CA1256265A - Process for manufacturing siamese-type cylinder block - Google Patents

Abstract

ABSTRACT OF THE DISCLOSURE
A process for manufacturing a siamese-type cylinder block which is disclosed herein comprises a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is cast in each cylinder barrel of a siamese-type cylinder barrel made of an aluminum alloy and consisting of a plurality of cylinder barrels connected in series, and a mechanically working or machining step of forming the inner peripheral surface of each sleeve of the cylinder block blank into a true circle. The process is characterized in that the blank making step includes placing highly rigid sleeves each having a thickness set as large as 10% or more of the inner diameter thereof into a siamese-type cylinder barrel molding cavity in a mold and then pouring a molten metal of aluminum alloy under a pressure into the cavity to effect a casting. The sleeve is cast-in as it is at an ambient temperature or in a heated state. A
cylinder block blank resulting from the casting-in of sleeves at an ambient temperature is subjected to a thermal tratment for reducing the casting strain in each cylinder barrel.

Description

~256~65 The present invention relates to a process for manu~ac-turing a siamese-type cylinder block and more particularly, to such a process comprising a blank making st.ep of providing a cylinder block blank in which a sleeve made of a cast iron is incorporated in each cylinder barrel of a siamese-type cylinder barrel made of an aluminum alloy and consisting of a plurality of cylinder barrels connected in ser~es, and a mechanical working or machining step of ~orming the inner peripheral surface of each sleeve of the resulting cylinder block blank into a true circle.
Such conventional blank making steps include placing sleeves in a siamese-type cylinder barrel molding cavity in a mold and then, pouring a molten metal of aluminum alloy under pressure into the cavity for casting. Thereby, a casting strain is produced in the cylinder barrels in the blank due to the cast-ing pressure and the action of rapid solidification of the alu-minum alloy. With a sleeve having a smaller thickness and a lower rigidity, such a casting strain influences the sleeve to produce a strain therein. To avoid this, the thickness of the sleeve may be increased, but with a too large thizkness, the amount of sleeve to be cut is increased in subsequent working into a true circle, which is uneconomical and causes an increase in working time. Even if the thickness of the sleeve is increased, there are the following problems which arise with a cylinder block resulting from the immediately working of the inner peripheral surface of the sleeve into a true circle after the casting of the blank. In the operation of an engine assem-bled using such cylinder block, the casting strain in the cylin-der barrel influences the sleeve ~hen the cylinder barrel heated during the operation has been returned to an ambient temperature after the stoppage of operation of the engine, thereby causing the amount of permanent deformation of the inner diameter of the sleeve to increase. ThuS, a clearance is produced between a pis-ton ring and the sleeve resulting in an increased amount of blow-by gas and a useless consumption of oil.

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When the sleeve has increased thickness at an ambient temperature, the heat of mol-ten metal is absorbed by the sleeve so that the molten metal close to the sleeve is solidified ear-lier than the molten metal close to a breakable core for forming a water jacket. Consequently, the metal structure in the cylin-der barrel is different from that at the portion close to the core. In this case, both the metal structures around the sleeves vary in thickness in the radial direction of the sleeve, and because the region between the adjacent sleeves is not occupied by the core, the metal structure between the ad~acent sleeves is different from both the above metal structures. In addition to the problem in metal structure, be~ause the shrinkage o~ the sleeve heated by the molten metal does not follow the solidifica-tion shrinkage of the molten metal, the casting stress remaining the sleeve is non-uniform around the circumference of the sleeve.
The absorption of the heat of the molten metal by the sleeve causes the early solidification of the molten metal to degrade the close adhesion between the sleeve and the molten metal, thereby producing a very small clearance between the sleeve and the cylinder barrel resulting in a poor release of heat from the sleeve.

Thus, if the casting stress remaininy in the sleeve is non-uniform around the circumference of the sleeve and the release of heat from the sleeve is poor, in the operation of an engine assembled using a cylinder block obtained through the working of the inner peripheral surface of such sleeve into a true circle, the amount of sleeve thermally expanded is non-uni-form around the circumference of the sleeve, causing a clearanceto be produced between a piston ring and the sleeve, resulting in the same problems as described above.

In providing a blank as described above and including a water ~acket to which the entire periphery of a siamese-type cylinder barrel faces, operations which have been adopted include ,~ ~

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placing sleeves and a water-~acket shaplng breakable core sur-rounding the sleeves into a siamese-type cylinder barrel molding cavity in a mold and then, pouring a molten metal of aluminum alloy into the cavity to cast a blank, removing unnecessary por-tions such as gates and runners from the blank and then, breakingthe breakable core to remove about half thereof by applylng vibration to the blank, and heating the blank for a period of about 4 hours at a temperature of 350C or more to burn a binder contained in the core and enhance the breakabillty of the remain-der of the core. In the above heating step, the heating causesthe hardness of the aluminum alloy portion in the blank to be considerably reduced and make it impossible for a cylinder head-bound surface, a crank ~ournal bearing holder, an oil pan-bound surface of a crankcase or the like to retain a satisfactory hard-ness. Therefore, the heating step has been ~ollowed by an opera-tion comprising subjecting the blank to a T6 treatment, namely to a thermal treatment of heating the blank for a period of about 2 hours at a temperature of about 500C and then cooling it with water to provide the recovery of the hardness, breaking the remainder of the core to remove it from the blank by applying vibration to the blank, subjecting the blank to cleaning and checking the resulting blank.

However, the abov~ conventional process is accompanied by a problem that even if the T6 treatment enables the hardness of the aluminum alloy portion in the blank to be improved, a non-uniform stress remains in the sleeve at the coollng step in the above treatment and thus, a high performance cylinder block can-not be obtained.

The conventional process also has the disadvantage of uneconomically increasing the amount of energy consumed due to two heating steps included therein.

The present invention provides a process for manufac-turing a siamese-type cylinder block wherein using a highly rigid J

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The present invention also provides a process for manu-; facturing a siamese-type cylinder barrel wherein using a highly rigid sleeve having a specific thickness, a siamese-type cylinder block can be produced with a reduced influence of the casting strain in a cylinder barrel on thl3 sleeve and wi-th the casting strain in the cylinder barrel being diminished by a thermal treatment, thereby to substantially reduce the amount of perma-nent deformation of each sleeve in its inner diameter.

