Bucking Bar System

Information

  • Patent Application
  • 20250073775
  • Publication Number
    20250073775
  • Date Filed
    April 12, 2023
    2 years ago
  • Date Published
    March 06, 2025
    3 months ago
  • Inventors
    • LeMieux; David Lawrence (Boulder, MT, US)
Abstract
A Bucking Bar System (BBS) for the assembly of aerospace components by setting solid core rivet fasteners and more specifically a BBS having a sender body or elongated neutral axis to operatively move the system center of mass or centroid near the tool handle, away from the rivet being set. Urging the centroid toward the handle improves technician ergonomics and offers other rivet fastener installation benefits.
Description
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
Not Applicable
THE NAMES OF THE PARTIES TO A JOINT RESEARCH AGREEMENT
Not Applicable
INCORPORATION-BY-REFERENCE OF MATERIAL SUBMITTED ON A COMPACT DISC
Not Applicable
BACKGROUND OF THE INVENTION

The art presented here is a Bucking Bar System (BBS), sometimes referred to as an “end effector”, and more specifically to a BBS having a slender body shape or form factor generally comprised of an anvil face, an elongated shaft, and a handle. The background art generally relates to bucking bar equipment used to set the ubiquitous solid core rivet fasteners or rivets when joining a plurality of work pieces to each other during the aero framing assembly process of aircraft manufacturing. When setting rivets, a pneumatic rivet gun impacts on the rivet manufactured head while the anvil face of the bucking bar is held against the rivet shank end face—this plastically deforms the rivet shank end into a button head to clinch or join the work pieces to each other.


Now to provide more background on prior art bucking bars. When backing the rivet the bucking bar technician must maintain coplanar alignment of the bucking bar anvil face with the rivet shank end face; however, this often requires holding the bucking bar mass an near arm's length distance from their torso and due to the mass of the bar and applied force, this causes worker fatigue. To reduce this fatigue, the technician often positions their body closer to the work; however, this results in poor working ergonomics and sometimes adversely affects the technician's balance.


Bucking bar tools bounce or “buck” from each rivet gun impact and are notorious for causing vibration injury. The technician's fingers, hands, arms, and body damp the bucking vibration which often causes technician injury, sometimes referred to as “white-finger injury”. Further, the bar resonances, producing a high decibel audible noise that causes hearing damage.


Due to bar's “buck” nature a high degree of skill is needed to maintain coplanar orientation of the anvil face to the rivet shank end face because non-coplanar alignment causes the rivet being set a skew angle and rivets set incorrectly require factory rework. Factory rework decreases productivity and can reduce the sales value of the airframe.


The new art presented here optionally incorporates PRIOR ART described in U.S. Pat. No. 9,764,376 and also described in preceding U.S. Pat. Nos. 8,316,524; 8,850,677; 8,978,231 and subsequently awarded international Pats. FR 2,344,234; BR 1,120,150,120,300; CA 2,892,774; and JP 6,177,341. Referencing U.S. Pat. No. 9,764,376 a rivet set tool is provided having an anvil body, a first end of an anvil body, first raised cylinder diameter having a captive shoulder, a second end having an anvil face, and other equipment operative to measure a protruding shank length, to monitor the forming shank length into a button head, and to control the rivet set process including enabling and disabling the rivet gun. This prior art provides automation capability to automatically control the button head formation and it's optional use is presented later.


The new art presented here also optionally incorporates PRIOR ART back riveting rivet set equipment viewable at website: www.aircraft-tool.com or found using web search key terms “back rivet set”. Features of this PRIOR ART back riveting rivet set equipment include an anvil body, a universal size (e.g. a “401” size) shank at a first end of the anvil body, an anvil face at the second end of the anvil body, located along the length of the anvil body a first raised cylinder diameter having a capture shoulder, a slotted plunger retained on anvil body by a pin, and spring or load source used to urge plunger nominally away from the anvil face. This equipment is conventionally installed in the rivet gun to backset rivets (deforming the shank end into a button head) while the manufactured rivet head is “backed” by a “back riveting plate”. This back rivet set equipment is referred to as PRIOR ART back riveting rivet set subsystem and it's optional use is presented later.


Those skilled in the art will readily recognize that the new BBS provided here offers many new benefits over prior art by use of a handle, an elongated shaft, and an anvil face to plastically deform the rivet shank into a button head. The elongated shaft provides a long moment arm to aid tool alignment and provide better working ergonomics. This configuration provides improved coaxial alignment of the BBS centroid between the anvil face and the handle and also moves the mass centroid closer to the handle to improve technician ergonomics. The PRIOR ART disclosures described above, of which are incorporated by reference as if fully set forth herein.


PRIOR ART bucking bar equipment inadequately prevents bucking bar vibration and does not allow for good working ergonomics or tool control resulting in worker fatigue and requiring a high level of skill to set rivets. Tool vibration and the bucking nature of the bucking bar makes it difficult to control, to maintain coplanar alignment, and causes worker injury. However, given the teachings provided here, those skilled in the art will recognize the new embodiment teachings as alternative improved ways to reduce technician fatigue, reduce injury, improve working ergonomics, improve rivet set quality, damp vibration, and avoid rivet set errors.


