The Boeing Company

Benjamin Jeffrey Stephenson

Charles William Thomas

William Stahl Hollensteiner

William Henry Ingram, Jr

Scott K Frankenbery

Jake Adam Reeves

Karl Marius Nelson

Jeffrey M Hansen

Gwen Marie Lanphere Gross

Dennis James Hanks

Hugh A Yap

Cameron Bunch

Daniel M Rotter

John Dempsey Morris

Jonathan A Santiago

Stephen Lee Metschan

Richard V Phillips

Samuel Ray Stewart

Marcus Anthony Belcher

Gabriel Zane Forston

Timothy David Aquino

Robert L Anderson

Richard Allen Miller, Ii

Megan Elizabeth Bliss

John R Henry

Amy E Bahe

Kieran Patrick Davis

John R Aubin

Cody Allan Beagley

Jordan McHale Edginton

Dennis J Hanks

Scott K Frankenberry

William S Hollensteiner

A method and apparatus for forming a radius filler. A lattice is formed of connecting elongate members having a three-dimensional shape of the radius filler. A resin is placed within the lattice.

Lattice reinforced radius filler

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

A pressure vessel for storing hydrogen is described. The pressure vessel includes at least one chamber to store hydrogen atoms. The pressure vessel also includes a mycelium structure within the at least one chamber. The mycelium structure has a surface area of at least 800 m/m. At least some of the hydrogen atoms are attached to the mycelium structure at a pressure greater than ambient pressure. Methods of storing hydrogen and methods of constructing a hydrogen storage tank are also described.

Mycelium storage medium for use in storing hydrogen

A structure comprising a plurality of walls defining a bladder cavity, the bladder cavity comprises an initial cross section size. A first plurality of wave features provided along at least one of the plurality of walls defining the bladder cavity. In one arrangement, the first plurality of wave features allow the structure to expand from the initial cross section size to a second cross section size after the structure becomes inflated during a composite charge cure, the second cross section size larger than the initial cross sectional size.

Bladder system for curing 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

Systems and methods are provided for enhancing edge breathers for composite manufacturing. One exemplary embodiment is an apparatus that includes an edge breather to facilitate manufacturing of a composite part. The edge breather includes a body, ridges disposed along a length of the body that each define an arc which is perpendicular to a lengthwise axis of the body, and openings disposed along the body that enable air to enter a hollow interior that runs along the length of the body. The arcs defined by the ridges resist compressive loads applied to the edge breather and prevent the hollow interior from collapsing under pressure applied to the edge breather by a vacuum bag during manufacturing of the composite part.

Ridged edge breathers for composite products

A blade-protecting sheath is configured to protect a cutting blade of an ultrasonic cutting system. The blade-protecting sheath includes a main body having a first end and an opposite second end, a blade-receiving channel formed through the first end, and a nut-retention chamber connected to the blade-receiving channel. The nut-retention chamber is defined by interior planar walls that are configured to receive and constrain a nut of the ultrasonic cutting system. A blade slot is connected to the nut-retention chamber. The cutting blade is configured to pass into the blade slot and be secured within a blade chamber.

Blade-protecting sheath for an ultrasonic cutting system

Edge breathers for composite products

A system and method for forming a composite filler. The method comprises applying a pressure to a first portion of a composite material blank with a pair of forming dies of a composite filler forming apparatus, the pair of forming dies having a pair of convex radii, each forming die of the pair of forming dies having a respective convex radius of the pair of convex radii. The method also repeats the applying step to a subsequent portion of the composite material blank to incrementally form the composite material blank into a desired cross-section along its length.

Composite filler forming apparatus

Systems and methods are provided for curing composite products. One exemplary embodiment is an edge breather for composite manufacturing. The edge breather is formed of a rigid material and includes an elongated body having a top open structure with a cross section that defines an arch. The edge breather also includes hollow passageways within the elongated body that are underneath the top structure and travel along a length of the elongated body. The top open structure defines multiple openings forming an open mesh through which air may enter.

Methods, systems and apparatuses are disclosed for making and post-processing a 3-D printed object for laminate-forming tooling, and components made using post-processed 3-D printed laminate-forming tooling.

Method and apparatus for high-temperature post-curing of UV-cured photopolymers

Devices, systems and methods for compacting a charge of composite material across an edge are disclosed herein. The devices include a vacuum compaction device including a compaction force transfer structure, a sealing structure, and a vacuum distribution manifold. The compaction force transfer structure includes a first barrier structure, a second barrier structure, and a junction support that extends at least partially between the first barrier structure and the second barrier structure. The junction support is configured to maintain the first barrier structure and the second barrier structure at an angle with respect to one another and to permit limited angular motion of the first barrier structure and the second barrier structure relative to one another. The systems include composite structure fabrication systems that include the vacuum compaction device. The methods include methods of operating the vacuum compaction device.

Devices, systems, and methods for compacting a charge of composite material across an edge

Growing community of inventors

Seattle, WA, United States of America

Benjamin Jeffrey Stephenson