The Boeing Company

Luis A Perla

Gagandeep Saini

Jeron D Moore

Brice Aaron Johnson

Michael Kenneth-Que Louie

Robert G Meyer

Robert Graham Albers

Shane Edward Arthur

Clayton Lynn Munk

Dan Dresskell Day

Bennett M Moriarty

Ryan M Trumbo

Seana B Kobak

Marcin Artur Rabiega

Jason Warner

Jeffrey Stephen Rebmann

Stewart James Ibbotson

Trevor S McCrea

Joseph Warren

William Thomas Kline

Michael K Louie

Geoffrey Allen Butler

Erik Lund

Charles Yuanxin Hu

Harry E Townsend

Thomas Joseph Kennedy

Christopher Wayne Fay

Stephen Glade Holley

Timothy D Jackson

John R Aubin

Peter J VanVoast

Wallace Kwan

Erika L Berhardt

Brandon J Steffensmeier

Nicholas J Schnoebelen

Charles J Nelson

Justin L Holland

Richard A Ransom

Curtis M Groth

Thang D Phung

Joseph F Warren

Jason S Warner

Jeffrey S Rebmann

Trevor S Mccrea

An illustrative example of the present disclosure provides a machine configured to form a composite structure. The machine includes a composite placement machine, measuring equipment, a tool path generator, and compaction equipment. The composite placement machine lays up composite plies. The measuring equipment measures surfaces of the composite plies to form measurements during layup of the composite plies. A computer includes a model of the composite plies for a structure. The tool path generator forms a modified tool path based upon a difference between the measurements and expected measurements for the composite plies in the model.

Machine configured to form a composite structure

A measurement probe edge guide tool includes an edge follower comprising two edge contact pins that spin around the outside of the measurement probe using a ball bearing. The edge contact pins hug the corner of a contoured edge of the workpiece or in-service part to provide a consistent distance of the center of the probe from the edge. The edge follower enables the tool to inspect the marginal portion bounded by a contoured (machined) edge of a workpiece or part. The edge follower is removable so that the tool may also be adapted for use in general acreage inspection. The tool features a spring-loaded mechanism with a positive probe protrusion relative to a roller-supported cage. The tool has either a handle which is coupled to the cage by means of a universal joint or a hand grip that is affixed to the cage.

Measurement probe edge guide tool

A method for analyzing a surface quality of a laminate part including the steps of creating a planned dimensioned representation of a laminate part desired to be built which includes a first surface having a first topography; placing fibers into locations for the laminate part desired to be built; and curing a resin associated with the placed fibers fabricating an as-built laminate part which includes a second surface having a second topography which corresponds to the first surface having the first topography. The method also includes aligning the first surface, the second surface and the locations of the fibers; determining a first elevation of a first point on the first surface and a second elevation of a second point on the second surface; and observing the first surface, the second surface and the locations of the fibers in alignment and the first elevation relative to the second elevation in analyzing the surface quality of the laminate part.

Method for analyzing the surface quality of composite laminates

Surface treatment of a tubular surface defining an axis extending from a first surface end to a second surface end includes partially surrounding the tubular surface, at a first position, with a first set of treating units, with the treating units arranged in a first arcuate array. Furthermore, each treating unit is configured to include a plurality of first applicator heads. In some examples, a position of each of the plurality of first applicator heads is determined relative to the tubular surface. The first set of treating units is moved from the first position towards a second position. In one non-limiting example, each of the plurality of first applicator heads is independently controlled to selectively apply a first treatment as the first set of treating units moves from the first position towards the second position.

Integrated automation of paint processes incorporating arrayed painting and inkjet printing

A method and apparatus for forming a composite object. A first plurality of tows is laid up over a tool according to a first path. A second plurality of tows is laid up over the tool according to a second path. A first portion of the first plurality of tows runs non-parallel to a second portion of the second plurality of tows. First ends of the first portion of the first plurality of tows and second ends of the second portion of the second plurality of tows meet at a merge zone along the tool to form a ply of a composite laminate.

Automated manufacture of complex contoured composite parts

A process and system for improving surface quality of composite structures, including laying up a first set of composite plies including a first outer ply of a first composite structure. A first intermediate surface of the first outer ply is measured to form a first set of measurements. A laydown surface for a tool path of a composite placement machine is modified to form a modified tool path, wherein modifying the laydown surface comprises modifying the laydown surface such that a laydown surface of the modified tool path matches the first set of measurements. A composite ply is laid down using the composite placement machine and the modified tool path.

Process and system for improving surface quality of composite structures

A method and system for forming a composite laminate. A layup plan is generated for laying up a plurality of plies having a plurality of merge zones, each ply of the plurality of plies having a corresponding merge zone at which ends of a first plurality of tows for each ply and ends of a second plurality of tows for each ply meet. The locations of the plurality of merge zones are offset relative to each other through a thickness of the composite laminate. The plurality of plies is then laid up according to the layup plan to form a composite laminate.

Method and system for generating a layup plan for forming a composite laminate

A method of treating a tubular surface which defines an axis extending from a first surface end to a second surface end includes partially surrounding the tubular surface, at a first position, with a first set of treating units, with the treating units arranged in a first arcuate array. Furthermore, each treating unit is configured to include a plurality of first applicator heads. Additionally, an embodiment of the method includes determining a position of each of the plurality of first applicator heads relative to the tubular surface and moving the first set of treating units from the first position towards a second position. In one non-limiting example, the method further includes independently controlling each of the plurality of first applicator heads to selectively apply a first treatment as the first set of treating units moves from the first position towards the second position.

A method for forming a structural member and a structural member produced thereby includes positioning a first composite section and a second composite section within a tool. The tool has an inner surface and a wall intersection and is supported by a tool platform. The tool platform and a pressure platform are relatively movable between an open position and a closed position. The tool has a non-planar outer surface against which the member may be pressed. A composite splice member is positioned at least partially overlapping both the first composite section and the second composite section to form a joint in the composite structural member. The composite structural member is pressed against the non-planar outer surface of the tool by applying pressure to the joint from a pressure bladder. Heat is applied to the composite structural member at the joint to cure the composite splice member to the first composite section and the second composite section.

Aircraft skin attachment system

A method and apparatus for performing an operation on a structure. In one illustrative embodiment, an apparatus comprises a tool system and a movement system. The tool system is configured to perform an operation at a location on a structure. The movement system is configured to move the tool system along an elongate frame on the structure to the location.

Small frame crawler system

A method for assembling wings includes supporting a pair of wing spars, which include a plurality of coordination features, upon a pair of stanchions in a generally horizontal position. A plurality of ribs and wing panels are accurately fastened to the pair of wing spars at a first workstation using the coordination features to position accurately the parts. The combination is transferred to downstream workstations via a ground transport vehicle for further processing and assembly to define a pulsed flow wing assembly system.

Single piece flow based wing assembly system

Growing community of inventors

Sammamish, WA, United States of America

Luis A Perla