Further, the present invention provides a process for manufacturing a siamese-type cylinder block wherein using a highly rigid sleeve having a specific thickness, a siamese-type cylinder block can be ob~ained with a reduced influence of the casting strain in a cylinder barrel on the sleeve and with the casting stress remaining in the sleeve being made substantially uniform around the circumference of the sleeve while the release of heat of the sleeve is improved by heating -the sleeve to a predetermined temperature to castingly incorporate it, so that the amount of each sleeve thermally expanded may be substantially uniform around the circumference of the sleeve during the opera-tion of the engine.

Still further the present invention provides a process for manufacturing a siamese-type cylinder block wherein a water-jacket shaping breakable core is removed at ambient temperature and a thermal treatment is conducted to an extent such that ; strain relieving may be achieved, thus economically producing a high performance siamese-type cylinder block.

Accorcling to the present invention, there is provided a 4 _ .:
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r3 process for manufac-turing a siamese-type cylinder block, compris-ing a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is incorporated in each cylin-der barrel of a siamese-type cylinder barrel made of an aluminum alloy and consisting of a plurality of cylinder barrels co~mected in series, and a mechanically wor]cing or machining step of form-ing the inner peripheral surface of each sleeve of the resulting cylinder block blank in-to a true circle, wherein -the blank making step includes placing highly rigid sleeves each having a thick-ness of 10~ or more of the inner diameter thereof lnto a siamese-- type cylinder barrel molding cavity in a mold and then pouring a molten metal of aluminum alloy under a pressure into the cavity to effect a casting.

According to the present invention, there is also provided a process for manufacturing a siamese-type cylinder block, comprising a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is incorporated in each cylinder barrel of a siamese-type cylinder barrel made of :20 an aluminum alloy and consisting of a plurality of cylinder bar-rels connected in series, and a mechanically working or machining step of forming the inner peripheral surface of each sleeve of the resulting cylinder blocX blank into a true circle, wherein the blank making step includes placing highly rigid sleeves each having a thickness of 10% or more of the inner diameter thereo~
into a siamese-type cylinder barrel molding cavity in a mold and then pouring a mo~ten metal of aluminum alloy under a pressure into the cavity to cast a cylinder block blank, and subjecting the cylinder block blank to a thermal treatment to reduce the casting strain produced in the cylinder barrel.

Further, according to the present invention, there is provided a process for manufacturing a siamese-type cylinder block, comprislng a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is incorporated in each cylinder barrel of a siamese-type cylinder barrel made of .:

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~2~ 65i an aluminum alloy and consisting of a plurallty of cylinder bar-rels connected in series, and a mechanically working or machining step of forming the inner peripheral surface of each sleeve of the resulting cylinder block blank into a true circle, wherein the blank making step includes heating highly rigid sleeves each having a thickness of 10% or more of the inner diameter thereof to a temperature of 150 to 700C, thereafter placing them in a siamese-type cylinder barrel mold:lng cavlty in a mold and then pouring a molten metal of aluminum alloy under a pressure into the cavity to effect a casting.

Yet further, according to the present invention, there is provided a process for manufacturing a siamese-type cylinder block, comprising a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is incorporated in each cylinder barrel of a siamese-type cylinder barrel made of an aluminum alloy and consisting of a plurality of cylinder bar-- rels connected in series and which includes a water ~acket faced by the entire periphery of the siamese-type cylinder barrel, and ~` 20 a mechanical working or machining step o~ forming the inner peripheral surface of each sleeve of the resulting cylinder block blank into a true circle, wherein the blank making step includes placing the sleeves and a water-jacket shaping breakable core surrounding the sleeves in a siamese-type cylinder barrel molding cavity in a mold and then pouring a molten metal of aluminum ~: alloy into the cavity to cast a cylinder block blank, breaking : the core at an ambient temperature to remove it from the cylinder block blank, and sub~ecting the cylinder block blank to anneal-ing.

According to the procedure of the above process, a highly rigid sleeve having a thickness of 10% or more o~ the inner diameter thereof is castingly incorporated in each cylinder barrel and therefore, the influence of the casting strain in the cylinder barrel can be diminished on the sleeve and moreover, the amount of sleeve cut can be reduced when working o~ the inner s~ s~
peripheral surface of the sl2eve into a true circle to improve economy.

While the casting incorporation of each thick and highly rigid sleeve having a thic]cness of 10% or more of the inner diameter thereof in each cy:Linder barrel results in a - diminished influence of the casting strain in the cylinder barrel on the sleeve, the cylinder block blank is then subiected to a thermal treatment to reduce the casting strain in the cylinder barrel and thereafter, the inner peripheral surface of the sleeve is worked into a true circle, so that even if the sleeve is con-sequently of a smaller thickness and a lower rigidity, the reduc-tion of the casting strain in each cylinder barrel enable the influence of such casting strain to be substantially eliminated.

:: Therefore, in the op~ration of an engine assembled using such a cylinder block, the amount of permanent deformation of each sleeve in inner diameter is very small and hence, a clearance is suppressed to the utmost from ~eing produced between a piston ring and the sleeve, thus making it possible to overcome problems of an increase in amount of blow-by gas and a useless consumption of oil.

In addition, since the influence of the casting strain : 25 in each cylinder barrel is reduced on each sleeve, it is possible to place the adjacent sleeves maximally close to each other, whereby the cylinder block and thus, the entire engine can be small-sided to achieve a lightweight.

Further, each thick and highly rigid sleeve having a thickness of 10~ or more of the inner diameter thereof is heated to a temperature of 150 to 700C and castingly incorporated in each cylinder barrel and hence, the influence of the casting strain in the cylinder barrel on the sleeve is reduced, while the casting stress remaining in the sleeve is substantially uniform around the circumference of the sleeve and further, the release \:
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of heat of the sleeve is good. In the operation of an engine assembled using such a cylinder block, the amount of each sleeve thermally expanded is substantially uniform around the circumfer-ence of the sleeve and thus, clearance can be minimized between the piston ring and the sleeve as in the case described above.

In addition, bscause the ~nfluence of the casting strain in each cylinder barrel on each sleeve is smaller and the casting stress remaining in the s:Leeve is substantially uniform - lO around the circumference of the s:Leeve, it is possible to place the ad~acent sleeves as close to each other as possible as in the case described above.

