The Boeing Company

Jonathan Y Ahn

Davis Tran

Shane Edward Arthur

Ricardo Andreas Fritzke

Joseph D Anderson

Long H Ly

Shuonan Dong

Chace Wilcoxson

Christopher Robert Brown

Darrell Darwin Jones

Jonathan A Santiago

Lisa Christina Carlson

Scott Edward Krajca

Silas Lawton Studley

Daniel J Cowan

Christopher Ralph Brown

Christopher R Loesche

Daniel James McMillan

Robert William Whiting

Bonnie Ann Keefe

Gregory R Klempel

Austin T McAnelly

Jacob E Koopmans

John D Sailing, Sr

Deborah A Fisher

Austin B Ball

Barton Stevens

An ultrasonic injection device and methods of use are presented. The ultrasonic injection device comprises a housing, an injection nozzle attached to the housing, an ultrasonic vibration generator attached to the housing, and a pressure applicator. The injection nozzle has a number of openings configured to dispense a fluid. The ultrasonic vibration generator is configured to apply ultrasonic energy to fluid within the injection nozzle. The pressure application is configured to propel the fluid towards and out of the number of openings.

Ultrasonic injection device

Systems for forming composite parts, methods of forming composite parts, and methods of precisely performing a plurality of operations on a composite part. The systems include a layup mandrel that includes a mandrel body and a plurality of regions of isotropic surface finish. The methods of forming the composite part include positioning a plurality of plies of composite material on a layup mandrel, conforming the plurality of plies of composite material to a layup surface shape of the layup mandrel, and curing the plurality of plies of composite material. The methods of precisely performing the plurality of operations on a composite part include detecting a corresponding imprinted feature of a plurality of imprinted features, aligning an operating assembly of an end effector relative to the corresponding imprinted feature, and performing a corresponding operation of the plurality of operations on the composite part.

Systems for forming composite parts, methods of forming composite parts, and methods of precisely performing a plurality of operations on a composite part

Conduit coupling devices comprise a body configured to be selectively attached to engage an outer surface of a conduit; and an elongate connecting member extending from the body or configured to selectively extend from the body. Systems comprise at least two conduit coupling devices. Methods comprise attaching a first conduit coupling device to a first conduit; attaching a second conduit coupling device to a second conduit; operatively attaching the first conduit coupling device to the second conduit coupling device; translating the first conduit coupling device and the second conduit coupling device toward each other to operatively position the first conduit relative to the second conduit; and clamping the first conduit to the second conduit.

Conduit coupling devices, systems for coupling conduits together, and methods of coupling conduits

A fastener includes a sleeve, a pin, and a visual indicator. The sleeve includes a tubular body. The pin includes a shank. At least a portion of the shank of the pin is configured to extend through the tubular body of the sleeve and to facilitate deformation of a portion of the tubular body into a bulb in response to a force applied to the tubular body of the sleeve by the shank of the pin. The visual indicator is configured to provide a visual verification of correct formation of the bulb.

Fasteners with visual indication of correct installation and method for fastening

Systems and methods are provided for facilitating pick and placement of preforms. One embodiment is a method for picking and placing a preform. The method includes placing an inner surface of a first caul plate into contact with a first side of a stringer preform, such that an outer surface of the first caul plate forms a first plane that is uniform along a length of the stringer preform, placing an inner surface of a second caul plate into contact with a second side of the stringer preform, such that an outer surface of the second caul plate forms a second plane that is parallel to the first plane along a length of the stringer preform, grasping the caul plates at the first plane and the second plane along the length of the stringer preform, and lifting the stringer preform together with the caul plates while maintaining the grasp.

Caul plates for preforms that undergo pick and placement

There is provided an automated removal apparatus for selectively removing one or more trimmed portions of a laminated ply in a ply-by-ply fabrication process. The automated removal apparatus includes a rotatable reel having a plurality of retractable vacuum panels attached around the rotatable reel. Each retractable vacuum panel has one or more retractable vacuum pad assemblies, and each retractable vacuum pad assembly has a vacuum pad with a vacuum port and a self-sealing valve. The automated removal apparatus further includes actuator assemblies attached to the plurality of retractable vacuum panels, friction reducing elements attached around the rotatable reel, a drive assembly attached to the rotatable reel, and a pneumatic system attached to the rotatable reel and including a valve manifold operable to control an air flow to the actuator assemblies and to one or more vacuum generators to generate a vacuum flow.

