The Boeing Company

Charles A Rhodes

Terry A Sewell

Carlos Angelo Fracchia

Daniel David Bloch

Eric Eldon Deck

Timothy J Luchini

Eric E Moyes

Roy Lewis Barr

Andrew R Mallow

Travis R Adams

Benjamin Richards

Juliette Dubon

Augustus J Ellis

Jeffry K Berner

Adam Martinez

Carlos A Fracchia

A system and method for removing a backing from a ply of composite material is disclosed. The system includes a roller having a roller axis and a roller surface that circumscribes the roller axis. The system also includes an adhesion feature disposed on the roller surface. The system further includes a roller drive to move the roller along a travel path that is perpendicular to the roller axis and to rotate the roller about the roller axis.

Systems and methods for removing a backing from a ply of composite material

A closed-angle composite airfoil spar is provided for an airfoil assembly. The composite airfoil spar comprises a web portion having a thickness. The composite airfoil spar also comprises a flange portion having a thickness. The flange portion extends transverse to the web portion. The composite airfoil spar further comprises a radius portion interconnecting the web and flange portions. The radius portion is an acceptable amount thinner relative to thickness of the web portion and thickness of the flange portion based on design requirements and material properties.

Closed-angle composite airfoil spar and method of fabricating the same

A composite comprising adhered components and method of refurbishing such composites are described herein. The composite includes a first component, a second component, and the first component being adhered to the second component using an adhesive stack. The adhesive stack comprises a first adhesive-impregnated scrim layer disposed between the first component and the second component and a bulk adhesive layer disposed between the first component and the second component.

Composites comprising adhered components

Methods of refurbishing an adhered component and composites comprising adhered components

A composite fiber placement mid-span redirect device (10) mounted on a fiber placement assembly (12) guides a plurality of composite material tows (14) along a fiber path from a material supply creel (20) to a fiber placement head (30) during a composite forming process. The mid-span redirect device (10) includes a frame assembly (38) to which a plurality of outer swivel roller assemblies (80) and a plurality of inner swivel roller assemblies (90) are attached. Each outer swivel roller assembly (80) contains an outer roller (82), an outer capture roller (84), an outer swivel bracket assembly (86), and a counterbalancing member (88). Each inner swivel assembly (90) contains an inner roller (92), an inner swivel bracket assembly (96), and a counterbalancing member (98). The outer swivel assemblies (80) and inner swivel assemblies (90) work in concert with one another to accommodate six axes of motion from a fiber placement assembly (12), and simultaneously allow the fiber tows (14) to move bi-directionally, both towards the material supply creel (20) and alternately towards the fiber placement head (30), without inducing twisting of the fiber tows (14).

Fiber placement mid-span redirect

Growing community of inventors

Saint Louis, MO, United States of America

Charles A Rhodes