The Boeing Company

Tanni Sisco

Kwok Tung Chan

Monica Joy Brockway

Jeffrey A Wilkerson

Eric M Reid

Blake Alexander Simpson

John Hartmann

Jeff Devlin

Jeffrey Devlin

Fei Cai

Scott Charles Tomchick

Paul E Ffield

Skye Jenkins

Brendan Elmore

Frank Charles Mestemacher

Richard Bruce Tanner

Sean Dennis Morden

Mark Albrecht

Antonio Carlos Rufin

Joe Heeter

Nathan A Muntz

Dale Winter

Kwok-Tung Chan

Matthew Ryan Dunaj

Brian Joseph Cobb

Jeffrey Martin Devlin

Darrell Darwin Jones

Daniel R Smith

Clayton Lynn Munk

Paul Reed Stone

Edward John Batt

Everette Desmond Gray

Riley Harrison HansonSmith

Daniel Richard Smith, Jr

James C Murphy

Thomas Dee Hall

Randy Woolridge

Samuel Edward Antonucci

Craig Roedel

Todd E Hubbell

Todd Christopher Grossaint

Mark William Brown

Michael George Payionk

Justin Ronald Via

Victor Joseph Bolton

Eric Scott Patton

Skye Sutherland Jenkins

Jeffrey Alan Wilkerson

Jeffrey M Devlin

Everette D Gray

Daniel Richard Smith Jr

Kowk Tung Chan

Riley Hansonsmith

A structural blind sleeve includes a monolithic body. The monolithic body has a sleeve shank having an elongated tubular structure defining a proximal portion and a distal portion, the sleeve shank having a structural portion proximate the proximal portion, a threaded portion proximate the distal portion, and a softened portion between the structural portion and the threaded portion. The structural portion is capable of carrying a clamp-up structural load. The monolithic body further includes a sleeve head connected to the proximal portion of the sleeve shank.

Structural blind sleeves and associated systems and methods for clamping a first structure relative to a second structure to yield a clamped-up structure

A blind fastener includes a sleeve defining a sleeve central axis and having a sleeve shank having a distal end portion and a proximal end portion axially opposed from the distal end portion and a stop connected to the distal end portion of the sleeve shank. The sleeve defines an eccentric through-bore that extends along a through-bore axis from the proximal end portion to the distal end portion. The blind fastener includes a core bolt at least partially received in the eccentric through-bore of the sleeve, defining a core bolt central axis. A core bolt shank has a distal end portion, a proximal end portion axially opposed from the distal end portion, and a threaded portion. A core bolt head is connected to the proximal end portion of the core bolt shank. An eccentric nut is threaded into engagement with the threaded portion of the core bolt shank.

Blind fasteners and associated systems

Systems and methods are provided for inspecting installation of a fastener. One method includes monitoring hydraulic pressure of a tool that is installing the fastener, detecting that the hydraulic pressure has dropped by more than a threshold amount within a period of time, determining that a pintail of the fastener has snapped in response to the detecting, and reducing the hydraulic pressure in response to the determining.

Sensor based control of swage tools

A method for installing a fastener system. A position on a structure relative to an overhang on the structure is automatically sensed for installing a fastener system in a hole using an offset collar installer. The offset collar installer is moved about a rotation axis to the position such that a collar in the fastener system is held in the position over the hole. The offset collar installer is connected to a platform and rotatable about the rotation axis. The collar is fastened to an engagement feature for a bolt in the hole.

Fastener installation

A compound contour vacuum track, and an automated fastening machine using the track, for automation of final assembly inside an aircraft fuselage. The track is mounted at an angle to a surface, such as an inside surface of the fuselage, wherein the surface has one or more holes through which fasteners are inserted. The automated fastening machine is mounted on the track to traverse the track while performing fastening functions and steps. The automated fastening machine includes a carriage, arm, and end effector, wherein the arm is mounted on the carriage and the end effector is mounted on the arm. The carriage is attached to the track for positioning the arm and end effector, the arm is attached to the carriage for positioning the end effector, and the end effector is attached to the arm for installing the fasteners into the holes of the surface.

Compound contour vacuum track for automation of final assembly from the interior of a fuselage

Systems, methods, and apparatus for a detector and reflector for automation cell safety and identification are disclosed. In one or more embodiments, a method for machinery safety comprises transmitting, by an active transponder, at least one interrogation signal. The method further comprises receiving, by at least one passive transponder located on a user or on an item, the interrogation signal(s). Also, the method comprises generating, by a non-linear device of the passive transponder(s) in response to the interrogation signal(s), at least one response signal. In addition, the method comprises receiving, by the active transponder, the response signal(s). Additionally, the method comprises determining, by at least one processor, a location of the passive transponder(s) based on the response signal(s). Further, the method comprises determining, by the processor(s), whether the passive transponder(s) is located within a threshold distance away from machinery by using the location of the passive transponder(s).