BRIEF SUMMARY OF THE INVENTION

The BBS provided herein aids technicians when setting solid core rivets during the assembly of aircraft components. The BBS departs from all conventional bucking bars by its slender body shape or form factor (characterized particularly by an elongated shaft member). The BBS also has a handle and an anvil face. Optionally the PRIOR ART referenced above can be coupled to a shaft end to provide automated rivet setting and/or in the case of the back-set prior art, to provide a shroud to prevent the anvil face from slipping off the rivet shank end face. The plunger shrouds prevent the anvil face from slipping of the rivet shank end face while the rivet is being set.


In a first object of the preferred embodiment the BBS is comprised of a handle, an elongated shaft, and an anvil face; this configuration is a slender body. In this preferred embodiment, a coupler subsystem is used to coaxially join the PRIOR ART automated rivet set tool subsystem and to join the elongated shaft and handle subsystem to each other. This arrangement comprises the handle, elongated shaft, and anvil face; however, the PRIOR ART subsystem provides automated rivet setting capability. This configuration provides the following advantages over all PRIOR ART bucking bars.


First, with the subsystems coupled together the BBS has rivet setting automation capability. Automation in factory assembly areas is critical to remaining competitive.


Second, this configuration makes the BBS take a slender body shape or form factor and moves the BBS center-of-mass or centroid away from the anvil face and towards the handle. Also, by the nature of the slender body shape, the BBS mass is coaxially aligned between the anvil face and the handle. This mass location reduces angular moment forces in the BBS, as a kinematic response from rivet gun impact blows and makes the tool easier to control and maintain proper alignment.


Third, by moving the BBS centroid closer to the handle, the mass also gets closer to the worker's torso feature. This allows the technician to position most of the bucking bar mass near their torso to reduce worker fatigue and serves to improve worker body posture or ergonomics.


Fourth, the slender body form factor of the BBS resulting from the elongated shaft is a configuration that aids maintaining coplanar alignment of the BBS anvil face and the rivet shank end face, to each other—while driving a rivet. When in use the technician holds the handle with one hand and supports the anvil with the other hand. The elongated form factor of the BBS provides a geometry that requires a large angular position change at the handle end to create small misalignments between the anvil face and the rivet shank end face. This is a key advantage and distinguishing feature of this invention over prior art.


The elongated configuration of the BBS requires a technician to move the handle a large angle distance with respect to the rivet shank axis to produce a small misalignment between the planes of the anvil face and the rivet shank end face. This further improves the measurement accuracy of the PRIOR ART rivet set tool subsystem when measuring the forming button head height because non-coplanar alignment of these surfaces also can produce non-coplanar mating of the plunger distal end and the aircraft surface, nominally the aircraft surface should and the distal end of the plunger should be maintained in flush contact with each other when the rivet is being set.


Fifth, the co-axial alignment of the BBS shaft and handle and BBS mass with the rivet shank requires bucking forces to move the entire BBS mass as a result of each hammer blow. This configuration reduces vibration from the hammer blow impulse forces, specifically reducing vibration amplitude.


Sixth, the co-axial alignment also reduces angular vibration response forces which aids tool position control. In conventional bucking bar tools this co-axial alignment is not as pronounced which causes a rotational bucking motion in conventional bucking bars that produces rivet set errors. Further by eliminating the described rotational response motion, this configuration also ensures the entire BBS mass is used to buck the rivet and consequently fewer rivet gun impact blows are used to set the rivet, resulting in an installed rivet having improved rivet fastener material strength properties because the rivet shank undergoes fewer hammer blow fatigue cycles during the plastic deformation rivet set process. The set rivet using the BBS is a higher quality rivet.


Seventh, the elongated shaft configuration and centroid mass location damps resonance vibration better than conventional bucking bar tools to improve worker safety. Common technician injuries from bucking bar tools includes hearing loss from bucking bar acoustic noise (bucking bars often “ring like bell”) and vibration injury to fingers, hands, arms, and joints often referred to as “white-finger injury”.


Eighth, the elongated shaft configuration allows vibration damp equipment to be installed on the tool to reduce the fundamental frequency caused by the rivet gun impact blows and the resonance vibration, caused by anvil chatter on the rivet shank end face, between impact blows, and caused by resonance vibration of the BBS. This reduces injury and aids the technician when maintaining proper bucking bar position/alignment during the rivet driving or rivet set phase.


In a second object and alternated embodiment of the BBS, the PRIOR ART automated rivet setting subsystem is replaced with the PRIOR ART back set apparatus. Except for the automation capability this is the same as the first object, presented above.


In a third object of the preferred embodiment of the BBS, a carbon fiber shaft is used to further move the centroid mass closer (as near as possible) to the handle. The carbon fiber shaft material properties also serve to additionally damp vibration forces from the rivet gun to help technicians control the “bucking” tool while the rivet is being set and to further improve safety through less vibration, less acoustic noise, and improved technician body position and working ergonomics.


In a fourth object and alternate embodiment of the BBS, shaft and/or handle surfaces (possibly including the shaft cavity) can be coated or filled with materials having properties that passively damp vibration.