Further, since the water-~acket shaping core is broken at ambient temperature and removed from the cylinder block blank, the hardness of the blank cannot be reduced. Thereupon, a T6 treatment i5 not required for recovering the hardness of the ; blank and thus, a high performance cylinder block can be provided by merely subjecting the blank to an annealing treatment for strain relief.
Any thermal treatment is also not required for removing the core, and the above annealing treatment is conducted in a shorter time at a relatively low temperature, thu9 making it possible to su~stantially reduce energy consumption and improve an economy.

The features and advantages of the invention will become apparent from reading the following description taken in con~unction with the accompanying drawings, in which:-Fig.s 1 to 4 illustrate an in-line siamese-type cylin-der block provided according to the present invention;

Fig. 1 is a perspective view of the apparatus from above;

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Fig. 2 is a sectional view taken along line II-II in Fig~ l;

Fig. 3 is a perspective view of the apparatus from below;
Fig. 4 is a sectional view taken along line IV-IV in Fig. 2;

Fig. 5 is a perspective view of a siamese-type cylinder block blank produced in a casting process accordlng to the pre-sent invention, viewed from above;

Fig. 6 is a front view in vertical section of the cast-ing apparatus with the mold open;
Fig. 7 is a front view in vertical section of the cast-ing apparatus with the mold closed;

Fig. 8 is a sectional view taken along line VIII-VIII
in Fig, 7;

Fig. 9 is a sectional view taken along line IX-IX in Fig. 8;

Fig. 10 is a sectional view taken along line X-X in Fig. 6;
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Fig. 11 is a perspective view of a sand core from above;
Fig. 12 is a sectional view taken along line XII-XII in Fig. 11;

Fig. 13 is a graph representing the relationship between time and displacement of plunger and the relationship i _ g _ '.

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between time and pressure of molten metal;

Fig. 14 is a graph illustrating the relationship between the depth of sleeve from its cylinder head-bound surface and the amount of sleeve permanently deformed at inner diameter;

Fig.s 15A to 15C are micrographs showing the metal structure of the cylinder barrel in the siamese-type cylinder block obtained according to the present invention, respectively;

Fig.s l~A to 16C are micrographs showing the metal structure of the cylinder barrel in the siamese-type cylinder block in the comparatlve example, respectively;

Fig. 17 is a micrograph showing the metal structure of the deposited portion between the cylinder barrel and the sleeve in the siamese-type cylinder block obtained according to the pre-sent invention, Fig. 1~ is a micrograph showing the metal structure of the deposited portion batween the cylinder barrel and the sleeve in the siamese-type cylinder block in the comparative example;

Fig. l9A is a graph illustrating the ~elationship between the depth of sleeve from its cylinder head-bou~d surface and the amount of sleeve permanently deformed in inner diameter in the siamese-type cylinder block obtained according to the pre-sent invention;
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Fig. l9B is a graph illustrating the relationship between the depth of sleeve from its cylinder head-bound surface and the amount of sleeve permanently deformed in inner diameter in the siamese-type cylinder block in the comparative example;
and Fig. 20 is a perspective view of a V-shaped slamese-, , ~.: . .

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~ 2 type cylinder block, viewed from above.

Referring to Figs. 1 to ~, therein is shown an in-line siamese-type cylinder block S obtained according to the present invention. The cylinder block S is comprised of a cylinder block body 2 made of an aluminum alloy and a sleeve 3 made of a cast iron and cast in the body 2. The cylinder block body 2 is con-stituted of a siamese-type cylinder barrel 1 consisting oE a plu-rality of, e.g., four (in the illustrated embodiment) cylinder barrels 11 to 14 connected to one another in series, an outer wall 4 surrounding the siamese-type cylinder barrel 1, and a crankcase 5 connected to the lower edges of the outer wall 4.
The sleeve 3 is cast in each of the cylinder barrels 11 to 14 to define a cylinder bore 3a.

A water jacket 6 is defined between the siamese-type cylinder barrel 1 and the outer wall 4, so that the entire periphery of the siamese-type cylinder barrel 1 faces the water jacket 6. At the opening on the cylinder head blnding side at the water jacket 6, the siamese-type cylinder barrel 1 is con-nected with the outer wall 4 by a plurality of reinforcing deck portions 8, and the space between the ad~acent reinforcing deck portions 8 functions as a communication port 7 into a cylinder head. Thereupon, the cylinder block S is constituted into a closed deck type.

Fig. 5 illustrates a cylinder block blank Sm produced by the casting, and a sleeve in this blank Sm has an inner diame-ter of 78 mm and a thickness of 10% or more of the inner diameter thereof, for example, of 8 mm.

Fig.s 6 to 10 illustrate an apparatus for casting a cylinder block blank Sm, which apparatus comprises a mold M. The mold M is constituted of a liftable upper die 9, first and second laterally split side dies 101 and 12 (see Fig.s 6 and 7) dis-posed under the upper die 9, and a lower die 11 on which both the -', ', . ' - - ' ' ~
-- --~ : i ~t.~ s side dies lOl and l2 are slidably laid.

A clamping recess 12 is provided at the underside of the upper die 9 to define the upper surface of a first cavity Cl, and a clamping pro~ection 13 adapted to be fitted in the recess 12 is provided on each of the side dies lOl and l2 The first cavity ~l consists of a siamese-type cylinder barrel molding cav-ity Ca defined between a water-jacket molding sand core 59 as a breakable core and an expansion shell 46, and an outer wall mold-ing cavity Cb defined between the sand core 59 and both the side dies lOl and 102, in the clamped condition as shown in Fig. 7.

AS shown in Fig.s 8 and 9, the lower die ll includes a basin 14 for receiving a molten metal of aluminium alloy from a furnace (not shown), a pouring cylinder 15 communicating with the basin 14, a plunger 16 slidably fitted in the pouring cylinder 15, and a pair of runners 17 bifurcated from the basin 14 to extend in the direction of the cylinder barrels. The lower die ll also has a molding block 18 projectin~ upwardly between both of the runners 17, and the molding block 18 defines a second cav-ity C2 for molding the crankcase 5 in cooperation with both the side dies 101 and 102. The cavity C2 is in communication at its upper end with the first cavity Cl and a~ ~ts lower end with both the runners 17 through a plurality of gates 19.

