GB2199528A - Method of and tool for cutting a collar off a fastener - Google Patents

Method of and tool for cutting a collar off a fastener Download PDF

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Publication number
GB2199528A
GB2199528A GB08725332A GB8725332A GB2199528A GB 2199528 A GB2199528 A GB 2199528A GB 08725332 A GB08725332 A GB 08725332A GB 8725332 A GB8725332 A GB 8725332A GB 2199528 A GB2199528 A GB 2199528A
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United Kingdom
Prior art keywords
collar
blade
dual
ram
housing
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Granted
Application number
GB08725332A
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GB8725332D0 (en
GB2199528B (en
Inventor
John J Kaelin
Gary L Port
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Huck Manufacturing Co
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Huck Manufacturing Co
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Publication of GB8725332D0 publication Critical patent/GB8725332D0/en
Publication of GB2199528A publication Critical patent/GB2199528A/en
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Publication of GB2199528B publication Critical patent/GB2199528B/en
Anticipated expiration legal-status Critical
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23DPLANING; SLOTTING; SHEARING; BROACHING; SAWING; FILING; SCRAPING; LIKE OPERATIONS FOR WORKING METAL BY REMOVING MATERIAL, NOT OTHERWISE PROVIDED FOR
    • B23D29/00Hand-held metal-shearing or metal-cutting devices
    • B23D29/007Hand-held metal-shearing or metal-cutting devices for splitting nuts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00Riveting
    • B21J15/38Accessories for use in connection with riveting, e.g. pliers for upsetting; Hand tools for riveting
    • B21J15/50Removing or cutting devices for rivets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B19/00Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/04Rivets; Spigots or the like fastened by riveting
    • F16B19/05Bolts fastening by swaged-on collars

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Shearing Machines (AREA)
  • Percussive Tools And Related Accessories (AREA)