In a fifth object and alternate embodiment an elongated slender body BBS is provided comprising an anvil face at a first end of an elongated shaft and a handle at a second end of the elongated shaft. Optionally, the anvil face may include a recess or pocket to prevent the rivet shank end from slipping off the anvil face as the rivet is being set. Preferably, the pocket depth is less than the height of the desired set button height, to prevent damage to the aircraft surface. In use the technician supports and positions the BBS with respect to a rivet to be set by locating the anvil face onto the shank end of the rivet and orientating the handle into a position that orthogonally positions the anvil face to the rivet shank end. The technician applies coaxial force through the BBS so that the applied force passes through the rivet shank axis.


In a sixth object and alternate embodiment, a tuned mass damper (TMD) device consisting of a mass, a spring or load source, and a damper is attached to the BBS in order to attenuate three vibration frequency responses produced by a pneumatic hammer blow: In the first case, a first TMD is used to attenuate a first frequency dynamic response formed by BBS's resonance natural frequency. In the second case, a second TMD is used to attenuate a second frequency dynamic response of the BBS's bouncing or “bucking” frequency as the BBS's anvil face returns to rest upon the rivet shank end. In the third case, a third TMD is tuned to match the rivet gun hammering frequency to attenuate a third frequency dynamic response of the BBS from the rivet gun impact blows (though not limiting pneumatic rivet guns impact rate ranges from about 20 to 50 Hz). All three described frequencies are excited by the impulse force of hammer blows.


Returning to the first case: The impulse energy from each hammer blow causes the BBS to vibrate at or near the gun's impact frequency. In this case the frequency of a first TMD is tuned to match or to be similar to the structural resonant frequency of the BBS. Operatively when the BBS resonance first frequency is excited, the TDM will resonate out of phase with the first frequency. So, although the inertia force from a hammer blow causes the BBS to resonate, the TMD dissipates energy or damps the resonant first vibration of the BBS.


Now returning to the second case: The impulse energy from each hammer blow also “bucks” the BBS's anvil face off the shank end of the forming rivet head and prior to the next impact the anvil face bounces (vibrates) as it attempts to return to a steady-state rest on the shank end before the next hammer blow, as a result of the technician's applied force (load source) to the bucking bar. Operatively when the BBS bouncing second frequency is excited, the second TDM will resonate out of phase with the described bouncing frequency to damp the second frequency.


Now returning to the third case: When in use the rivet gun produces a burst of impact blows that correspond to the hammering rate (gun frequency) and impact force (frequency amplitude) are dominantly a function of the gun size and BBS mass. The third TMD will resonate to the natural frequency of the BBS. To damp the BBS vibrations described as first, second, and third vibration frequencies enables technicians to better control the tool position and reduces vibration injury. Those skilled in the art will recognize that TMD devices can be attached to the BBS's elongated shaft, to the shaft outside diameter or preferably to the shaft inside cavity, or alternately to the handle. TMD concepts have been applied since 1909 to reduce the rolling motion of ships at seas and have many other well-known applications.


Those skilled in the art will recognize the many benefits of the slender body BBS configuration also distinctly differentiated it from conventional bucking bars. Upon assembly of the preferred embodiment, the PRIOR ART set tool subsystem, coupling subsystem, and bucking bar subsystem are coaxially joined together. In use the technician positions the BBS anvil face on the rivet shank end, nominally forming a coplanar alignment of these surfaces to each other; the technician orbits the handle above the rivet until coplanar alignment is achieved and then applies coaxial force through the BBS so that the applied force passes through the shank end and rivet shank axis while the rivet is being set.


As used herein, the following terms and variations thereof have the meanings given below, unless a different meaning is clearly intended by the context in which such term is used:


“Anvil face” means a rivet impacting surface of an anvil on a bucking bar or a set tool.


“Resilient member” means a “load source” and may be understood as a force applying system or component; for example a spring.


“Tuned Mass Damper” or “TMD” means a harmonic resonance absorber or damper and is an attached device to reduce mechanical vibrations, generally consisting of a mass mounted on one or more damped springs or damped load sources.


“Slender body” is also an “elongated body” and means a mechanical body that is substantially longer than it is wide and by definition a slender body has a high slenderness ration (L/r), where L is the nominal length and r is the nominal radius of the BBS. Though not limiting and for purposes of illustration to help distinguish this new art from prior art, the slenderness ratio of the new art may range from 6 to 45 while the slenderness ratio of conventional bucking bars may range from 1 to 6.


“Neutral axis” means the line nominally formed by the elongated central axis or axial axis of a slender body.


The BBS in these teaching used to set a solid core rivet fastener that has a rivet manufactured head, a shank, a shank face, and a shank neutral axis. When fastened the shank end rivet plasticly deforms into a button head to join a plurality of work pieces to each other. The BBS equipment is comprised of an elongated shaft having a first end and a second end with an anvil face located at the first end the shaft and an anvil located at said second end of said shaft.


The BBS is long, forming a slender body with a length to radius (L/r) slenderness ratio greater than six. This geometry operatively places mass centroid of the bucking bar system toward the handle and away from the anvil face; this aids colinear alignment of said bucking bar system with said rivet shank and ergonomics. The arrangement also requires a large angular pivot rotation of said handle over said rivet to substantially misalign the anvil face relative to the rivet shank face. This prevents rivet setting errors due to skew alignment. In addition, the arrangement also substantially (i.e. predominately) coaxially aligns the mass of the BBS with the rivet shank. This reduces vibration because the impact force from the rivet gun must displace the entire BBS.