Detector and reflector for automation cell safety and identification

An end effector provides one up assembly drilling through mated components, including a panel, by preloading the components. The end effector includes a drill and clamp dispenser for temporarily inserting and removing expansible single-sided clamps at various pre-drilled locations in the panel. In one method, pilot holes are first pre-drilled into mated components, for example an aircraft wing panel and a wing rib or spar; an initial pilot hole location is identified, and an expansible clamp is inserted into a pilot hole adjacent a desired initial fastener hole location. The clamp is torqued, causing its expansion for preloading the wing panel and rib and/or spar components under a predetermined load. The fastener hole is then drilled, the end effector untorques and removes the clamp and identifies a second (and/or next) pilot hole location, and the process is replicated.

One up assembly aircraft panel drilling system

Systems and methods are provided for fastening via a swage tool. One embodiment is a method for fastening via a swage tool. The method includes steps of selecting a hole located at a part, aligning an axis of a lockbolt collar with a center of the hole, placing the lockbolt collar flush against the part at a first end of the hole, and swaging the lockbolt collar onto a lockbolt that has been driven through the hole. This securely fastens the lockbolt collar to the lockbolt.

Offset collar delivery for swage tools

Systems and methods are provided for fabricating fasteners. One embodiment is an apparatus that includes a fastener. The fastener includes a head, a cylindrical shank that extends from the head and is dimensioned to engage in a fit with a corresponding hole, and a coating that is discontinuously speckled around a circumference of the shank and extends axially along the shank, leaving irregular portions of a surface of the shank exposed. The coating exhibits a higher lubricity than the surface, and the coating exhibits a higher dielectric withstand voltage than the surface.

Fasteners having enhanced electrical energy dispersion properties

An indexing pin comprises a central axis. The indexing pin further comprises a threaded portion, extending along the central axis. The indexing pin also comprises a stem, extending along the central axis opposite the threaded portion. The indexing pin further comprises a cylindrical surface, extending along the central axis between the threaded portion and the stem. The indexing pin further comprises a tapered surface, extending between the threaded portion and the cylindrical surface. The indexing pin further comprises a flange, located between the stem and the cylindrical surface.

Indexing pins and indexing clamps for aligning a first body and a second body of a structure

An assembly comprising first and second structural elements having aligned holes, a fastener that occupies at least respective portions of the holes without a surrounding sleeve, and a mating part that is coupled to the fastener. The fastener comprises: a head; a circular cylindrical shank extending from the head; a mating portion comprising external projections; and a transition portion disposed between the shank and the mating portion. The transition portion comprises a tapered lead-in section that meets the shank at a shank/lead-in intersection and a radiused lead-in section that meets the tapered lead-in section. The tapered lead-in section tapers gradually in a first axial direction toward the mating portion and has a first profile that is linear and a taper angle equal to or less than 20 degrees, while the radiused lead-in section curves abruptly in the first axial direction and has a second profile that is a circular arc having a radius.

Tapered lead-in for interference fit fasteners

Systems and methods are provided for fastening via a swage tool. One embodiment is a method for fastening via a swage tool, the method including selecting a hole located at a part; aligning an axis of a lockbolt collar with a center of the hole; placing the lockbolt collar flush against the part at a first end of the hole; and swaging the lockbolt collar onto a lockbolt that has been driven through the hole.

A plug gauge includes a housing, defining an internal volume, first openings, and second openings. The plug gauge includes first contact elements, each at least partially received in a respective one of the first openings. The plug gauge includes a first plunger in the internal volume and movable relative to the housing. The first plunger is biased to urge the first contact elements radially outward through the first openings. The plug gauge includes a first sensor sensing movement of the first plunger. The plug gauge includes second contact elements, each at least partially received in a respective one of the second openings. The plug gauge includes a second plunger in the internal volume and movable relative to the housing. The second plunger is biased to urge the second contact elements radially outward through the second openings. The plug gauge includes a second sensor sensing movement of the second plunger.

Plug gauge and associated system and method for taking multiple simultaneous diametric measurements

An electromagnetic effect suppressing termination part for a fastener formed of a metallic material, the fastener having a head, a shank, and a male threaded portion opposite the head, has a metallic core coated by a layer of dielectric material. An internal bore of the termination part includes an inner wall, a counterbore hole, and a cavity disposed therebetween. An outer surface includes an outer wall, and a frustoconical wall positioned proximally relative to the outer wall, the frustoconical wall extending radially outwardly from the outer wall and having an included angle of less than approximately 90 degrees. A seal is disposed in the counterbore hole, and the frustoconical wall is configured so that a compressive force applied to the frustoconical wall deforms the inner wall to conform to the male threaded portion of the fastener and deforms the seal to fill the cavity.

Electromagnetic effect protective fastener with swageable termination body

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Mukilteo, WA, United States of America

Tanni Sisco