The molding block 18 is comprised of four first taller semi-columnar molding portions l8l formed at predetermined inter-vals, and second protruded molding portions 182 located between the ad~acent first molding portions l8l and outside both of the outermost first molding portions l81. Each first molding portion 18l is used for molding a space 20 (see Fig.s 2 and 3) in which a crankpin and a crankarm are rotated, and each second molding por-tion 182 is employed to mold a crank journal bearing holder 21 (see Fig.s 2 and 3). Each gate 19 is provided to correspond to each of the second molding portions l82 and designed to p0rmit the charging or pouring of a molten metal in larger volume por-~, .

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tion of the second cavity C2 in an early stage.

soth the runners 17 are defined with their bottom sur-faces stepped in several ascending stairs to stepwise decrease in section area from the basin 14 toward runner extensions 17a.
Each raised portion 17c connected to each of the stepped portion 17b is angularly formed to be able to smoothly guide molten metal into each of the gates 19.

With the sectiona] area of the runner 17 decreasing stepwise in this manner, a larger 'amount of molten metal can be charged or poured, at the portion larger in sectional area, into the second cavity C2 through the gate 19 at a slower speed, and at the portion smaller in sectional area, into the second cavity through the gate 19 at a faster speed, so that the molten metal level in the cavity C2 rises substantially equally over the entire length of the cavity C2 from the lower ends on the oppo-site sides thereof. Therefore, the molten metal cannot produce any turbulent flow and thus, a gas such as air can be prevented from being included into the molten matal to avoid the generation of mold cavities. In addition, a molten metal pouring operation is effectively conducted, leading to an improved casting sffi-ciency.

As shown in Fig.s 6 and 7, a locating projection 22 is provided on the top of each of the first molding portions 181 and adapted to be fitted in the circumferential surface of the sleeve 3 of cast iron, and a recess 23 is defined at the central portion of the locating projection 22. A through hole 24 is made in each of two first molding portions 181 located on the opposite sides to penetrate the first molding portion 181 on each of the oppo-site sides of the locating projection 22. A pair of temporarily placed pins 2~ are slidably fitted in the through holes 24, respectively, and are used to temporarily place the water-jacket molding sand core 59. The lower ends of the pins 25 are fixed on a mounting plate 26 dlsposed below the molding block 18. Two .

' support rods ~7 are inserted through the mounting plate 26, and a coil spring 28 is provided in compression between the lowex por-tion of each of the support rods 27 and the lower surface of the mounting plate 26. During opening of the mold, the mounting plate 26 is subjected to the resilient force of each of the coil springs 28 to move up untll it abuts against the stopper 27a on the fore end of each of the support rods 27. This causes the fore end of each of the pins 25 to protrude from the top surface of the first molding portion 181. A recess 25a ls made in the fore end of each of the pins 25 and adapted to be engaged by the lower edge of the sand core.

A through hole 29 is macle between the two first molding portions 181 located on the opposite sides at the middle between both the through holes 24, and an operating ~in 30 is slidably ~- fitted in the through hole 29. The lower end of the operating pin 30 is fixed to the mounting plate 26. During opening of the mold, the fore end of the operating pin 30 protrudes into the recess 23, and during closing of the mold, it is pushed down by an expanding mechanism 41, thereby retracting the pins 25 from the top surfaces of the first molding portions 181o A core bedding recess 31 for the sand core 59 is - provided at two places: namely in the central portions of those walls of the first and second side dies 101 and 12 defining the second cavity C2. Each of the core bedding recesses 31 consists of an engaging bore 31a in which the sand ~ore is positioned, and a clamp surface 31b formed around the outer periphery o~ the opening of the engaging bore 31a for clamping the sand core.

In the clamping recess 12 of the upper die 9 are a plu-rality of third cavities C3 opened into the first cavity C1 to permit the overflow of molten metal and a plurality of fourth cavities C4 for shaping the communication holes 7. The upper die 9 also has gas vent holes 32 and 33 therein which are communi-cated with each of the third cavities C3 and each of the fourth .

~ 2 cavities C4, respectively.

Closing pins 34 and 35 are inserted into the gas vent holes 32 and 33, respec-tively, and are fi~ed at their upper ends to a mounting plate 36 disposed above the upper die 9.

The gas vent holes 32 and 33 have smaller diameter por-tions 32a and 33a, respectively, which extend upwardly a prede-termined length from the respect:Lve ends of the gas vent holes 32 and 33, communicating with the cavities C3 and C4, and which are fitted with the corresponding closing pins 34 and 35 so that the third and fourth cavities C3 and C4 may be closed.

A hydraulic cylinder 39 is disposed between the upper surface of the upper die 9 and the mounting plate 36 and operates to move the mounting plate 36 upwardly or downwardly, thereby causing the individual closing pins 34 and 35 to close the corre-sponding smaller diameter portions 32a and 33a. It is to be noted that the reference numeral 40 designates a rod for guiding the mounting plate 36.
The expanding mechanism 41, which is provided in the upper die 9 for applying an expansion force to the sleeve 3 cast in each of the cylinder barrels ll to 14, is constituted in the following manner.

: A through hole 42 is made in the upper die 9 with its center line aligned with the extension o~ the axis of the operat-ing pin 30, and a support rod 43 is loosely lnserted ~nto the through hole 42. The support rod 43 is fixed at its upper end to a bracket 44 above the upper surface of the upper die 9, and it has, as a sealing member, a plate 45 secured at its lower end for blocking the entry of molten metal. The blocking plate 45 is formed at its lower surface with a pro~ectlon 45a which is fit-table in the recess 23 at the top of the first molding portion 181 .

.- ~ ~ . , : - ' ' ` -The hollow expansion shell ~6 has a circular outerperipheral surfac~ and a tapered hole 47 having a downward slope from the upper portion toward the lower portion. The lower por-tion of the support rod 43 pro~ecting downwardly from the upper die g is loosely inserted into the tapered hole 47 of the expan-sion shell 46 whose upper end sur~Eace bears against a pro;ection 48 disposed as a sealing member on the recess 12 of the upper die 9 and whose lower end ~urface is carried on the blocking plate 45. AS shown in Fig. 10, a plurality of slit grooves 49 are made in the peripheral wall of the expansion shell 46 ak circumferen-tially equal intervals to radially extend alternately from the inner and the outer peripheral surfaces of the expansion shell 46.