The BBS preferably has a tubular shaft this is operative to damp vibration from rivet tool impact blows and to position the mass centroid proximal to the handle.


In the preferred embodiment a coupler subsystem is used to join a PRIOR ART subsystem comprised an automated rivet set tool subsystem or a back set tool subsystem to a shaft/handle subsystem. The shaft of the shaft/handle subsystem mates with the shaft of the PRIOR ART subsystem in a coaxial arrangement to form a rigid body between these subsystems.


The BBS is always comprised of an elongated shaft and an anvil face at the first end and a handle at the second end. Operatively this locates the BBS's mass centroid proximal to said handle and away from said anvil face to coaxially align the said rivet shank with said elongated shaft. This geometric arrangement requires a large angular motion the handle with respect to the neutral axis of the rivet shank, when positioning the BBS over a rivet; therefore, improper coplanar misalignment between the shank end and the anvil face becomes less probable.


A coupler subsystem is used to coaxially join the PRIOR ART subsystem(s) to the shaft/handle subsystem. In this case the PRIOR ART subsystem can comprised of a set tool having a set tool shoulder and a first distal end and an anvil face located at a second distal end of said set tool. Further the shaft/handle subsystem is further comprised of a shaft with a first end and a second end, a handle that is affixed to the first end of the shaft, and a pocket is located proximal to the second end of the shaft. Also, a set of external threads are also located proximal to the second end of the shaft. Next the coupler also has internal through hole cavity, a group of internal threads, and a coupler shoulder for joining the PRIOR ART subsystem to the shaft/handle subsystem. Upon coupling assembly, the described internal and external threads are engaged which urges a set tool shoulder and a coupler shoulder toward other until the first end of the set tool seats into the pocket located at the end of the shaft. When the PRIOR ART subsystem shaft and the shaft/handle subsystem shaft become coaxially coupled or joined to each other forming a rigid body BBS.


Further aspects of the invention will become apparent from consideration of the drawings and the ensuing description of preferred embodiments of the invention. A person skilled in the art will realize that other embodiments of the invention are possible and that the details of the invention can be modified in a number of respects, all without departing from the disclosed concepts. Thus, the following drawings and description are to be regarded as illustrative in nature and not restrictive.





BRIEF DESCRIPTION OF THE DRAWINGS

The features of the invention will be better understood by reference to the accompanying drawings which illustrate presently preferred embodiments of the invention. In the drawings:



FIG. 1A presents an isometric view of a PRIOR ART automated rivet set tool subsystem.



FIG. 1B presents an isometric view of a PRIOR ART back riveting rivet set subsystem.



FIG. 1C presents an isometric view of a BBS with PRIOR ART automated rivet set tool subsystem depicted in FIG. 1A.



FIG. 2A presents an isometric view of a PRIOR ART rivet set tool subsystem with a coupler.



FIG. 2B presents an isometric view of a PRIOR ART rivet set tool subsystem with coupler subsystem.



FIG. 2C presents a side view of preferred embodiment first BBS, depicting PRIOR ART rivet set tool subsystem with coupler subsystem and elongated shaft with handle subsystem.



FIG. 3 presents a side view of and alternate embodiment second BBS.



FIG. 4A is a diagram of coaxial motion tuned mass damper coupled to BBS.



FIG. 4B is a diagram of pendulum motion tuned mass damper coupled to BBS.





The following reference numerals are used to indicate the parts and environment of the invention on the drawings:

    • PRIOR ART FIG. 1A
    • 2 PRIOR ART drawing of rivet setting tool, PRIOR ART rivet set tool, PRIOR ART rivet set, PRIOR ART automated rivet set tool, PRIOR ART rivet set subsystem;
    • 4 anvil body, anvil;
    • 6 first end of an anvil body, first end of anvil, first end;
    • 8 feature of anvil body depicting a shoulder, first capture shoulder, first anvil shoulder;
    • 10 housing, housing assembly;
    • 12 plunger, plunger assembly;
    • 14 plunger face, plunger distal end;
    • 16 feature of anvil body 4 depicting anvil face, anvil second end, anvil face;
    • 18 bolt fastener, fastener;
    • 20 cover, cap;
    • 22 plug, electrical receptacle, multi-conductor receptacle;
    • PRIOR ART FIG. 1B
    • 24 PRIOR ART back riveting tool, PRIOR ART back rivet set tool, PRIOR ART back set, PRIOR ART back rivet set subsystem;
    • 25 compression spring, spring, load source
    • 26 second anvil shoulder, second capture shoulder;
    • 27 plunger shoulder;
    • 28 slotted plunger
    • 29 role pin, pin
    • FIG. 1C
    • 5 Slender Body bucking bar, elongated bucking bar, bucking bar system, BBS, PRIOR ART automated rivet set tool subsystem with coupler subsystem and elongated shaft and handle subsystem;
    • FIG. 2A
    • 30 subassembly of PRIOR ART automated rivet set tool subsystem and coupler, first subassembly;
    • 32 coupler tool, coupler;
    • 34 recess or cavity in coupler body, cavity;
    • 36 coupler internal threads, internal treads (thread location depicted but threads not show for simplicity);
    • 38 feature of coupler depicting a shoulder, coupler shoulder;
    • FIG. 2B
    • 40 subassembly of PRIOR ART automated rivet set tool subsystem and coupler subystem, subassembly of rivet set tool and coupler and coupler mate, second subassembly;
    • 42 coupler mate component, coupler mate;
    • 44 external face of protruding cylinder, coupler mate cylinder face, cylinder face;
    • 46 feature of coupler mate depicting shoulder, coupler mate shoulder;
    • 48 feature of coupler mate depicting externally threaded cylinder, externally threaded cylinder;
    • FIG. 2C
    • 50 subassembly of PRIOR ART automated rivet set tool subsystem with coupler subassembly and shaft with handle subassembly, BBS, slender body bucking bar, first BBS, third subassembly, first BBS;
    • 52 preferred embodiment of slender body bucking bar, slender body bucking bar, slender body bucking bar subsystem, elongated bucking bar subsystem;
    • 54 slender body tubular shaft, extended length tubular shaft, tubular shaft, shaft;
    • 56 first end of shaft;
    • 58 second end of shaft;
    • 60 handle transition component;
    • 62 protrusion feature of handle transition component, stem;
    • 64 handle;
    • FIG. 3
    • 70 alternate embodiment of slender body bucking bar, second BBS;
    • 72 slender body rod, extended length rod, rod, solid shaft, shaft;
    • 74 first end of solid shaft;
    • 76 second end of solid shaft;
    • 78 solid shaft protrusion, shaft protrusion;
    • 80 pocket in handle, handle pocket;
    • 82 anvil face pocket;
    • FIG. 4A
    • 100 Tuned Mass Damper (TDM) system, first TDM system
    • 102 first load source
    • 104 second load source
    • 106 first damper
    • 108 second damper
    • 110 mass
    • 112 first oscillatory motion, first motion
    • FIG. 4B
    • 120 Tuned Mass Damper (TDM) system, second TDM system
    • 122 second oscillatory motion, second motion


DETAILED DESCRIPTION OF THE INVENTION

The following description of the preferred embodiments of the invention is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses.


Referring to PRIOR ART FIG. 1A the isometric sketch of rivet set tool 2 shows anvil body 4, first end of anvil body 6, a feature of anvil body 4 depicting a shoulder 8 (discussed later), a housing 10, and plunger 12, and plunger distal end 14, a feature of anvil body 4 depicting anvil face 16, bolt fasteners 18 operative to affix cap 20 to housing 10, and an electrical receptacle 22. In operation these components form an assembly capable of monitoring the plastic formation of a solid-core rivet shank into a button head when the rivet is set. The set tool 2 is coupled with other PRIOR ART components including a valve and power supply (not discussed here) to automatically set solid core rivets to desired button head heights.


In operation of set tool 2, plunger 12 slides co-axially over anvil body 4 and after calibration, a sensor inside cap 20 measures axial displacement of plunger 12 relative to fixed frame cap 2 and housing 10 and more specifically measures distance between distal end 14 of plunger 12 and anvil face 16. Although not shown in FIG. 1A, an internal load source nominally urgers distal end 14 of plunger 12 away from housing 10 and beyond anvil face 16. When a rivet is set, distal end 14 is in contact with aircraft surface and the measured distance is representative of the protruding rivet shank or forming rivet button head. Set tool 2 is this operative to measure the protruding rivet shank length, determine a desired button head height, monitor measured distance between anvil face 16 and plunger 12 distal end 14 as the rivet undergoes plastic deformation, and stops the rivet set process when the forming button substantially matches a desired button heat height.



FIG. 1B is PRIOR ART back set tool subassembly 24 having an anvil body 4, first end of anvil body 6, a feature of anvil body 4 depicting a shoulder 8, compression spring 25, second anvil shoulder 26, plunger shoulder 27, slotted plunger 28, pin 29, with plunger 28 having a distal end 14, and anvil body 4 having an anvil face 16. Operatively load source spring 25 urges plunger 28 and plunger distal end 14 away from anvil face 16. PRIOR ART back set tool subassembly 24 is optionally attached by coupling to the elongated shaft and handle of BBS; the coupling function works identical to the equipment described in FIG. 1A and therefore will be discussed using that equipment.


Referring now to FIG. 2A. To begin teaching the coupling assembly of the preferred embodiment described in FIG. 1A, FIG. 2A provides a sketch showing first subassembly 30 comprising automated rivet set tool 2 (described in FIG. 1A) and coupler 32. Coupler 32 body has sidewall pocket 34 to allow first end 6 of anvil body 4 to be inserted into cavity of coupler 32. Coupler 32 also has internal threads 36 (not shown in drawing for simplicity and discussed later), and coupler shoulder 38. On assembly first end 6 of anvil 4 passes sidewall pocket 34 as first end 6 is inserted into coupler 32 cavity until neutral axis of anvil 4 and coupler 32 become coaxially aligned, this position allows shoulder 38 to mate or seat against shoulder 8 of anvil body 4.


