The Boeing Company

Timothy David Aquino

Kenneth Marvin Dull

Michael K Louie

Andrew Elmer Modin

Michael L Glain

Andrew Atkins Head

Thomas R Cundiff

Robert Alexander Coleman

Steven Charles Stenard

David J Kehrl

Scott A Harris

Joo Hyun Han

Kurtis Shuldberg Willden

Benjamin Jeffrey Stephenson

Jack Allen Woods

William Stahl Hollensteiner

Michael D Ridges

Michael Kenneth-Que Louie

Dennis James Hanks

William Henry Ingram, Jr

John R Henry

Joshua P Carlsen

Christopher Kovalenko

Cody Allan Beagley

Jordan McHale Edginton

Teresa Bennett

Phillip Keller Lathrop

David A Limon

W Taylor Peterson

Shane Rahrle

Isabel Calderon Glasmann

Ian Cox Matheson

Eli Scott Fielden

Philip Keller Lathrop

A method for vacuum bag sealing a composite part including: using a composite bagging sheet including a first sealing surface and a first interlocking strip coupled to the first sealing surface of the composite bagging sheet; joining the first interlocking strip with a second interlocking strip coupled to a second sealing surface; and forming a sealed vacuum bag around an uncured composite part positioned between the first sealing surface and the second sealing surface.

Vacuum bag sealing system and method for composite parts

A vacuum port base comprises an upper face, a lower face, a first channel, and a second channel. The upper face is configured to interface with a vacuum port. The lower face is configured to interface with a surface of a tool. The first channel formed in the lower face is configured to receive an edge breather. The second channel formed within the vacuum port base is configured to receive the vacuum port such that the vacuum port is in fluid communication with the first channel and the edge breather to remove gases from a composite structure.

Vacuum port base

A modular accelerated cure system, for which the modules are of a size and weight to each be easily portable by one person, may be configured to fit a variety of parts, e.g., carbon fiber reinforced plastic (CFRP) components, such as found in the manufacture of composite aerospace structures. The system may be used to accelerate the cure of materials that allow elevated temperature cures, e.g., sealants, primers, coatings, paints, adhesives, and protective coatings, by increasing the ambient temperature surrounding a part, or a portion of the part, within each module in a controlled manner. The system is modular in that a number of modules may be fitted together to operate in unison and also may be adapted to fit parts of a variety of contours, shapes, and sizes. Temperature within each module may be controlled using a heat controller that receives a temperature indication from each module.

Modular portable accelerated cure system

Testing of vacuum bags used in manufacturing of complex co-cure composite structures provides leak detection that allows an operator to identify leaks within a custom vacuum bag without further damaging the bag, such as by cutting vacuum ports into the bag. Such leak detection can allow the operator to find and repair the leak or, if not repairable or at a location of the bag for which repair is not feasible, take other corrective action.

Non-destructive leak source detection and identification for complex bagging in conjunction with flow measurement systems

A vacuum bag sealing system may include a composite bagging sheet, and at least one interlocking strip connected to a surface of the composite bagging sheet, wherein the interlocking strip is configured to join a first section of the composite bagging sheet to a second section of the composite bagging sheet to form a sealed vacuum bag.

A vacuum bag assembly is used to process the composite part. The vacuum bag assembly includes a stretchable vacuum bag attached to a stretchable breather.

Vacuum bag processing of composite parts using a conformable vacuum bag assembly

A vacuum bag assembly may include a bagging film and a tube bag. The bagging film may have a bagging film length and may be positioned over a composite layup and sealed to a tool surface having an inside corner. The tube bag may have opposing tube ends and a tube bag length and may be positioned over the composite layup along a length of the inside corner. Each one of the tube ends may be sealed to the tool surface along a first portion of a tube end perimeter edge and may be sealed to the bagging film along a second portion of the tube end perimeter edge such that each one of the tube ends is openable to atmosphere.

System and method of vacuum bagging composite parts

A reusable vacuum bag for processing parts is made by encapsulating a generally rigid frame within a flexible diaphragm.

Integrally stiffened, reusable vacuum bag and method of making the same

An apparatus for tensioning a preform may include a mandrel to receive a preform. The mandrel may have a first mandrel end and a second mandrel end. The preform may have a first preform end and a second preform end. The apparatus may include an anchoring groove disposed at the first mandrel end, and an anchoring device being configured and located to urge the first preform end towards the anchoring groove to secure the first preform end therebetween. The apparatus may include a tensioning groove disposed between the first mandrel end and the second mandrel end, and a tensioning device being configured and located to urge at least a portion of the preform into the tensioning groove.

Device for tensioning a preform

An apparatus to prepare a preform for fabrication includes a mandrel, anchoring groove, anchoring device, tensioning groove, and tensioning device. The mandrel receives the preform. The mandrel has a first mandrel end and a second mandrel end. The preform has a first preform end and a second preform end. The anchoring groove is disposed at the first mandrel end. The anchoring device is configured and located to urge the first preform end towards the anchoring groove to secure the first preform end therebetween. The tensioning groove is disposed between the first mandrel end and the second mandrel end. The tensioning device is configured and located to urge a portion of the preform into the tensioning groove.

Tensioning device for composite structures

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

Growing community of inventors

Olympia, WA, United States of America

Timothy David Aquino