A method of making remateable cracked connecting rods

Abstract: A method of making exactly remateable cracked connecting rods (10) comprised of forged wrought steel possessing typical ductility, said rods (10) having a big end (11) with a big bore (12) therein and an arm-like body (15) extending therefrom with a small end (14) at its extremity, the big end (11) having crack initiating crevices (15) formed therein to promote a cracking plane (16), comprising the following steps: (a) placing the big bore (12) of an uncracked connecting rod (10) onto a nestable separable pair of cantilevered hemispherical blocks (31,32) complementary to the internal shape of the big bore (12); (b) continuously and uniformly separating the cantilevers of said blocks to initially assure contact of said blocks (31,32) with the rod at a tangent point aligned substantially on the longitudinal axis of the uncracked connecting rod, and thereafter to exert sufficient force through said cantilevers to the blocks (31,32) to pull apart the connecting rod at the cracking plane (16) determined by said crack initiating crevices (15), the connecting rod cap (41) and body (42) being free to experience small but independent macro-rotation relative to the connecting rod axis during such cracking separation.

Description: This invention relates to a method of making bipartite connecting rods by cracking, and more particularly doing so with a forged wrought steel connecting rod possessing typical ductility. Connecting rods have been made bipartite for some time by sawing the enlarged end of the connecting rod into two pieces and reassembling the sawed pieces with bolts (see U.S. patents 1,831,325 and 2,371,400). Fracturing is a more attractive alternative because it allows the irregular jagged ridges on the cracked plane to facilitate more exact rematching of the pieces. One of the earliest patented approaches to cracking forged wrought steel rods is disclosed in U.S. patent 2,553,935 (to Parks et al, 1951). The steel used for connecting rod in the 1940's was tough and ductile. To encourage cracking of such wrought steel, the cross-sectional area of the cracking plane was reduced by Parks with saw kerfs and drilled holes. This avoided using heat treatment to make the steel more brittle, which heat treatment would discourage ease of subsequent finish machining and would degrade the toughness of the connecting rod. This also avoided use of other brittlyzing techniques, such as cryogenics, which is exorbitantly expensive. An extension of the Parks idea of reducing the cross-sectional area is also shown in the later U.S. patent 4,693,139, employing dual V-notches to make the initiation of cracks easier. The Parks patent, as well as U.S. patents 4,569,109; 4,768,694; and 4,860,419, have used a mode of cracking that employs a mandrel placed in the big bore of the connecting rod; the mandrel is expanded by forcing a wedge sideways therethrough. Wedge expandable mandrel cracking is disadvantageous because it is difficult to control cracking uniformity and lacks repeatability of quality when processing large volumes of connecting rods. Slight material variations or dimensional discrepancies between rods will require a slightly different wedge or stroke of the wedge to achieve uniformity. Such control of the wedge cannot be easily obtained. Application of a cracking force has been tried in other modes, such as in U.S. patent 3,994,054, wherein conical members were thrust into smaller but separate openings drilled transversely through the cracking plane of the connecting rod. This mode resulted in uncontrolled cracking since the greatest force would occur unevenly on the side of the connecting rod where the conical members first entered the openings. From US-A 4 754 906 representing the closest prior art it is known a method of making remateable cracked connecting rods comprised of forged wrought steel possessing typical ductility, said rods having a big end with a big bore therein and an arm-like body extending therefrom with a small end at its extremity, the big end having crack initiating crevices formed therein to promote a cracking plane, the method comprising the following steps: (a) placing the walls of the big end bore of an uncracked connecting rod onto a nestable pair of cantilevered hemispherical blocks which are complementary to the internal shape of the big bore and (b) continuously and uniformly separating the cantilevers of said blocks to initially assure contact of said blocks at a tangent point aligned substantially on the longitudinal axis of the uncracked connecting rod, and thereafter to exert sufficient force through said cantilevers to the blocks to pull apart the connecting rod at a cracking plane determined by said crack initiating crevices. What is needed is a reliable method of consistently making excellently balanced and smoothly cracked connecting rods with the method operating on a one-piece forged wrought steel connecting rod possessing typical ductility and which method eliminates the need for any brittlyzing techniques. According to the present invention