Next, in FIG. 2B teaching of the coupling assembly resumes. FIG. 2B is a sketch showing second subassembly 40 comprising rivet set tool 2 described in FIG. 1A, coupler 32 described in FIG. 2A, and coupler mate 42. Coupler mate 42 is a component of the preferred embodiment BBS but is depicted in FIG. 2B to teach coupler system assembly using coupler 22. Coupler mate 42 features a protruding cylinder face 44, shoulder 46, and protruding externally threaded cylinder 48 (threads not shown for clarity). Additionally, though not shown in FIG. 2B for clarity, distal end of protruding externally threaded cylinder 48 also has a pocket that coaxially aligns with the neutral axis of coupler mate 42, the pocket termed a “coupling pocket” serves to receive first end 6 and portion of anvil body 4 shaft. Those skilled in the art will recognize that preferably the coupling pocket and anvil body 6 nest as a close tolerance sliding fit.


Still referring to FIG. 2B, and further upon assembly, coupler mate 42 is threadedly attached to coupler 32 by screwing together external threads on surface of 48 and internal threads 36 on coupler 32 (FIG. 2A). As these threads engage, coupler shoulder 38 is urged towards coupler mate 42 and when shoulder 38 contacts shoulder 8 (of anvil body 4), anvil body 4 is also urged toward coupler mate 42. Threading ceases when anvil body 4 first end 6 seats in bottom of coupling pocket of coupler mate 42; upon seating a rigid body is formed among PRIOR ART automated rivet set tool 2 subsystem, coupler subsystem (comprised of coupler 32), and coupler-mate/shaft/handle subsystem (comprised of coupler mate 42, shaft 4, and handle 64). Those skilled in the art will recognize that shaft 4 is affixed to coupler mate 42, preferably by mating with surface 44 and shoulder 46. This configuration is operative to axially transfer load sources between anvil face 16 and handle (presented later) across seated surface of anvil body 4 first end 6 and bottom of coupling pocket.


Now refer to FIG. 2C, a side view of an assembled BBS 50 is shown. Finally in teaching the coupling assembly of preferred embodiment of this invention, FIG. 2C presents a shaft/handle subsystem 52 comprised of coupler mate 42, tubular shaft 54 having first end 56 and second end 58, handle transition component 60 having stem 62, and handle 64. Shaft 54 first end 56 seats against shoulder 46 of coupler mate 42 and shaft 54 is affixed to surface 44 (also see FIG. 2B). Shaft 54 is similarly affixed to at shaft end 58 to transition component 60 and stem 62 of transition component 62 is affixed to handle 64. Operatively the coupling attachment of the PRIOR ART subsystem previously described in FIG. 1A, the coupler subsystem 32, and shaft/handle subsystem 52 (comprised of coupler mate 42, shaft 54, transition component 60, and handle 64) creates a ridged body among these subsystems. After assembly the slender body BBS 50 has anvil face 16, elongated shaft 54, and handle 64.


Still referring to FIG. 2C, those skilled in the art will recognize that a less preferred alternate embodiment BBS could also be made by extending the length of anvil body 4 and press fitting distal end 62 into handle 64 (not using a coupler system). However, this would make set PRIOR ART rivet set tool 2 (FIG. 1A) unusable for other job functions because it would void the universal attachment feature of anvil body 4 at first end 6 with shoulder 8 of the coupler 32. Set tool 2 is by itself new to the industry but being able to adaptively coaxially join set tool 2 to bucking bar subsystem 52 preserves the universal attachment shape and function of set tool 2 while producing BBS 50 that provides technicians many working benefits. Yet another less preferred embodiment of FIG. 2C is a shaft/handle subsystem 52 where shaft 54, coupler mate 42 and transition component 60 are a singular body.


A carbon fiber shaft 52 is preferred because it is lightweight, rigid or stiff, and has an inherit property of being able to passively damp vibration from pneumatic hammers. In an alternate embodiment, cylinder 54 can be filled with a vibration absorbing material such as foam or rubber to further attenuate system 50 vibration. These vibration damp approaches of subsystem 52 help protect technicians from vibration induced injury.


Further, lightweight shaft 52 (such as a carbon fiber tube shaft) also moves the assembled BBS's 50 center of mass or centroid towards handle 64. Notably, unlike all other bucking bars, this also moves the centroid away from the aircraft surface. The slender body BBS 50 has the advantage of allowing the technician to optionally hold the BBS 50 with the handle 64 near their body's torso, making it more ergonomic for technical posture and reducing technician fatigue. Further still, BBS 50 optionally allows the technician to coaxially align their forearm with shaft 54 to allow bucking bar motion and vibrations to be absorbed by a pivot motion from their shoulder.


Another advantage of BBS 50 is that the slender body system inherently requires a very large angular movement or pivot of handle 64 relative to the rivet surface to change the angle between the anvil face 16 and a rivet shank end face. This is highly beneficial because it helps prevent the technician from installing rivet sets at skew angles; a common type of rivet setting error when using conventional bucking bars because maintaining the proper bucking bar anvil face position when bucking is difficult, and rivets set at a skew angle to the rivet shank axis often require rework.