A hollow operating or actuating rod 50 is slidably fit-ted on the support rod 43 substantially over its entire length for expanding the expansion shell 46, and is comprised of a frus-toconical portion 50a adapted to be fitted in the tapered hole ~7 of the expansion shell 46, and a truly circular portion 50b con-tinuously connected to the frustoconical portion 50a so as to be slidably fitted in the through hole 42 and protruded from the upper die 9. A plurality of pins 57 protrude from the frustocon-ical portion 50a and e~ch is inserted into a vertically long pin hole 58 of the expansion shell 46 to prevent the expansion shell 46 from being rotated while permitting the vertical movement of the frustoconical portion 50a.
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A hydraulic cylinder 51 is fixedly mounted on the upper surface of the upper die g and contains a hollow piston 52 therein. Hollow piston rods 531 and 532 are mounted on the upper and lower end surfaces of the hollow piston 52 and pro~ect there-from to penetrate the upper and lower end walls of a cylinder body 54, respectively. The truly circular portion 50b of the operating rod 50 is inserted into a hole through the hollow pis-ton 52 and the hollow piston rods 531 and 532~ and anti-slip-off stoppers 561 and 562 each fitted in an annular groove of the -.

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: , ' ~ ~ S6~ ~ 5 truly circular portion 50b are mounted to bear against the upper end surface of the hollow piston rod 531 and the lower end sur-face of the hollow piston rod 532~ respectively, so that the hol-low piston 52 causes the operating rod 50 to be moved up or down.
The four expanding mechanisms 41 may be provided to correspond to the individual cylinder barrels 11 to 14 of the cylinder block S, respectively.

Fiy . s 11 and 12 show the water-jacket molding sand core 59 which is constituted of a core body 61 comprising four cylin-drical portions 601 to 604 corresponding to the four cylinder barrels 11 to 1~ of the cylinder block S with the peripheral interconnecting walls of the ad~acent cylindrical portions being eliminated, a plurality of pro~ections 62 formed on the end sur-face of the core body 61 on the cylinder head binding side todefine the communication ports 7 for permitt~ng the communication of the water jackets 6 with the water ~ackets of the cylinder head, and a core print 63 protrudedly provided on the opposite (in the direction of the cylinder barrels) outer side surfaces of the core body 61, e.g, on the opposlte outer side surfaces of two cylindrical portions 602 and S03 located between the outermost ones in the iIlustrated embodiment. Each of the core prints 63 is formed of a larger diameter portion 63a integral with the core body 61, and a smaller diameter portion 63b on the end surface of the larger diameter portion 63a. In this case, the projection 62 is sized to be loosely fitted in the aforesaid fourth cavity C4.
The sand core 59 is formed, for example, of a resin-coated sand.

Description will now be made of an operation of casting a cylinder block blank Sm in the above casting apparatus.
First, as shown in Fig. 6, the upper die 9 is moved up and both the side dies 101 and 12 are mo~ed away from each other, thus causing the opening of the mold. In the expanding mechanism 41, each hydraulic cylinder 51 is operated to cause the hollow piston 52 to move the operatin~ rod 50 downwardly, so that `.i~
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the downward movement of the frustoconical portion 50a allows the expansion shell 46 to be co~tracted. In addition, the hydraulic cylinder 39 of the upper die 9 is operated to move the mounting plate 36 upwardly. This causes the individual closing pins 34 and 35 to be released from the corresponding smaller diameter portions 32a and 33a, respectively communicating with the third and fourth cavlties C3 and C4. Further, the plunger 16 in the pouring cylinder 15 is moved downwardly.

The substantially truly circular and highly rigid sleeve 3 of cast iron having a thi~kness as large as ~ mm is loosely fitted in each expansion shell 46, and the opening at the upper end of the sleeve 3 is fitted and closed by the pro~ection 48 of the upper die 9. The end surface of the sleeve 3 is aligned with the lower end surface of the pro;ection 45a on the blocking plate 45, while the opening at the lower end of the sleeve 3 is closed by the blocking plate ~5. The hydraulic cylinder 51 of the expanding mechanism 41 is operated to cause the hollow piston 52 therein to lift the operating rod 50. The frustoconical portion 50a is thereby moved upwardly, so that the expansion shell 46 is expanded. Thereupon, the sleeve 3 is sub-jected to an expansion force and thus reliably held on the expan-sion shell 46.

As shown in Fig.s 6 and 12, the lower edges of the cylindrical portions 601 and 604 on the outermost oppositP sides in the sand core 59 are each engaged in the recess 25a of each pin 25 projecting from the top of each of the first molding por-tions 181 on the opposite sides in the lower die 11, thereby tem-porarily placing the sand core 59.

The side dies 101 and 12 are moved a predetermined distance toward each other to engage each core bedding recess 31 with each core print 63, thus really plac~ng the sand core 59.
More specifically, the smaller diameter 63b of each of the core prints 63 in the sand core 59 is fitted into the engaging hole , 31a of each of the core bedding recesses 31 to position the sand core 59, with the end surface of each of the larger diameter por-tions 63a a parallel to the direction of the cyllnder barrels, being mated wi-th the clamping surface 31b of each core bedding recess 31 to clamp the sand core 59 by the clamping surface 31b.

As shown in Fig. 7, the upper dle 9 is moved downwardly to insert each of the sleeves 3 into each of the cylindrical por-tions 601 to 604 of the sand core 59, and the projection 45a of the molten metal-entering blocking plate 45 is fitted into the ~ecess 23 at the top of the first Imolding portion 181. This causes the pro~ection 45a of the blocking plate 45 to push down the operating rod 30, so that each of the pins 2s is moved down and retracted from the top surface of the first molding portion 18~. In addition, the clamping recesses 12 of the upper die 9 are fitted with the clamping projections 13 of both the side dies 101 and 12~ thus effecting the clamping of the mold. This down-ward movement of the upper die 9 causes the projection 62 of the sand core 59 to be loosely inserted into the fourth cavity C4, wh2reby a space is defined around the pro~ection 62. A space 70 for shaping the reinforcing deck portion 8 is also defined between the end surface of the sand core 59 and the inner surface of the recess 12 opposed to such end surface.