as claimed in claim 1 there are the following features which contribute to the inventive distinction from the closest prior art: (a) the blocks are smaller than the big bore of the connecting rod (b) the contact between the blocks and the big bore is at tangent points aligned with the longitudinal axis of the rod (c) the force applied to the blocks is through the cantilevers (d) the contact between the blocks and the connecting rod allows the parts of the connecting rod to be free for independent macro-rotation. The invention is a low-cost method of making cracked connecting rods comprised of forged wrought steel possessing typical ductility. The process comprises, in its most essential aspects, the following steps: (a) placing the big bore of a connecting rod onto a nestable pair of cantilevered hemispherical blocks complementary to the internal shape of the big bore; (b) continuously and uniformly separating the cantilevers of said blocks to initially assure contact of said blocks at a tangent point aligned substantially on the longitudinal axis of the connecting rod, and thereafter to exert sufficient force through said cantilevers to the blocks to pull apart the connecting rod at a cracking plane determined by crack initiating crevices in the connecting rod, the connecting rod cap and body being free to experience small but independent macro-rotation relative to the connecting rod axis during such cracking separation. To facilitate balanced separating forces within the connecting rod while continuously pulling the cap and body apart, the cracking head apparatus, used to carry out step (b), is: (i) oriented to pull in a generally vertical plane, (ii) the longitudinal axis of the connecting rod is canted (in the range of .05-.15/) to compensate for stretch or deflection of a movable cantilever; (iii) the rod is completely suspended on the cantilevered blocks just prior to initiating cracking; (iv) the relative macro-rotation may preferably be limited by positioning shoulder stops adjacent the cap within a distance of 0.05 to 0.1 cm (.02-.04 inch) and a cradle spaced from the small end of the rod within a distance of 0.05 to 0.1 cm (.02-.04 inch); and (v) one of the blocks is desirably held fixed while the other is moved for separation. A transfer fixture may be used to position the connecting rod onto the cracking head cantilevered blocks, which fixture desirably carries away the split rod pieces in mated position for subsequent operations such as finish machining and reassembly. The transfer fixture advantageously uses resilient snugging contacts which offer little or no resistance to cracking forces. The force used to create tension and resulting fracture in the connecting rod is preferably in the range of 155 687,77 - 200 169,99 N (35,000-45-000 pounds), applied at the rate of about 11,43 cm/s (4.5 inches/second, and is administered preferably by a hydraulic piston and cylinder assembly. The invention will now be described further, with reference to the accompanying drawings in which: Figure 1 is a perspective view of a forged one-piece connecting rod prepared for cracking; Figures 2-13 are sequential operative views of front and side elevations of the apparatus used to carry out the method of this invention; Figure 14 is an elevational view of a torque machine used to bring the cracked cap and body into its fully mated position; Figure 15 is an enlarged view of a circled portion of the rod in Figure 14; Figure 16 is a side of the structure in Figure 15 taken along lines 16-16 showing degree of guiding provided by the bolts; and Figure 17 is a view like that of Figure 16 showing exact realignment after sufficient clamping load is applied. A preferred process mode for carrying out the invention is depicted in a flow diagram attached. The process is designed to make possible the cracking of wrought steel connecting rods, having typical ductility, with clean and level cracking planes that are exactly rematchable. Forging steels used for commercial connecting rods for the past several decades have generally included designations of 1151, 1141, and 1541. These steels are typically characterised as being "ductile". This level of ductility has normally led to stretching or deformation at the cracking plane during cracking unless such ductility characteristic is modified prior thereto by heat treatment or cryogenics as taught by U.S. patent 4,569,109. The one-piece forged wrought steel connecting rod 10 has a big end 11 with a big bore 12 therein and an arm-like body 13 extending therefrom which terminates in a small end 14 at its extremity. The rod 10 is prepared with at least one pair of crack initiating crevices 15 to define a cracking plane 16 through the sides 17, 18 of the big end 11 and across the big bore 12 of the rod. The crevices are sharp V-shaped grooves that are machined (such as by broaching) into the internal surface 19 of the big bore, extending parallel to the axis 20 of the big bore. Sometimes it is desirable to provide an additional pair of external grooves 21 to control the line of cleavage thereat, such grooves