When using BBS 50, the technician preferably uses two hands. The first hand grasps handle 64 to support the BBS mass and coaxially align the slender body neutral axis of BBS 50 with the rivet shank axis while the second hand supports housing 10 to position anvil face 16 upon a rivet shank end, perhaps while optionally resting the back second hand against aircraft surface. The first hand orbits handle 64 about rivet location (a pivot point) until the described axes are colinear. The technician then applies axial force to handle 64 urging anvil face 16 against face of rivet shank end. When setting the rivet, cylindrical body of plunger 12 encircles the forming rivet prevents anvil face 16 from slipping off the rivet shank end face. This creates a stable and ergonomic work position for the technician.


To further contrast BBS 50 with conventional bucking bar equipment, technicians hold conventional bucking bar (a mass of several pounds) near arm's length to do work which causes fatigue or else they must move their body towards the airframe which produces poor body posture. Also, conventional bucking bars often require rivet gun forces imparted into bucking bars to be absorbed by the technician's fingers and wrists, often resulting in injury known as “white finger.” Further in contrast to conventional bucking bars, the elongated shaft 54 distinguishes itself as a slender body by functionally moving the BBS 50 centroid towards handle 64—though not limiting and for illustration purposes only, to further draw a distinct difference from all PRIOR ART bucking bars—the preferred embodiment BBS 50 forms a slender body that may have a length of about 18-inches.


Those skilled in the art will appreciate other embodiments. For example, without deviating from this invention subassembly 52 can be altered so that coupler mate 42, tubular member 54, and handle transition component 62 can be replaced with a solid shaft while still coupling to set tool 2 with coupler 32. Other embodiments are possible.



FIG. 3 presents a side view of yet another alternate embodiment of BBS having slender body bucking bar 70. Shaft 72 is depicted as a split body or break to further educate that elongated shaft 72 (like tube 54 in FIG. 2C) can be any length. Referring again to FIG. 3, shaft 72 has first end 74 and second end 76. End 76 has a shaft protrusion 78 that operatively affixes shaft 72 to handle 64; handle 64 has a pocket 80 to accept protrusion 78. Distal first end 74 of shaft 72 has an anvil face 16, and optionally has a cavity or anvil face pocket 82. FIG. 3 drawing hidden lines further illustrate pocket 82 and anvil face 16. When in use anvil face 16 abuts the shank end face of a solid core rivet while it undergoes plastic deformation into a button head while shoulder formed by pocket 82 serves to help prevent anvil face 16 from slipping off shank end of rivet while setting a rivet. Those skilled in the art will appreciate that anvil face 16 could be replaced with a concave anvil face surface to back set common head rivets or that pocket 82 could be eliminated without deviation from the invention.



FIG. 4A depicts a coaxial motion Tuned Mass Damp, TMD system 100 preferably coupled to BBS 50 shown in FIG. 2C. The anvil body 4, handle 64, and elongated shaft 54 features are sketched diagrammatically to teach the TMD 100. Damper 100 is equipped with mass 110 coupled to body 4 and handle 64 with at least one of first load source 102 and second load source 104; respectively. Mass 110 further coupled to body 4 and handle 64 with at least one of first damper 106 and second damper 108; respectively. Mass degree-of-freedom is oscillatory motion 112 and motion 112 is preferably coaxial to elongated shaft 54 (in FIG. 2C).



FIG. 4B depicts a pendulum motion Tuned Mass Damp, TMD 120 preferably coupled to BBS 50 shown in FIG. 2C. The elongated shaft 54 and handle 64 features are sketched diagrammatically to teach the TMD 120. TMD 120 is equipped with mass 110 coupled to handle 64 with first load source 102 and first damper 106. Mass degree-of-freedom is oscillatory motion 122 and motion 122 is preferably forms an arc relative to handle 64. Given this teaching, those skilled in the art will recognize the benefit installing two opposing pendulum motion TMDs 120, each located 180-degrees from each other and about the neutral axis of shaft 54 to cancel moment forces applied from TMD 120 motion 122 onto BBS 50.


TMDs depicted in FIGS. 4A and 4B are used to damp system vibrations from any one from the following list of: 1) the impulse force from a rivet gun impact hammer blow, 2) the de-bouncing vibration of the BBS as it tries to come to rest before the next hammer blow, and 3) the natural frequency resonance response of the BBS. The elongated slender body form factor of the BBS enable TMDs to be installed along the shaft or handle which are substantially located a distance away from the rivet being set. This allows more room for the TMDs because there are usually tight space restrictions near the rivet, often because of support structures. Those skilled in the art recognize that the TMDs are used to reduce unwanted vibration and are tuned to match the application.


A person having ordinary skill in the art would understand that the invention has applications in the rivet setting industries and in particular the aerospace assembly industry. This invention could be incorporated into other machines without limitation. Further, provided these teachings many variations of the invention will occur to those skilled in the art. Some variations include different lengths of BBSs, distinguished primarily by length changes to the tubular or shaft members while other variations include form factor changes; however, still other variations are allowed without limit. All such variations are intended to be within the scope and spirit of the invention. Further still, although some embodiments are shown to include certain features, the applicant specifically contemplates that any feature disclosed herein may be used together or in combination with any other feature on any embodiment of the invention. It is also contemplated that any feature may be specifically excluded from any embodiment of the invention.