Automated removal apparatus, system, and method for selectively removing trimmed portions of a laminated ply in a ply-by-ply fabrication process

The magnetic handling systems comprise a bladder and a magnetic carriage system. The bladder is configured to be received within a stringer interior volume of a hat stringer and comprises a magnetic insert having a plurality of magnetic walls, each configured to align with a respective wall portion of the hat stringer. The magnetic carriage system comprises a carriage having a magnetic head that comprises a bracket and a plurality of magnetic sources supported by the bracket. Each magnetic source is configured to magnetically couple with a respective magnetic wall of the magnetic insert to produce an attractive magnetic force therebetween. The methods comprise disposing a bladder having a plurality of the magnetic inserts within the hat stringer, magnetically engaging a plurality of the magnetic heads with the plurality of magnetic inserts, and conforming the hat stringer by moving at least one magnetic head relative to another magnetic head.

Magnetic handling systems for hat stringers and related methods

Methods of forming a curvature into a composite stiffener and a forming tool are presented. The composite stiffener is positioned in a forming region created by a base assembly and an upper assembly. A first airflow is applied through the material of the base assembly. A second airflow is applied through the material of the upper assembly. A plurality of brackets of the upper assembly is moved relative to each other to change a curvature of the forming region along a length of the forming region to form the curvature into the composite stiffener.

Forming tool and methods for forming a curvature into a composite stiffener

A system includes a U-shaped chute, one or more feeder mechanisms, a sock application assembly, and a film application assembly. The chute has a chute inlet and a chute outlet and is configured to receive a mandrel having a mandrel length. The one or more feeder mechanisms are configured to move the mandrel into the chute inlet and through the chute. The sock application assembly has a sock material spool containing a breather sock in tubular form. The sock application assembly is configured to progressively apply the breather sock over the mandrel length as the mandrel exits the chute outlet. The film application assembly has a film material spool containing a film in tubular form. The film application assembly is configured to progressively apply the film over the breather sock covering the mandrel exiting the sock application assembly to thereby form a film-sock-mandrel assembly.

Automated system and method for preparing a mandrel for use in composite stringer manufacturing

An ergonomic frame-filler placement tool is manually operable to supply a vacuum fluid flow at a distal end of the tool that can be used by a worker to pick up and hold a piece of frame-filler material to the distal end of the tool, which enables the worker to manipulate the tool to position the piece of frame-filler material over a desired location of a fuselage mandrel and then manually stop the vacuum fluid flow at the distal end of the tool to position the piece of frame-filler material at the desired location on the mandrel.

Ergonomic frame-filler placement tool for manual installation

A stiffener composite charge placement system is presented. The stiffener composite charge placement system comprises a longitudinal end effector having a first attachment point and a second attachment point; a first rotational arm having a first connector configured to connect to the first attachment point; a first movement system configured to move the first rotational arm within a manufacturing environment; a second rotational arm having a second connector configured to connect to the second attachment point; and a second movement system configured to move the second rotational arm within the manufacturing environment.

Stiffener composite charge application system

Disclosed herein is an apparatus for removing material from a surface of a carrier. The apparatus comprises a buckling mechanism that comprises a gripper configured to engage the material. When engaged with the material, the gripper is movable relative to the surface of the carrier to move the material relative to the surface of the carrier and to form a buckle in the material. The apparatus also comprises a separation mechanism that is coupled to the buckling mechanism and comprises a wedge that is movable relative to the surface of the carrier to be insertable into the buckle formed in the material.

Material removal apparatus, system, and method

Systems and methods are provided for active vibration damping. One embodiment is a method for damping vibration in a mechanical system. The method includes detecting a vibration at a coupling of the mechanical system, generating a countervibration based on the detected vibration, and operating the mechanical system while generating the countervibration.

Growing community of inventors

Seattle, WA, United States of America

Jonathan Y Ahn