also being sharply V-notched and parallel to the big bore axis. Such crevices may be more pronounced or sharp by originally forming them in the blank (to a degree slightly deeper than possible with machining) from which the rod is forged and then, during forging, closing the crevices by folding them over under pressure. In further preparation, the one-piece connecting rod is manually placed onto an upright transfer fixture 22 that has been brought to a station across from a cracking head (see Figures 2 and 3, as phase 1). The transfer fixture serves not only to station the connecting rod in a stationary position in preparation for cracking, but is subsequently used to carry the rod along a carousel to permit other rod operations, including finish machining and reassembly. The transfer fixture has a cradle 24 comprised of biased right and left surfaces 25, 26 to support the small end 14 or bottom of the connecting rod during the preparatory or transfer stages. A resilient stop (crowder) 27 is brought down onto the top of the rod to snug the rod against the cradle 24. A pair of lateral supports 28, 29 are used to resiliently hold the midsection of the connecting rod, support (crowder) 29 being actuatable to resiliently contact the connecting rod to snug it against fixed support 28. As shown in Figures 4 and 5, cracking head 30 is moved laterally up to fixture 22 to allow insertion into the big bore of the connecting rod a pair of nestable, vertically separable hemispherical blocks 31, 32, each of which is cantilevered at 31a, 32a, respectively, by integral attachment to a slide assembly 33 which in turn is actuated by a hydraulic piston and cylinder device 34 acting through connection 35. The hemispherical blocks 31, 32 are nested within the big bore 12 of the rod which in turn is nested within the crowder 27, cradle 24, and lateral supports 28, 29. Rod cap shoulder stops 36, 37 are carried by the cracking head 30, also as cantilevers, and interleave with the fixture nesting elements (crowder 24, supports 28, 29), but in spaced relation to the rod. The machine head 30 has a fixed assembly connected by a cantilever with the lower hemispherical block 32. The vertically movable slide assembly 33 supports the upper cantilevered block 31 for applying tension force to the rod. The blocks, prior to hydraulic separation, are slightly smaller than the internal diameter of the rod bore 12 with a radial spacing on each side of about 0.178 mm (.007 inch). The cracking head initially separates the blocks to pick up such 0.178 mm (.007 inch) slack. After taking up such internal slack, the connecting rod will be raised and removed from any contact with the fixture cradle 24 at its small end 14; the lateral support 29 is resilient and offers little or no restraint against movement due to cracking action since the spring force does not exceed 30 pounds. Similarly, the top snugging crowder 27 offers a resilient force no greater than 33 pounds. The cap shoulder stops 36, 37 on the cracking head 30 are spaced at least 0.05 cms (.02 inch) from any part of the connecting rod. This is considerably greater than any machining tolerance. Thus, the connecting rod will be virtually suspended at tangential contact points 38, 39 of the hemispherical blocks (aligned with the longitudinal axis 40 of the rod) and there is no other restraining or solid contact maintained with the fixture or with the cracking head (see Figures 7 and 8). To commence cracking, the lower block 32 is held stationary while the upper block 31 is moved hydraulically uniformly upwardly and continuously by actuation of the piston and cylinder 34. The cantilevered upper block 31 is moved upwardly at a rate of about 11.25 cms (4.5 inches)/second to apply a pulling force of about 155 687,77 - 200 169,99 N (35,000-45,000 pounds). The slack is taken up in a first phase to suspend the rod on the tangential contact points of the blocks, free of fixture 22. As the pulling force continues, the bore opening will begin to be slightly stretched by such continued force, but only along the longitudinal axis of the rod, causing a somewhat greater surface of the block to engage the internal bore 12 of the rod. A crack is initiated at the crevices 15 and progresses along the crack plane 16 upon sustained tension from the cantilevered blocks because the cap 41 and body portion 42 portions of the rod are permitted freedom for small macro-rotation relative to each other during such cracking. This will promote a fishtailing effect where, upon severance of one side, the cap and body portions will rotate away from each other using the non-severed side as a pivot (see Figures 8 and 9). For example, the fishtailing may be to the left with the small end 14 contacting the left side 26 of the cradle 24 while the right side of the rod is cracked at 43 and the cap 41 rotated to the shoulder stop 37. A space of at least 0.05 cms (preferably 0.1 cms [.02 inch (preferably .02-.04 inch)] is maintained at 44 between the cradle surface 25 and the rod end 14, and of at least 0.05 cms (preferably 0.1 cms [.02 inch (preferably .02-.04 