Description

Cl 1 0 219952o A HYDRAULICALLY ACTUATED LOCKBOLT COLLAR CUTTER AND METHOD
OF CUTTING A COLLAR
BACKGROUND AND SUMMARY OF THE INVENTION
The present invention relates generally to an automatically actuated device for removing a swaged metal collar or nut like member from a two piece lockbolt type fastener. Lockbolt type fasteners have been in use for many years. A typical example is shown in U.S. Patent No. 4,342,529 to J. Ruhl and R. Dixon, which is incorporated herein by reference. Additional examples of such fasteners, which may also be referred to as two p-Jece swage type fasteners include those shown in U.S. Patent No. 3, 915,053 to J. Ruhl and U.S. Patent No. 2,531,048 to L. Huck. In each case the fastener comprises a pin and a generally annular collar adapted to be swaged into annular, non-helical lockgrooves in the pin. Because the collar is generally annular and the lockgrooves non-helical it is not possible to torque the collar off the -ener pin when one wishes-to disassemble the joint secured by fast the fastener, as one can do with a helically threaded bolt and nut combination type fastener. Instead conventional practice has usually been to cut off the collar with a single bladed cutting chisel impacted either by a pneumatically actuated hammer or a hand held hammer. Such means are often unsatisfactory because of the time or energy required to complete the job. Further, in many instances there is not sufficient access to the fastened joint to permit such methods. An additional hardship is encountered-with such techniques when the collar includes a prominent flange at the base of the fastened joint since chisel blade tends to ride over the flange. Even further, one cut through the collar rarely spreads the collar sufficiently to allow the pin lock.grooves to completely disengage the interfitting swaged collar portions whereby the pin can be slipped out of engagement with the collar.
Another past practice includes cutting the collar Orf with a torch. Yet another technique, limited to non-flanged collars has been a hydraulically actuated collar cutter including two diametrically opposed, single edged cutting blades wherein one blade is hydraulically forced downwardly and forwardly through the collar along an axis inclined relative to the workpiece members claimped by the fastener. One of the principal difficulties with this latter system is that the cutting blade may dig into the workpiece. member as it cuts the collar.
It is a general object of the present invention to provide an improved device for disassembling swage type fasteners.
It is another object of the present invention to provide an improved collar cutter including one or more of the features noted above and those as shown and described.
According to one aspect of this invention there is provided an actuable tool f or re=ving a swaged collar from a pin ffr of a lockbolt type fastener, the collar and pin rTr serving as a two piece lockbolt type fastener, said actable tool corrprising:
a housing having a collar receiving opening therein having opposite walls, a piston slidably mounted in said housing, power means operatively connected to said housing for moving said piston, a ram secured to the forward face of said piston to be positioned thereby at one of said opposite walls, and dual cutter blade means tranversely spaced and longitudinally extending with respect to said opening and fixedly secured in said housing oppositely disposed from said ram and adjacent the other of said opposite walls, said spaced cutter blade means and said ram being arranged to receiv-- a swaged collar of a lackbolt tyT,>-- connector therebetween prior to actuation of said piston and further adapted to be engageable..7iith the swaged collar upon actuation of said piston, said ram being arranged to force said swaged collar with respect to said blade means to cause said blade means to cut through and spread said collar upon movement of said ram to thereby separate said collar from the pin member.
P.
i i According to another aspect of this invention there is provided a method for removing a swaged collar from a pin wr of a lockbolt type fastener wherein the collar and pin nr serve as a two piece lockbolt type fastener, said method con-prising the steps of:
a providing an actuable tool having a housing with a collar access opening therein; fixing dual blade means transversely spaced and longitudinally extending with respect to the access or pening; c.
providing a slidable piston in said housing with a ran on the forward face of said piston oppositely disposed from the dual blade means; d. mounting the housing to dispose a collar of a lockbolt fastener in the access opening to be engageable by the dual blade means and the ram; 1 forcing said ram against the collar to cause it to move into engagement with the dual spaced blade means to thereby cause said dual blade means to cut through the wall of and spread said collar to separate it into major and minor parts for removal from the pin member of the lockbolt type fastener.
The present invention includes, but is not limited to, the following features:
1. Lightweight, hand-held and compact.
2. Automatically actuated by the same hydraulic power supply used by the automatic tools designed for installing such fasteners.
3. Cuts the collar cleanly in one operation.
4.
Spreads the collar substantially out of engagement with the lockgrooves, to permit strippin_2 of the pin from the collar.
5. Generally eliminates the need to perform any operations on the pin or collar subsequent to the cuttinE operation prior to disengaging the two fastener members.
Allows disassembly of pin and collar without destroying in any way the fastener hole in the members joined together by the fastener.
Removes lockbolts which have been incorrectly installed, e.g. where the pintail does not break away.