Claims
  • 1. A bucking bar system is used to set a solid core rivet fastener, said rivet having a manufactured head a shank a shank face and a shank neutral axis where upon fastening, the shank end of said rivet plasticly deforms into a button head to join a plurality of work pieces to each other, said bucking bar system comprising: an elongated shaft, said shaft having a first end and a second end,an anvil face, said anvil face located at said first end of said shaft,a handle, said anvil located at said second end of said shaft,wherein said bucking bar system forms a slender body and said bucking bar system is operative to plastically deform said shank into side button head.
  • 2. The system of claim 1, wherein the form factor of said bucking bar system forms a slender body, said slender body having a slenderness ratio greater than 6.
  • 3. The system of claim 1, wherein the form factor of said bucking bar system forms a slender body, said slender is operative to position the mass centroid of said bucking bar system away from said anvil face and toward said handle,wherein said position of said centroid of said bucking bar system is configured to improve ergonomics.
  • 4. The system of claim 1, wherein the form factor of said bucking bar system forms a slender body, said slender is operative to aid colinear alignment of said bucking bar system with said rivet shank.
  • 5. The system of claim 1, wherein the form factor of said bucking bar system forms a slender body, said slender is operative to aid colinear alignment of said bucking bar system with said rivet shank, andwherein a large angular pivot rotation of said handle over said rivet is required to substantially misalign said anvil face with said rivet shank face.
  • 6. The system of claim 1, wherein the form factor of said bucking bar system substantially coaxially aligns the mass of said bucking bar with said rivet shank, and said coaxial alignment is operative to reduce vibration of said bucking bar system.
  • 7. The system of claim 1, wherein the form factor of said bucking bar system is configured to at least one of, reduce technician fatigue,reduce injury,improve working ergonomics,improve rivet set quality,damp vibration, andavoid rivet set errors.
  • 8. The system of claim 1, where said elongated shaft is comprised of a tubular shaft, wherein said tubular shaft is operative to at least one of, damp vibration, said vibration resulting from rivet gun impact blows, and to position mass centroid proximal to handle.
  • 9. The system of claim 1, where said bucking bar system is further comprised of a PRIOR ART subsystem comprised of at least one of, an automated rivet set tool subsystem, said subsystem having a plunger, said plunger operative to provide a shroud, said shroud operative to prevent said anvil face from slipping off said rivet shank end and said automated rivet set tool subsystem operative to automate the rivet setting process,a back set tool subsystem, said subsystem having a plunger, said plunger operative to provide a shroud, said shroud operative to prevent said anvil face from slipping off said rivet shank end,a shaft/handle subsystem, said subsystem comprised of, a coupler mate component,a shaft component,a handle transition component, anda handle component,a coupler subsystem, said subsystem comprised of, a coupler component,
  • 10. A bucking bar system is used fasten a solid core rivet having a manufactured head a shank and a shank end where upon fastening the shank end plasticly deforms into a button head when joining a plurality of work pieces to each other, said bucking bar system further comprising: an elongated shaft, said shaft having, a first end, said first end having, an anvil face,a second end, said second end having, a handle,
  • 11. The bucking bar system of claim 10 wherein said slender body shape is operative to locate the bucking bar system's mass centroid proximal to said handle and away from said anvil face, tocoaxially align the said rivet shank with said elongated shaft, and torequire a large angular motion of said handle with respect to the neutral axis of said rivet shank, when positioning said bucking bar system over said shank end, to cause coplanar misalignment of said rivet shank end and said anvil face surfaces.
  • 12. A coupler subsystem to form, a bucking bar system by joining a PRIOR ART subsystem to a shaft/handle subsystem wherein said coupler subsystem coaxially joins the ends of two shafts to each other, wherein PRIOR ART subsystem is comprised of: a set tool, said set tool having, a set tool shoulder,a first distal end, said first distal end operative to be the end of a shaft to be said coaxially joined,an anvil face, said anvil face located at a second distal end of said set tool and wherein said shaft/handle subsystem is further comprised of,a shaft, said shaft has a first end and a second end,a handle, said handle is affixed to said first end of said shaft,a pocket, said pocket located proximal to said second end of said shaft,a set of external threads, said external threads located proximal to said second end of said coupler subsystem further comprised of, a coupler, said coupler having,an internal cavity, said internal cavity having, a group of internal threads, anda coupler shoulder,
  • 13. The coupler system of claim 12, wherein upon assembly said PRIOR ART subsystem shaft, said shaft/handle subsystem shaft, are coaxially coupled to each other.
  • 14. The coupler system of claim 12, wherein upon assembly said first shaft, said second shaft, and said coupler form a rigid body with each other.
CROSS-REFERENCE TO RELATED APPLICATIONS

This art may optionally incorporate PRIOR ART most clearly described in U.S. Pat. No. 9,764,376 but is also described preceding U.S. Pat. Nos. 8,316,524; 8,850,677; and 8,978,231 and subsequently international Pats. FR 2,344,234; BR 1,120,150,120,300; CA 2,892,774; and JP 6,177,341. The disclosures of which are incorporated by reference as if fully set forth herein.