The Boeing Company

Mcdonnell Douglas Corporation

Michael Leslie Hand

Douglas Alan McCarville

Juan C Guzman

Michael J Robinson

William Preston Keith

Leanne L Lehman

Creed E Blevins

Gopal Prasad Mathur

Ali Yousefiani

Buddhadev Chakrabarti

John Michael Comfort

John G Vollmer

Keith Y Chong

Christopher Stephen Roper

Tobias A Schaedler

Jonathan David Embler

Gary David Grayson

James B Blackmon, Jr

Jennifer Sue Noel

Randall C Schubert

Nelson Edwin Jones

Donald L Edberg

Jonathan Edward Bosley

Alexandra K Dillon

Robert E Drubka

Jordan Oliver Birkland

Edwin C Cady

Timothy L Gaynor, Iii

Miklos Paul Petervary

Samuel S Yao

Jeffrey D Eichinger

R Andrew Gerrick

Matthew Jeffrey Molitor

Russel J Sanui

Paul Dufour

Edward E Cook

Adam C Smith

Jeffrey Dale Fukushima

Creed Ernest Blevins

Juan Carlos Guzman

Matthew Molitor

Douglas A Mccarville

Douglas Mccarville

Alexandra K Dillan

Randall Colin Schubert

Jennifer S Noel

Timothy Leo Gaynor Iii

Michael James Robinson

Douglas A Mc Carville

A panel is disclosed, including a first facesheet, a second face sheet, and a plurality of pultrusion-formed web structures. Each web structure has a middle support portion, a first end portion, and a second end portion. The first end portion of each web structure is attached to the first facesheet and the second end portion of each web structure is attached to the second facesheet. The middle support portion, first end portion, and second end portion of each web structure form a single monolithic structure.

Web core sandwich structures

A method and apparatus for strong bonded wide joints for cryogenic applications. In one advantageous embodiment, an apparatus may comprise a three-dimensional preform and a plastic matrix. The plastic matrix may be impregnated in the three-dimensional preform to form a softening strip that may be capable of remaining flexible at a temperature at which a gas may have a liquid form.

Strong bonded joints for cryogenic applications

A method and apparatus for forming a joint. A composite insert may be placed into a joint region for a first structure. The composite insert may comprise a structure having a first portion, a second portion, and a third portion all extending from a junction; and a resin impregnated into the structure to form the composite insert. The second structure may be laid up. The composite insert may be bonded to the first structure and the second structure.

Method for forming a fabric preform insert for a composite tank Y-joint

Additively manufactured parts are disclosed comprising an integral additively manufactured nut plate cradle, and methods of their manufacture and use in part and component installation and to facilitate joining parts and components to larger structures.

Integral nut-retaining cradle for a nut plate assembly and methods of manufacturing using additive manufacturing

A method, a composite joint, and a composite tank are presented. The composite tank comprises a curved wall, a plurality of shear fittings, and a plurality of bolts. The curved wall has an opening. The plurality of shear fittings is threaded into a plurality of blind holes in the curved wall around the opening. The plurality of bolts engages the plurality of shear fittings and joins a cap to the curved wall.

Composite joint

A composite resin tank includes a wall joined to a dome along a joint. A softening strip is located in the joint.

Composite tank having joint with softening strip

A composite resin tank includes a wall joined to a dome along a joint. A softening strip is used to control stress in the joint.

Method of making a device for controlling stress in joints at cryogenic temperatures

An integrated composite structure with a graded coefficient of thermal expansion (CTE) is formed by selecting a plurality of layers of materials with a graded CTE and using build-up (bottom-up) fabrication approaches such as metal deposition or powder metallurgy to produce a CTE-graded layered composite preform, which is then consolidated and heat treated to create the CTE graded integrated composite billet or near net shape. The integrated composite billet or near net shape is then processed to produce a first surface for attachment of a first structural member having a first CTE and to produce a second surface of for attachment of a second structural member having a second CTE.

Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applications

Fluted core sandwich panels are joined together to form a composite structure. Variations in panel ends are accommodated by a core stiffener insert installed in a joint between ends of the panels.

Method for joining sandwich truss core panels and composite structures produced therefrom

Apparatus and methods provide for a non-linear scarf joint and a method for joining two components utilizing a non-linear scarf joint. A non-linear scarf joint includes multi-planar surfaces on connection ends of two components being joined to create a structure. Each multi-planar surface includes a first faying surface, a second faying surface, and a transition faying surface joining the first and second faying surfaces. A transition scarf angle associated with the transition faying surface is different than scarf angles associated with the first and second faying surfaces.

Non-linear scarf joint

A method for assembling a composite wall assembly edge joint including laying up a first composite face sheet, laying up a first composite buildup pad having a first tapered section onto the first composite face sheet and positioning a composite flute core member, including a tapered first portion with a first inclined surface and a second inclined surface. First inclined surface is positioned onto the first tapered section of the first composite buildup pad and a second portion of the composite flute core member extends from the tapered first portion along first composite face sheet. The method also includes laying up a second composite buildup pad having a second tapered section with the second composite buildup pad spaced apart from the first composite buildup pad and having at least a portion of the second tapered section overlying the second inclined surface of the tapered first portion.

Method of assembly of composite core sandwich edge joint

A hybrid softening strip for controlling stresses in a joint at low temperatures includes a layer of sacrificial material that can be tailored to fit the softening strip in the joint after the softening strip has been bonded to a structure.

Softening strip for controlling stress in joints at very low temperatures

A composite wall assembly edge joint including a first composite buildup pad having a first tapered section is secured to and extends along a first composite face sheet. A second composite buildup pad having a second tapered section is secured to and extends along a second composite face sheet, wherein the first and second composite buildup pads are positioned between spaced apart first and second composite face sheets. A composite flute core member includes a tapered first portion positioned between and secured to the first tapered section and to the second tapered section. A second portion of the composite flute core member extends in a direction away from the tapered first portion of the composite flute core member and is positioned between, extends along and is secured to the first and second composite face sheets.

Fluted core sandwich shell edge joint

A composite wall assembly edge joint, includes a first composite buildup pad secured to a first composite face sheet with the first composite buildup pad having a first tapered section with a first inclined surface which extends in a first direction and having a second section which extends from the first tapered section with a second surface which extends in a second direction, different from the first direction, toward a first end of the first composite face sheet. The assembly further includes a composite flute core member, having a tapered first portion secured to the first tapered section; a second portion secured to the first composite face sheet; and a third portion which extends in the second direction, away from the tapered first portion, toward the first end of the first composite face sheet secured to the second section.

Growing community of inventors

Huntington Beach, CA, United States of America

Michael Leslie Hand