Additional advantages and features of the present invention will become apparent from the subsequent description and the appended claims taken in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a partially sectioned view of a fastener in accordance with the present invention shown in operative relation to a pair of workpieces and having an installation tool in initial engagement with the fastener.
Figure 2 is similar to Figure 1 but illustrating the final step in the installation sequence showing the collar completely swaged onto the pin, pin break and the tool being backed off the collar.
Figure 3 is an end view of the present invention.
Figure 4 is a bottom view of the present invention.
Figure 5 is a cross-sectioned side view taken along the lines 5-5 of Figure 3.
Figure 6 is a cross-sectioned side view taken along lines 6-6 of Figure 3.
Lf- 1 Figure 7 is an.expanded side view of the fastener shown in Figures 1 and 2 after it has been severed by the collar cutter cons-tituting the present invention.
Figure 8 is an expanded end view of the fastener shown in Figures 1 and 2 after it has been severed by the collar cutter constituting the present invention.
Figure 9 is a bottom view of the present invention, similar to Figure 4, but showing the split collar in the collar receiving chamber at the end of the collar cutting sequence and without the pin.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring now to the drawings and in particular to Figures 1 and 2 thereof, there is illustrated a fastener indicated generally at 10 comprising a pin member 12 having a head 14 provided on one end thereof and an elongated shank portion 16.
N Shank portion 16 has a plurality of substantially identical annular combination locking and breakneck grooves 18 extending along substantially the entire length thereof and may include a relatively short smooth cylindrical portion 19 immediately adjacent the juncture with head 14. While smooth cylindrical portion 19 is illustrated as being relatively short, it may extend ^ equal to a predetermined minimum total material up to a length thickness with which fastener 10 is to be used. Thus, grooves 18 will extend along the length of shank 16 from a point greater than this predetermined minimum thickness.
Fastener 10 is designed to be inserted in aligned openings 34 and 36 provided in a pair of members 38 and 40, x7espectively, which are to be joined by fastener 10. A tubular member 42 in the form of a.generally cylindrically shaped collar is placed on shank portion 16 with flanged end portion 44 thereof being brought into engagement with member 40. As shown, shank portion 16 is of a length substantially greater than the total thickness of members -F and Cl. plus the axdal length of collar 42 thereby providing an end portion 6, also having combination grooves 18 which grooves may be engaged by jaws 48 of pulling tool 50.
Pulling tool 50 is of conventional construction having a swaging anvil 52 extending outwardly from the nose portion 54 of the tool 50; the jaws 48 are adapted to be moved rearwardly relative to anvil 52 as shown in the drawings. Anvil 52 of pulling tool 50 has a central frusto conically shaped opening 58 provided therein having a first relatively sharply tapered inner portion 60 and second tapered inner portion 62.
Actuation of pulling tool 50 will cause jaws 48 to engage and grip a predetermined number of combination grooves 18 and thereby exert a pulling or tensioning force upon pin 12 and against collar 42. During the initial stages of the pulling action, anvil 52 exerts an oppositely directed force on collar 42 thereby causing members 38 and 40 to be drawn into mutual engagement.
Thereafter, portion 60 of anvil 52 begins to deform or cause the outer end portion 56 of collar 42 to be extruded into a preselected one 18a of combination grooves 18. This initial deformation causes a locking action to occur between collar 42 and pin 12. Thereafter, continued movement of jaws 48 cause anvil 52 -erial to to move along collar 42 thereby causing the collar mat flow into combination grooves 18c, d, e, and possibly others approaching members 38 and 40 as well as continuing to compress the collar material which has been swaged into groove 18a.
Because of the defined groove configuration which is not part of the present invention, the continued compression and flow of the collar material into groove 18a causes an axially directed localized force to be exerted on sidewall 20 as a portion of the G 2 P.
1 collar material experiences a backward extrusion or flowing to the right as seen in the drawings into the next outwardly disposed groove 18f. The axial component of swaging or material flow force developed by this continued compression and I'low of the collar material incorbination with the axial tension exerted by-the pulling action of the jaws 48 will cause groove 18a to function as a breakneck with end portion 46 of pin 12 breaking thereat. It will also be noted that this swaging sequence results in a secondary flange portion 45 immediately adjacent flange 44 conforming to the shape of anvil 52 and of greater diameter than the remainder of barrel portion 57.
In other fastener constructions, the breakneck may be at a specific point along the pin and may extend well beyond the collar. In any event, the fastener is one in which the collar is swaged in.to non-helical, annular grooves and is not capable of being removed except by destruction, namely cutting or use of a" torch.
The present invention, referring now to Figures 3-6 and 9, constitutes a generally cylindrical, hydraulically actuated tool 70.
