The Boeing Company

Tyler Jacob Zimmerman

Kay Youngdahl Blohowiak

Mark Richard Brei

Anthony M Westren

Tara Kovacs Baker

Ashley C Tracey

Richard Charles Barclay

Yuliya Shafranyuk

Frederick Theodore Calkins

James Henry Mabe

Eileen Olga Kutscha

Richard Allen Miller, Ii

Matthew Anthony Dilligan

There is provided a method for determining a quality of an abrasive surface preparation of a composite surface, prior to the composite surface undergoing a post-processing operation. The method includes fabricating levels of abrasive surface preparation standards for a reference composite surface; using a surface analysis tool in the form of an ohm meter, to create target values for quantifying the levels; and measuring, with the surface analysis tool, one or more abrasive surface preparation locations on the composite surface of a test composite structure, to measure one or more of, electrical resistance and surface resistivity, of the composite surface, to obtain test result measurement(s). The method further includes comparing the test result measurement(s) to the levels, to obtain test result level(s); determining if the test result level(s) meet the target value(s); and determining whether the composite surface is acceptable to proceed with the post-processing operation.

Method and system for determining a quality of an abrasive surface preparation of a composite surface using electrical resistance and surface resistivity

Provided are molds, comprising non-metal base portions and protective optical layers that cover and shield these base portions from laser ablation. For example, a protective optical layer may reflect a laser beam used for ablating the mold. Methods of forming these protective optical layers on non-metal base portions are also provided. In some embodiments, this protective optical layer is the outermost layer exposed to the environment. Alternatively, the protective optical layer may be covered by a release layer. The release layer may be retained or removed during laser ablation. In some embodiments, light emitted by a mold during laser ablation is analyzed to determine performance of its protective optical layer. This feedback may be used to control the laser ablation such as to control orientation of the laser beam relative to the mold.

Processing tool cleaning using laser ablation

Provided are methods for cleaning processing tools from residue using laser ablation. Also provided are processing tools comprising non-metal base portions and protective optical layers that cover and shield these base portions from laser ablation. For example, a protective optical layer may reflect a laser beam used for ablating the tool. Methods of forming these protective optical layers on non-metal base portions are also provided. In some embodiments, this protective optical layer is the outermost layer exposed to the environment. Alternatively, the protective optical layer may be covered by a release layer. The release layer may be retained or removed during laser ablation. In some embodiments, light emitted by a processing tool during laser ablation is analyzed to determine performance of its protective optical layer. This feedback may be used to control the laser ablation such as to control orientation of the laser beam relative to the processing tool.

A shape memory structure includes a plurality of bases directly attached to a composite structure and arranged along a first line at a first edge of the composite structure. A plurality of buckle-shaped shape memory structures are attached to corresponding ones of the plurality of bases, such that first ends of the plurality of buckle-shaped shape memory structures are raised relative to the composite structure. Second ends of the plurality of buckle-shaped shape memory structures are directly attached to the composite structure along a second line at a second edge of the composite structure, the second edge being opposite the first edge. When activated, the shape memory structure changes from a buckled shape to an original shape to cause the composite structure to assume a deployed shape; when deactivated, the shape memory structure to resumes a buckled shape and the composite structure an undeployed shape.

Shape memory alloy actuator system for composite aircraft structures

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Seattle, WA, United States of America

Tyler Jacob Zimmerman