the upper most ply to consolidate the plies and the energy level applied to the horn is sufficient to reduce the viscosity of the thermoset resin to the point where the plies can be debulked but not high enough to fully cross-link the resin so that another ply can still be fully cross-linked to the uppermost ply. Pressure is applied to the plies as the horn moves to debulk the plies.

Growing community of inventors

Kent, WA, United States of America

Jack Allen Woods