Vertically Oriented hydraulic lines 72, 74 provide the means for actuating the tool. If desired such lines can be horizontally disposed at inlets 76, 78, respectively, shown as being plugged. Thus fluid will be supplied to the end of the piston 80 during the power stroke either through passageway 82 or 84 and will be returned to a suitable reservoir during the return stroke through passageway 86 only or passageways 86 and 88, collectively, respectively. Tool housing 90 is a single casting of relatively high strength steel. It will be noted that the outer dimensions of housing 90 are maintained at the minimum required to handle the hydraulic operating pressures and collar cutting forces so that the tool will be of least weight and maximum compactness for lockbolt and collar sizes it is adapted to handle. This includes 7 a barrel portion 92, power supply portion 94, nose or front end 1 11 - e PO tio 9 and base portion 98 common to both the barre', and nos portions.
containing an 0-ring -1 y Barrel portion 92 incluces an inner bore 1100 of relative. constant diameter throughout its length terminating at a pair of abutment shoulders 102 constituting part of the nose portion. Extending radially into the bore 100 around its entire circumference is sealing flange 104 having groove 106 throughout, of general cross-sectional shape as seen in Figure 5, for type seal 108. Piston 80 travels within the bore and includes at one en' a sealing flange 110 extending outwardly therefrom having a groove 112 and 0-ring type seal 114 therewithin, similar to that at the forward end of the bore 100. The bore 100 is sealed by an end cap 116 having an D-ring type seal 118 at its forward end within groove 118. Seals 114 and 117 preclude hydraulic fluid bypass during the power stroke of the piston, whereas seals 108 and 114 preclude such bypass during the piston return stroke, as explained in more detail below. Attached to the piston by a screw 119 at its lowermost forward end is a ram 120 which extends the full width of collar access opening 142 and is contained by the sidewalls 122 of the collar access opening such that it provides a means for precluding rotation of the ram and thus the piston. Groove 124 extends the full width of Aam 120 and provides a retaining edge 126 at the bottom of the ram. The height of the retaining edge 126 from the lower planar surface of base portion 98 (and member 40) is such that the retaining edge will just clear the collar flange 44 as best seen in Figure 6. Finishing with the end cap 116 it will be noted that the cap is threaded at 128 into the barrel portion and diametrically opposed recesses are provided for installing or removing the end cap with a typical spanner wrench.
A primary feature of the present invention resides in the design of the nose portion 96 and the manner in which the dual edged cutter blades 180 cut and simultaneously spread the collar m off the pin. Nose portion 96 includes an access chamber 140 for receiving the fastener. At the base portion 96 the access chamber is defined by the rectangular shaped collar access opening 142 defined by side shoulders 122, front wall 144 against which cutters 180 rest and rear wall 146.
At the top of nose portion 96 the access chamber functions as a pin access opening and is defined by a generally oval opening 148 of considerably less width, bounded on the sides thereof by. abutment shoulders 102, at the front by wall 150 and at the rear by wall 152. The bottom access opening is thus sized to fit the preselected size range of collars to be cut and the uppermost access opening is sized for the corresponding pin size or pin diameter range..
Each abutment shoulder 102 terminates at lower wall 103 which defines the height of the collar access opening 150. The collar access opening may also be referred to as a collar receiving chamber whereas the remainder of access opening 140 may be referred to as a exposed pintail receiving chamber. While the fastener 10 shown at Figure 6 is one in which the pintail is designed to break off within or slightly outside the collar 42, there are instances in which the pintail may fail to break off. If the collar is nonetheless swaged, or at least partly so, it will have to be cut off-and a new fastener installed. The exposed pintail receiving chamber allows one to slip the tool 70 over the unbroken pintail. The top of the ram 120 resides just below lower wall 103 such that there is no interference during the piston power stroke.
Further, front wall 144 includes a recessed portion 145 stepped back a distance generally equal to the thickness of the barrel 57 of any collar to be cut. The base portion 98 is relieved at both sides and the front to provide passages 162, 162 and 160 extending through to the collar receiving chamber 150. The side passages 162 are provided primarily as a means of allowing the collar flange 44 to spread as the cutters 180 move through it, as best seen in Figure 9. However, both side passages 162 also serve as knockout passages, as explained below. The side passages eac -Jncljte walls 161 and 166 d,Jvergiinz outward1v ing cham 2ar recz-iv. assage 160, wr,jc'r towards the cc e-. Fro!t p serves-solely as a knockout passage, is in width slightly greater than the distance separating cutters 180. It will be noted that front wall 144 is recessed transversely of the front knockout passage 160, thereby defining a U-shaped slot 143 within which cutter blades 180 may be received and firmly restrained in all directions other than in the direction of the piston 80. The depth of each knockout opening is slightly greater than the ram retaining edge 126 is high so that, while the retaining edge will engage and embed secondary flange portion 45 of the collar during the piston power stroke, the front wall will have maximum engagement with only the barrel portion of the collar and the collar barrel portion may be spread the entire width of the collar receiving chamber.