inch)] at 45 between the rod's left shoulder and shoulder stop 36. In the final cracking phase, the body portion 42 of the rod fishtails to the right contacting the right side 25 of the cradle 24, and the left side of the rod is cracked as the cap portion 41 is pulled further upwardly by the cantilevered block 31 and pivots about the stop 37. In one of the last phases, the loose body portion 42 of the connecting rod falls down into the cradle 24 (see Figures 13 and 14) and, subsequently, the cap portion 41 is lowered to rest on the cracked surface of the rod body portion 42 while the cracking head 30 is withdrawn from the connecting rod big bore. Due to the large tension force (energy) that must be applied gradually and uniformly 177 928,88 N (40,000 pounds) at a movement rate of about 11.25 cms/second (4.5 inches/second) to effect clean cracking, the movable cantilever may stretch or bend a micro-amount, angularly opposite to the direction of pulling. This may result in non-flat cracking or inability of the crack to follow the intended crack plane smoothly. This is overcome by canting of the cantilever of the movable block 31 a micro-degree in the direction of pulling (or away from the anticipated deflection of the cantilever during separation). Such canting may be in the range of .05-.15/ for 1080 steel, but will depend on the nature of the material. As shown in Figures 14 and 15, the split and separated rod pieces are carried by the fixture 22 (preferably along a carousel) to a remating station. Rotary drivers 50 and 51 are used to torque tie bolts 52 and 53 into threaded seats 54, 55, respectively, in the body portion 42. The unthreaded shank 56 of each bolt has an intended clearance 57 with its cylindrical opening 58 in the cap portion 41 of about 0.675 cms (range of 0.375 to 0.75 cms) [.27 inch (range of .15-.30 inch)]. As the torquing force increases, the bolt heads 59 force the rod cap portion 41 and its cracked surfaces into substantial remating relationship with the ridges 60 within micro-close, but not exact, seating in their corresponding valleys 65 of the cracked surface of the body portion 42. As the cracked surfaces are brought more tightly together, the cap and body portions are free to reshuffle laterally (held only by light spring tension of crowder 27 and support 29) and thus the corresponding ridges of opposite surfaces act as conical guiding surfaces for achieving a more exact rematch. When the torquing force is finally increased to its final level (preferably to within 20% of the yield point of the bolt shank material), any dislocation needed to achieve exact rematch is assured by yielding of the ridges. Block diagram of a preferred process mode of this invention;

Claims: A method of making remateable cracked connecting rods (10) comprised of forged wrought steel possessing typical ductility, said rods having a big end (11) with a big bore (12) therein and an arm-like body (13) extending therefrom with a small end (14) at its extremity, the big end (11) having crack initiating crevices (15) formed therein to promote a cracking plane (16), the method comprising the following steps: (a) placing the walls of the big end bore (12) of an uncracked connecting rod (10) onto a nestable pair of cantilevered hemispherical blocks (31,32) which are complementary to the internal shape of the big bore (12) and which are smaller than the big bore (12); (b) continuously and uniformly separating the cantilevers of said blocks (31,32) to initially assure contact of said blocks (31,32) at a tangent point aligned substantially on the longitudinal axis of the uncracked connecting rod, and thereafter to exert sufficient force through said cantilevers to the blocks (31,32) to pull apart the connecting rod at a cracking plane (16) determined by said crack initiating crevices (15), the contact between the blocks (31,32) and the connecting rod being such that the connecting rod cap (41) and body (42) are free to experience small but independent macro-rotation relative to the connecting rod axis during such cracking separation. A method as claimed in claim 1, in which the step of separating the cantilevers of the blocks (31,32) is carried out in any plane. A method as claimed in claim 1, in which the step of separating the cantilevers of the blocks (31,32) is effected by maintaining one of said blocks stationary and moving the other block. A method as claimed in claim 3, in which the step of separating the cantilevers of the blocks (31,32) is carried out by initially canting the cantilever of the movable block away from any anticipated deflection of the cantilever during the step of separation. A method as claimed in claim 4, in which the step of separating the cantilevers is carried out by initially canting the cantilever of the movable block away from the axis of the big bore by an angle in the range of 0.05 to 0.15° in the direction of pulling. A method as claimed in claim 1, in which the step of separating the cantilevers of the blocks (31,32) includes suspending the uncracked connecting rod (10) solely by said blocks (31,32) just