The Boeing Company

Thomas Dee Hall

Darrell Darwin Jones

Tanni Sisco

Clayton Lynn Munk

Paul Reed Stone

Fei Cai

David L Wagner

Matthew K Lum

Monica Joy Brockway

Noel A Spishak

Gerfried Rudolf Achtner

Daniel Richard Smith, Jr

James C Murphy

Vincent T Olson

Ryan M Mahn

Joseph A Appleton

Victor Joseph Bolton

Eric Scott Patton

Javier Manriquez

Daniel Richard Smith Jr

A method and apparatus for positioning one component relative to another component. First metrology data may be identified for a first component and second metrology data may be identified for a second component. First locations of first features may be identified on the first component using the first metrology data. Second locations of second features on the second component may be identified using the second metrology data. A transformation may be computed based on the first locations identified and the second locations identified for use in modifying a movement plan of a robotic system for positioning the second component relative to the first component.

Method and apparatus for multi-stage spar assembly

A fastener assembly which includes a sleeve which includes a cylindrical construction having a first and second end portions and an outside diameter. The fastener assembly further includes a washer associated with the sleeve wherein the washer includes a body which defines a first side and an opposing second side and defines an opening which extends from the first side toward the second side. The opening defines a diameter greater than the outside diameter of the sleeve and the body defines a recess which has a diameter greater than the diameter of the opening wherein the recess extends from the second side toward the first side such that the recess and the opening are in communication with one another. A method for using this fastener assembly is also provided.

Hole-filling sleeve and washer design for bolt installation

A one-piece barrel assembly cart includes a right assembly cart base connected with a left assembly cart base and at least three stabilizer rings that are attached to the assembly cart base. The one-piece barrel assembly cart may be used to stabilize a tapered cured composite barrel, for example the large fuselage barrel of the aft section of a large new generation aircraft, such as a 7E7 Boeing airplane. A modular assembly cart includes at least two identical modules. Each of these modules includes a cart base and a stabilizer ring. The diameter of the inner surface of the stabilizer ring may vary as needed. Other modules including a fuselage support may be added. By providing modular assembly carts any shape and size of a one-piece composite barrel may be stabilized after curing of the composite material.

One-piece barrel assembly cart

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Everett, WA, United States of America

Thomas Dee Hall