The only remaining structural detail to be described is the pair of dual edged cutter blades 180. From Figures 4-6 and 9 it will be noted one blade is the mirror image of the other. Each is held to the housing by suitable means such as a screw 182 and each is received within a generally U-shaped pocket 143 within the nose portion 96 as earlier described. Each includes a lower collar flange cutting edge 186 and an upper collar barrel cutting edge 188. Each lower cutting edge is defined by outwardly diverging side walls 190 and 192, while each upper cutting edge is defined by outwardly diverging side walls 190 and 194. Side wall 190, common to both upper and lower cutting edges 188 and 186 is plane and as installed the walls 190 of each cutter blade are parallel and spaced a distance equal to or slightly greater than the maximum pintail diameter of the smallest or least diameter pin within the preselected range of pin sizes for the tool. Walls 192 and 194 are also straight, however alternatively, each may be curved so as to be concave thereby providing a thinner knife point /0 1 POOR. GUALITY, but an equal degree of spread t 1 o the collar preferably curved on a slightly larger radius.
As seen best in Fizures 5 and 6, each upper cutting edwe 188 is inclined 1frorn the base. thereof in a direction toward the front or nose portion such that the cutting edge will first embed the collar barrel portion at the secondary flange portion 45, thereby creating a reaction force that tends to press the tool down onto the collar.
Further it is preferred that each cutting edge include a slight relief r to increase the strength of the cutting edge and provide additional assurance that the blades will pass over the pintail and cut only the collar.
Cutters 180 and ram 120 are made of the usual hardened or higher carbon content steel, or carbide, to provide long life and cutting cycles against the softer steel collars.
In operation, the tool is powered by the same hydraulic fluid power supply as used fo-r the installation tools used for swaged type fasteners, reference being made to U.S. Patent No. 4,587,829 to B. Sukarevsky. A suitable power source is one such as shown in U.S. Patent No. 3,001,548 to VanH ecke. For a 5/8 inch nominal size pin the power stroke may require 5700 psi and the return stroke about 2400 psi. Given a piston of approximately 2 3/8 inch maximum diameter this will give a force of about 25,250 lbs to cut and spread the collar.
Upon-actuation of an air or electric switch, fluid on the power stroke enters passageway 82 through inlet 72, forcing the piston toward the nose portion 96 until one seal flange 104 engages the other 110 which stops the forward travel. Forward piston travel causes ram 120 to engage the collar. As forward motion continues the collar will become wedged between the ram 120 and the upper cutting edges of blades 180. Further travel will simultaneously cause ram retaining edge 126 to embed itself into the secondary flange 45 of the collar while blade cutting edges 186,188 begin near simultaneously cutting into the flange and barrel portions of the collar. As piston travel continues the collar is spread by the diverging cutt-ing walls 190, 19,/"194 of the blades until piston travel ceases. At this point as shown in Figure 9 a minor collar portion 42a, will be nested between cutter blade walls 190 and the major collar portion 42b will be completely spread out of engagement with the lock grooves of pin 12. To further aid in understanding the cutting and spreading action of the tool, the cut surfaces of the collar which are spread by the upper and lower cutting edges of each blade are shown at 51 and 52, respectively, of Figures 7 and 8..
Upon completing the power stroke, the return stroke is actuated by release of the trigger and pressurized hydraulic fluid is supplied through inlet 74 and passage 86 to the chamber on the return side of piston 80. Given seal flange 110, the fluid force differential will cause the piston to return to its initial position shown in Figures 5 and 6 as the fluid on the power stroke side of the piston exist through passage 82.
At this point, the pin will be free from the collar and the tool can be removed from the now disassembled fastener and joint. Should any portion 42a or 42b of the collar remain wedged in the tool these pieces can be knocked out by inserting a screwdriver or the like through passages 160, or 162 and tapping it out.
1 - V 1 1 f-1 While a specific tool structure has been described and illustrated above, it will be appreciated that the method used to cut and strip the flanged collar froir the.pin may be embodied in other devices. The method is generally that of:
Engaging said collar on diametrically opposed sides, Causing a pair of cutting edges to simultaneously begin cutting through the_flange and barrel portion of said collar and along the entire vertical extent or length of such collar, 3. Such side of blades parallel to the pin being spaced parallel from one another the diameter of the pin around which the collar is swaged, 4. The cutting edges causing the collar, both barrel and flange, to be spread off the pin progressively as the cutting sequence eontinues, and finally, The collar being divided into segments, a major segment and a minor segment, by the cutting edges as the collar is completely severed, with the minor segment being disposed between the cutting edges and of a width equal to that of the pin and the ends of the major portion being spread to such an extend that only the locking grooves at the side of the collar opposite the cutting edges continue to be engaged by the collar, and 6. Removing the collar completely from the pin.
While it will be apparent that the preferred embodiment of the invention disclosed is well calculated to provide the advantages and features above stated, it will be appreciated that the invention is susceptible to modification, variation and change without departing from the proper scope or fair meaning of the 1? subjoined claims.
1 / 1