A molten metal of aluminum alloy is supplied out of a furnace into the basin 14 of the lower die 11, and the plunger 16 ~- is moved up to pass the molten metal through both the runners 17 and pour it into the second cavities C2 and the first cavities Cl from the opposite lower edges of the second cavities C2 vla the gates 19. The application of this bottom pouring process allows a gas such as air in both the cavities Cl and C2 to be forced up by the molten metal and vented upwardly from the upper die 9 via - the gas bent holes 32 and 33 in communication with the third and fourth cavities C3 and C4.

In the present case, both the runners 17 have the run-- , . - . -. . .
, , . .. , . . -. ' . - - - ' ' ' . . ~ ' , ' - .

.
.

-j5 ner bo-ttom stepped in several upward stairs form the basin 14 so that the sectional area may decrease stepwise toward the runner extensions 17a as described above and hence, the upward movement of the plunger 16 causes a molten m0tal to be passed from both the runners 17 through the gates 19 and to smoothly rise in the second cavlties C2 substantlally lmiformly over the entire length thereof from the opposite side lo~er end thereof. Thus, the molten metal cannot produce a turbulent flow in both the cavities Cl and C2, and a gas such as air can be prevented from being included into the molten metal to avoid the generation of any mold cavities.

After the molten metal has been poured in the third and fourth cavities C3 and C4, the hydraulic cylinder 39 on the upper die 9 is operated to move the mounting plate down, thereby caus-ing the closing pins 34 and 35 to close the smaller diameter por-tions 32a and 33a communicating with the cavities C3 and C4, respectively.

In the above pouring operation, the displacement of the plunger 16 for pouring the molten metal into the second and first cavities C2 and Cl and the pressure of the molten metal are con-trolled as shown in Fig. 13.

More spscifically, the speed of plunger 16 is con-trolled at three stages of first to third velocities Vl to v3.
In the present embodiment, the first velocity Vl is set at 0.08-0.12 m/sec., the second velocity V2 is at 0.14-0.18 m/sec., and the third velocity V3 is at 0.04-0.08 m/sec. to give a substan-tial deceleration. This control in velocity at three stages pre-vents the waving of the molten metal and produces a calm molten metal flow which cannot include a gas such as air thereinto, so that the molten metal can be poured into both the cavities C2 and Cl with a good efficiency.

At the first velocity Vl of the plunger 16, the molten metal merely ~ills both the runners 17 and hence, the pressure Pl of the molten metal is kept substantially constan-t. At the sec-ond and third velocities V2 and v3 of the plunger 16, the molten metal is poured or charged into both the cavities Cl and C2 and therefore, the pressure P2 of the molten metal rapidly increases.
After the plunger 16 has been moved at the third velocity V3 for a predetermined period of time, the pressure P3 of the molten metal is maintained at 150-400 kg/cm2 for a period of about 1.5 seconds, whereby the sand core 5~ is completely enveloped in the molten metal to form a solidified film of molten metal on the surface thereof.

After the above time has elaps0d, the plunger 16 is deceleratively moved at the velocity v4, so that the pressure P4 of the molten metal increases. When the pressure has reached a level P5 of 200-600 kg/cm2, the movement of the plunger 16 is stopped, and under this condition, the molten metal is solidi-fied.

If the pressure of the molten metal is kept constant for a predetermined period of time to form the solidified ~ilm of molten metal on the surface of the sand core 59 as described above, the sand core 59 can be protected by th~ fil~ against breaking. In addition, the sand core 59 is expanded due to the molten metal, but because the projection 62 is loosely inserted in the fourth cavity C4, it follows the expansion of the sand core 59, whereby the folding of the pro;ection 62 is avoided.

Since the sand core 59 is clamped in an accurate posi-tion by both the side dies 101 and 12 through each of the core prints 63, it cannot float up during pouring the molten metal into the first cavities Cl and during pressing the molten metal in the cavities Cl. In addition, since the end surface of the larger diameter portion 63a of each core print 63 mates with the clamping surface 31b, as the sand core 59 is being expanded, the deforming force thereof is suppressed by each of the clamping :.

~56?~65 surfaces 31b to prevent the deformation of the sand core 59.
Thus, a siamese-type cylinder barrel 1 is provided having a uni-form thickness around each of the sleeves 3.

As discussed abnve, a closed deck-type cylinder block blank can be cast with substantially the same production effi-ciency as in a die casting process, by controlling the speed of plunger 16 and the pressure of the molten metal.

After the completion of solidification of the molten metal, the hydraulic cylinder 51 of the expanding mechanism 41 is operated to move the operating rocl 50 down, thereby eliminating the expansion force of the expansion shell 46 on the sleeve 3.
The mold is opened -to yield a cylinder block blank Sm as shown in Fig, 5.
In this cylinder block blank Sm, the influence of the -~ casting strain in each of the cylinder barrels 11 to 14 on each sleeve 3 is small, because each sleeve 3 is thick and highly rigid.
Then, the cylinder block blank Sm is sub;ected to a thermal treatment for a period of 3 hours at a temperature of 220~ to reduce the casting strain produced in each of the cylin-der barrels 11 to 14~
Thereafter, the protruded portions 64 (Fig. 5) eachincluding the pro~ection 62 of the sand core 59 are cut away from the cylinder block blank Sm, so that the communication poxts 7 are consequently defined at the portions corresponding to the projections 62 and the reinforcing deck portions 8 are each also formed between the adjacent communication ports 7. Subsequently, the sand extraction is effected to define the water jacket 6, and the inner peripheral surface of each sleeve 3 is worked into a true circle to finish it to a thickness of 5 mm and further another predetermined working operation is conducted to produce a ,:

'' ' , ~ '." : : ' : ~ - ' ' ' , - ' , . ~ .

. , , ~ . , .
, ~ ~
- .

. . , cylinder block S as shown in Fig.s 1 to 4~

In Fig. 14, the line a represents the results of mea-surements obtained by heating the whole of the above ob-tained cylinder block S for a period of one hour at the temperature reached during operation of an engine, ~.e., at 200C and deter-mining the amount of permanent deformation of the inner diameter of the sleeve at an ambient temperature. The line b represents the results of measurements obtained in the same manner with the cylinder block produced in the comparative example from the : cylinder block blank as cast without the thermal treatment.