prior to initiating cracking of the connecting rod. A method as claimed in claim 1, in which during the step of separating the cantilevers, the said freedom for macro-rotation during cracking separation is limited by stops coupled to the cantilevered block associated with and in contact with such cracked piece of rod. A method as claimed in claim 7, in which during the step of separating the cantilevers, the said freedom for macro-rotation during cracking separation is limited by stops spaced from the rod piece a distance in the range of 0.05 to 0.1 cms (0.02 to 0.04 inches) prior to initiating cracking. A method as claimed in claim 8, in which during the step of separating the cantilevers, the said freedom for macro-rotation during cracking separation is limited by stops which include a pair of stops associated with the cap of the said rod (10) to act as shoulders, and a pair of stops oriented as cradling surfaces to limit macro-rotation of the small end of the rod (10). A method as claimed in claim 1, in which the step of continuous and uniform separation of the cantilevers of the blocks (31,32) includes applying a force through the cantilevers of about 177 928,88 N (40,000 pounds) at a movement rate of about 11.25cms (4.5 inches) per second. A method as claimed in claim 1, applied to making a remateable cracked connecting rod from a one piece rod in which the said crack initiating crevices have been preformed in an unforged metal blank and closed by folding during forging of the blank. A method as claimed in claim 1, in which the step of continuous and uniform separation of the cantilevers of the blocks (31,32) is effected by hydraulic means. A method as claimed in claim 12, in which the said hydraulic means is effective to move said blocks (31,32) apart at a rate of about 11.25 cms (4.5 inches) per second. A method as claimed in claim 1, in which during the step of separating the cantilevers, only the cantilevered blocks (31,32) are in a linear path and said cap (41) and body (42) receive longitudinally balanced tension forces. A method of making a bipartite connecting rod (10) of forgeable ductile steel, said rod having a big bore (12), the method comprising the steps of: (a) preparing a forged steel one-piece connecting rod (10) with at least one pair of spaced stress riser grooves (15,21) to define a common cracking plane (16) extending through each side of said rod (10) and bisecting said big bore (12); (b) continuously pulling apart said prepared rod (10) by use of relatively separable cantilevered pull blocks (31,32) extending into said big bore (12) and having surfaces generally complementary to but smaller than the internal surface of said big bore, said blocks (31,32) being effective to initially contact the internal surface of said big bore (12) at a pair of tangent points lying on the longitudinal axis (40) of said rod, the contact between the blocks (31,32) and the connecting rod (10) being such that separated pieces (41,42) of said rod are free to experience small but independent macro-rotation during such unlimited continuous separation except as inhibited by frictional contact with said blocks (31,32); and (c) remating said pieces (41,42) by using bolts (52,53) extending therebetween and threaded into one of said pieces (42), said pieces (41,42) being free to adjust laterally of the axis (40) of the rod during such remating except as limited by the clearance (57) of the threaded bolts (52,53) within their unthreaded openings (58), said bolts (52,53) being torqued sufficiently to exert a clamping force on the ridges (61) of said cracked plane reshuffling them into substantial rematch and thereafter adjusting such ridges (61) to promote exact remating. A method as claimed in claim 15, in which the step of remating said pieces (41,42) is performed with bolts (52,53) in which the clearance between the bolt shank (56) of each bolt (52,53) and the bolt openings (58) is in the range of 0.375 to 0.75 cms (0.15 to 0.30 inch) so as to locate the mating cracked pieces (41,42) in a first proximity where the irregular ridges (61) guide the cracked surfaces into substantial rematch. A method as claimed in claim 15, in which during the step of remating said pieces, the said clamping force is exerted to within 20% of the yield point of the bolt shank (56) of each bolt (52,53). A method as claimed in claim 15, which is applied to making a connecting rod in which the stress riser grooves (15) are on the internal surface of the big bore (12). A method as claimed in claim 15, applied to making a connecting rod having two pairs of stress riser grooves (15,21), one pair of the grooves (15) being on the internal surface of the big bore (12) and the other pair of grooves (21) being on the outer surface of the big bore (12).

Inventors: HOAG PETER Y, KYTE RALPH L, STUECK JOEL P, HOAG, PETER Y., KYTE, RALPH L., STUECK, JOEL P.
Applicants: FORD FRANCE, FORD MOTOR CO, FORD WERKE AG, FORD FRANCE S. A., FORD MOTOR COMPANY LIMITED, FORD-WERKE AKTIENGESELLSCHAFT
Application year: 1992
Main classification: B23D31
IPC codes: F16C33, B23D31, F16C9