Claims (15)

CLAIMS:
1. A n actuable tool for removing a swaged collar from a pin member of a lockbolt type fastener, the collar and pin member serving as a two piece lockbolt type fastener, said actuable tool comprising:
a housing having a collar receiving opening therein having opposite walls, a piston slidably Mounted in said housing, power means operatively connected to said housing for moving said piston, a ram secured to the forward face of said piston to be positioned thereby at one of said opposite walls, and dual cutter blade means tranversely spaced and longitudinally extending with respect to said opening and fixedly secured in said housing oppositely disposed from said ram and adjacent the other of said opposite walls, said spaced cutter blade means and said ram being arranged to receiva a swaged collar of a lac}bolt tyry-- connector therebetween prior to actuation of said piston and further adapted to be engageable;,-i-Lh t-he swaged collar upon actuation of said piston, said ram being arrange tO force said swaged collar with resTpect to said blade means to cause said blade means to out through and spread said collar upon movement of said ram to thereby separate said collar from the pin member.
2. ' '.,-L.he actuable tool of c-lain. 1, wherein said ram includes a retaining edge formed on said ram for engaging one side of said collar to embed said ram therein while said dual cutter blade means simultaneously cuts through the opposite side of said collar.
TIve. actuable tool of claim 1, wherein eac-h of said dual cutter blade means have dual edge cutter blades.
4. The actuable tool of claim 3, wherein said dual edged cutter blades each have upper and lower blades, each of said upper and lower blades having diverging cutting walls for spreading the collar as the blades cut through the wall of the collar.
5. The actuable tool of claim 3, wherein one blade of each of said dual edged cutter blades engage one portion of said collar, the other blade of each of said dual edged cutter blades being inclined in a direction to initially engage the body portion of said collar in the vicinity of said one portion for producing a reaction force to press said housing against said collar.
6. The actuable tool of claim 1, wherein said housing has spaced shoulders thereon with side passages aligned to receive portions of the collar which are spread apart by said blade means.
7. The actuable tool of claim 4, wherein said housing has spaced shoulders thereof with side passages aligned to receive portions of the collar which are spread apart by said dual edged cutter blades.
8 The actuable tool of claim 7, wherein said dual edged cutter blades are spaced to define a knock-out space therebetween, said knock-out space being arranged to receive a cut-away minor portion of the collar said side passages being configured to receive a major collar portion spread apart by said dual edged cutter blades.
9. The actuatable tool of claim 5 being adapted to remove a collar having a flanged lower portion and upper barrel portion of lesser diameter wherein said one blade is said lower blade and said other blade is said upper blade, said upper blade being of greater longitudinal extent at the lowermost portion thereof than is the lower blade, and said lower blade length exceeding the height of the flanged lower portion of the collar whereby upon actuation of the tool the upper c- eu i.
1 blade will make first contact with the barrel portion of the collar.
10. A method for removing a swaged collar from a pin member of a lockbolt type fastener wherein the collar and pin member serve as a two piece lockbolt type fastener, said method comprising the steps of:
providing an actuable tool having a housing with a collar access opening therein; b. fixing dual blade means transversely spaced and longitudinally extending with respect to the access ol.y--ning; c.
1 providing a slidable piston in said housing with a ram on the forward face of said piston oppositely disposed from the dual blade means; mounting the housing to dispose a collar of a lockbolt fastener in the access opening to be engageable by the dual blade means and the ram; e. forcing said ram against the collar to cause it to move into engagement with the dual spaced blade means to thereby cause said dual blade means to cut through 'the wall of and spread said collar to separate it into maJor and minor parts for removal from the pin member of the lockbolt type fastener.
11. The method of claim 10, including spreading the major part of the collar while cutting through the wall thereof to remove the collar from the pin member.
/7
12. The method of claim 10, further including applying a reactive force between the dual blade mans and the follar to force the housing against the collar during the cutting thereof.
13. The method of claim 11, further including separating the minor part of the collar from the major by providing a knock-out space between the dual blade mews.
14. An actuable tool substantially as herein described with reference to and as shown in the accaTpanying drawings.
15. A method for removing a swaged collar from a pin nir of a lockbolt type fastener substantially as herein described with reference to and as shown in the accompanying drawings.
4 / 1 PubLis!7ed 1988 at T,ie Patent Office. State- House. 66'71 High Holborn, LonOm WC1R 4TP Further copies may be obtained from The Patent Office. Sales Branch, St Ma.-y Cray. Orpir-g'c.-. Ken, BF.5 311LI Printed by MWtiplex techniques It& St Mary Crky, Kent Cor. 1/87.
GB8725332A 1986-11-04 1987-10-29 A hydraulically actuated lockbolt collar cutter and method of cutting a collar Expired - Fee Related GB2199528B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US92719586A 1986-11-04 1986-11-04