As apparent from Fig. 14, in the cylinder block in the comparative example, the amount of permanent deformation of the inner diameter of the sleeve Pxhibits a maximum value of 61~m at the depth of the sleeve of 20 mm from its cylinder head-bound surface, while in the cylinder block S obtained according to the present invention, the amount of permanently deformed inner diam-eter of the sleeve exhibits a maximum value of 15 ~ m at the depth of the sleevle 30 mm from its cylinder head-bound surface c.
This means that the thermal treatment of the cylinder block blank Sm after casting enables the amount of permanent deformation of the sleeve at its inner diameter to be substantially reduced.

It is to be noted that if the thickness of sleeve 3 is less than 10% of its lnner diameter, riyidity of the sleeve 3 is reduced, so that the castlng strain in each of the cylinder bar-rels 11 to 14 may influence each sleeve 3 to produce a strain in the sleeve 3. Therefore, a thickness less than 10% of the inner diameter is not pre~erred.

In the above casting operation, if the sleeves 3 are castingly ~ncorporated in a state previously heated to a tempera-ture of 150 to 700C, the casting stress remaining in the sleeve 3 can be substantially uniform around the circumference of the sleeve 3, and a good close adhesion can be ensured between each ~, .
' . .

.:
.

of sleeve 3 and each of the cyl~nder barrels 11 to 14.

Fig.s 15~, 15B and 15C show the metal structure of the aluminum alloy in micrographs (200 times1 of the cylinder barrels 11 to 14 in the cylinder block S produced in the process of the present invention, i.e., by previously heating the sleeves 3 to a temperature of 250 to 500C and casting-in the sleeves, respec-tively, at the portion close to the sleeves 3 (in Fig. 15A~, the central portion (in Fig. 15B) and the portion close to the sand core 59 (in Fig. 15C). As apparent from these Figures, ln the cylinder barrels 11 to 14, the metal structures are substantially identical with one another at the portion close to the sleeves 3, at the central portion and at the portion close to the sand core 59. This is because the heating of the sleeves 3 to a tempera-15 ture of 250 to 500C followed by the casting-in thereof permits the speed of the molten metal solidified to be substantially uni-form around the sleeve 3. The metal structure at the portion between the adjacent sleeves 3 is substantially identical with that shown in Fig. 15A. Also due to the fact that the shrinkage of the sleeve 3 follows the solidification shrinkage of the molten metal, the casting stress remaining in the sleeve 3 is substantially uniform around the circumference of the sleeve 3.

` Fig.s 16A, 16B and 16C show the metal structure of the 25 aluminum alloy in the micrographs (200 times) of the cylinder barrels in the cylinder block obtained in the comparative example from the incorporation of the sleeves in the cylinder barrels at an ambient temperature and corresponding to Fig.s 15A, 15s and 15C, respectively. As apparent from these Figures, the use of the sleeves at an ambient temperature results in different metal structures at the portion close to the sleeves, the central por-tion and the portion close to the core, and in substantially the same metal structure at the portion between the adjacent sleeves as that shown in Fig. 16A. In addition, the shrlnkage of the sleeve may not follow the solidification shrinkage of the molten metal and consequently, the casting stress remaining in the ., ; - 24 -, ', . ' ',, ' , ' .
. .
- . .
. , - --sleeve may be non-uniform around its circumference.

Fig. 17 shows th~ metal structure of the cast iron and the aluminum alloy in the micrograph (400 times) of the deposited portion between the sleeve 3 and cylinder barrel 11 in the cylin-der bloc~ S produced according to the present invention. It can be seen in this Figure that the adhesion between the cast iron and the aluminum alloy is good at the interface, namely the deposited portion between the sleeve 3 and the cyllnder barrel and no clearance is produced between them. This results in a good release of heat from the sleeve 3.

Fig. 18 shows the metal structure of the cast iron and the aluminum alloy in the micrograph ~400 times) of the deposited portion between the sleeve 300 and the cylinder barrel 1001 in the cylinder block obtained from the incorporation of the sleeve at an ambient temperature. It can b~ seen in this Figure, that the adhesion between the casting iron and the aluminum alloy is inferior at the interface, namely the deposited portion between the sleeve 300 and the cylinder barrel 1001 and a very small clearance G is produced between them. As a result, the release of heat from the sleeve 300 is inferior.

In the cylinder block S produced according to the pre-sent invention, the casting stress remaining in the sleeve 3 is substantially uniform around its circumference and the release of heat of the sleeve 3 is good. Therefore, when an engine assem-bled using this cylinder block is operated, the amount of each sleeve thermally expanded is substantially uniform around its circumference.

After removing each protruded portion 64 formed in cooperation of each fourth cavity C4 and each pro~ection 62 of the sand core 59 in the cylinder block blank Sm as shown in Fig.
5 to make each communication port 7 and each reinforcing deck portlon 8, the cylinder block blank Sm is subjected to sand ex-,, :;., :. .

~2 ~
traction and to anneali.ng in a manner described herelnbelow, thus making it possible to economically provide a high performance cylinder block S.

First, the sand core 59 is roughly broken from the com-munication port 7 and the opening 75 made from each core print 63 of the sand core 59 in the cylinder block blank Sm using a chisel, punch, drill or the like, and vibration is then applied to the cylinder block blank Sm to promote ~he breaking of the sand core 59, followed by the extraction of the sand from the blank Sm. In this case, the vibration causes the breaking of the sand core 59 to proceed and hence, approximately 90% of the sand : core 59 is removed from the cylinder block blank Sm.

Further, utilizing the aforesaid communication port 7 and opening 75, the inside of the cylinder block blank Sm is sub-jected to a short blasting or sandblasting treatment to com-pletely remove the sand core 59 from the blank Sm, thus producing the water ~acket 6.

The cylinder block blank Sm having the sand core 59 thus removed therefrom is subjected to annealing, i.e., a thermal treatment of heating the blank Sm to a temperature of 220C for a period of 3.5 hours for strain relief.
: 25 The resulting cylinder block blank Sm is subjected to cleaning and checking, followed by machining such as working into :- a true circle for each sleeve 3 to provide a cylinder block S as shown in Fig.s 1 to 4.

Fig. 19A illustrates the results of the measurements for the amount of permanent deformation of the inner diameter of a sleeve at an ambient temperature, when the above cylinder block S as a whole is heated to the temperature reached during the operation of the engine of 200 for a period of 1.5 hours, and Fig. l9B illustrates the results of the similar measurements in , .

.

~5~ 5 the case of the cylinder block obtained in the comparative example from the conven-tional method, i.e., the procedure includ-ing the heating treatment for the removal of the sand core, the T6 treatment and the like.