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GB8725332D0 GB8725332D0 (en) 1987-12-02
GB2199528A true GB2199528A (en) 1988-07-13
GB2199528B GB2199528B (en) 1990-08-29

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GB8725332A Expired - Fee Related GB2199528B (en) 1986-11-04 1987-10-29 A hydraulically actuated lockbolt collar cutter and method of cutting a collar

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AU (1) AU588712B2 (en)
CA (1) CA1292178C (en)
DE (1) DE3737447A1 (en)
FR (1) FR2605919A1 (en)
GB (1) GB2199528B (en)
ZA (1) ZA878251B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2257080A (en) * 1991-06-28 1993-01-06 Hydra Tight Ltd Nut splitter
CN103317183A (en) * 2013-06-19 2013-09-25 常熟市同利电力工具厂 Double-acting hydraulic scissors

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836888A (en) * 1956-11-23 1958-06-03 Lockheed Aircraft Corp Tools for removing the collars of fasteners
FR1234180A (en) * 1959-05-09 1960-10-14 Sud Aviation Rivet ring removal pliers
GB1601772A (en) * 1978-03-21 1981-11-04 Gkn Bolts & Nuts Ltd Device for splitting nuts
GB8503777D0 (en) * 1985-02-14 1985-03-20 Allspeeds Holding Ltd Nut splitter device

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2257080A (en) * 1991-06-28 1993-01-06 Hydra Tight Ltd Nut splitter
GB2257080B (en) * 1991-06-28 1994-11-30 Hydra Tight Ltd Improvements in and relating to nut splitters
US5479710A (en) * 1991-06-28 1996-01-02 Hydra-Tight Limited Nut splitters
CN103317183A (en) * 2013-06-19 2013-09-25 常熟市同利电力工具厂 Double-acting hydraulic scissors
CN103317183B (en) * 2013-06-19 2015-06-17 常熟市同利电力工具厂 Double-acting hydraulic scissors

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Publication number Publication date
ZA878251B (en) 1988-05-02
GB8725332D0 (en) 1987-12-02
DE3737447A1 (en) 1988-06-09
AU8017787A (en) 1988-05-05
GB2199528B (en) 1990-08-29
AU588712B2 (en) 1989-09-21
CA1292178C (en) 1991-11-19
FR2605919A1 (en) 1988-05-06

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