In Fig. l9A, the lines i to iv represent the results of the measurements of the sleeves 3 in four cylinder barrels 1l to 14, respectively.

n As can be seen in Fig. 19A, the amount of permanent deformation of the inner diameter of the sleeve in the cylinder block S produced according to the present invention is of a maxi-mum value of 20~ m at a depth of 30 to 50 mm from the cylinder head-bound surface c, and in this way, the amount of sleeve per-manently deformed is substantially reduced and also less dis-tributed in the above range of depth. This is attributable to the fact that the removal of the sand core 59 at an ambient tem-perature causes the non-uniform stress not to remain in each sleeve 3.

On the other hand, as can be seen in Fig. l9B, the amount of permanent deformation of the inner diameter of the sleeve in the cylinder block in the comparative example exhibits a maximum value of 55 ~ m at a sleeve depth of 30 mm from the cylinder head-bound surface of the sleeve, and the amount of per-manent deformation of the sleeve is largely distributed over the regions in a range of depth of 10 to 50 mm which are at an increased temperature during the operation of the engine. This is due to the fact that the T6 treatment causes non-uniform stress to remain in each sleeve.

~ .
- .' ' ' ~ : .. : -: :
.

Fig. 20 shows a V-shaped siamese-type cylinder block S' including two siamese-type cylinder barrels 1. The cylinder block S' is also made by the same blank making s-tep and machining step as described above. In this Figure, the same reference characters are used to designate the same parts as in the embodi-ment shown in Fig. 1.

,.; 10 : : ' ' ' '' : ' :

.. ..

-- `
..
.

Claims (23)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:

1. A process for manufacturing a siamese-type cylinder block, comprising a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is cast in each cylinder barrel of a siamese-type cylinder barrel made of an aluminum alloy and consisting a plurality of cylinder barrels connected in series, and a mechanically working or machining step of forming the inner peripheral surface of each sleeve of said cylinder block blank into a true circle, wherein said blank making step includes placing highly rigid sleeves each having a thickness set as large as 10% or more of the inner diameter thereof into a siamese-type cylinder barrel molding cavity in a mold and then pouring a molten metal of aluminum alloy under a pressure into the cavity to effect a casting.

2. A process for manufacturing a siamese-type cylinder block according to claim 1, wherein the inner diameter of said sleeve in said blank making step is set at 78 mm, and the thickness thereof is at 8 mm.

3. A process for manufacturing a siamese-type cylinder block according to claim 1 or 2, wherein said cylinder block is of an in-line type.

4. A process for manufacturing a siamese-type cylinder block according to claim 1 or 2, wherein said cylinder block is V-shaped.

5. A process for manufacturing a siamese-type cylinder block, comprising a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is cast in each cylinder barrel of a siamese-type cylinder barrel made of an aluminum alloy and consisting of a plurality of cylinder barrels connected in series, and a mechanically working or machining step of forming the inner peripheral surface of each sleeve of said cylinder block blank into a true circle, wherein said blank making step includes placing highly rigid sleeves each having a thickness set as large as 10% or more of the inner diam-eter thereof into a siamese-type cylinder barrel molding cavity in a mold and then pouring a molten metal of aluminum alloy under a pressure into the cavity to cast a cylinder block blank, and subjecting said cylinder block blank to a thermal treatment to reduce the casting strain produced In said cylinder barrel.

6. A process for manufacturing a siamese-type cylinder block according to claim 5, wherein the inner diameter of said sleeve in said blank making step is set at 78 mm, and the thick-ness thereof is at 8 mm.

7. A process for manufacturing a siamese-type cylinder block according to claim 5, wherein said thermal treatment is carried out by holding said cylinder block blank at a temperature of 170 to 230°C for a period of 2 to 10 hours.

8. A process for manufacturing a siamese-type cylinder block according to claim 6, wherein said thermal treatment is carried out by holding said cylinder block blank at a temperature of 170 to 230°C for a period of 2 to 10 hours.

9. A process for manufacturing a siamese-type cylinder block according to claim 7 or 8, wherein said thermal treatment is carried out by holding said cylinder block blank for a period of 3 hours at a temperature of 220°C.

10. A process for manufacturing a siamese-type cylinder block according to claim 5 or 6, wherein said cylinder block is of an in-line type.

11. A process for manufacturing a siamese-type cylinder block according to claim 5 or 6, wherein said cylinder block is V-shaped.

12. A process for manufacturing a siamese-type cylinder block, comprising a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is cast in each cylinder barrel of a siamese-type cylinder barrel made of an alu-minum alloy and consisting of a plurality of cylinder barrels connected in series, and a mechanically working or machining step of forming the inner peripheral surface of each sleeve of said cylinder block blank into a true circle, wherein said blank mak-ing step includes heating highly rigid sleeves each having a thickness set as large as 10% or more of the inner diameter thereof to a temperature of 150 to 700°C to place them into a siamese-type cylinder barrel molding cavity in a mold and then pouring a molten metal of aluminum alloy under a pressure into the cavity.

13. A process for manufacturing a siamese-type cylinder block according to claim 12, wherein the inner diameter of said sleeve in said blank making step is set at 78 mm, and the thick-ness thereof is at 8 mm.

14. A process for manufacturing a siamese-type cylinder block according to claim 12 or 13, wherein the heating tempera-ture of said sleeve is of 250 to 500°C.

15. A process for manufacturing a siamese-type cylinder block according to claim 12 or 13, wherein said cylinder block is 31 .

of an in-line type.

16. A process for manufacturing a siamese-type cylinder block according to claim 12 or 13 wherein said cylinder block is V-shaped.

17. A process for manufacturing a siamese-type cylinder block, comprising a blank making step of providing a cylinder block blank in which a sleeve made of a cast iron is cast in each cylinder barrel of a siamese-type cylinder barrel made of an alu-minum alloy and consisting of a plurality of cylinder barrels connected in series and which includes a water jacket faced by the entire periphery of said siamese-type cylinder barrel, and a mechanically working or machining step of forming the inner peripheral surface of each sleeve of said cylinder block blank into a true circle, wherein said blank making step includes plac-ing said sleeves and a water-jacket shaping breakable core sur-rounding said sleeves in a siamese-type cylinder barrel molding cavity in a mold and then pouring a molten metal of aluminum alloy into said cavity to cast a cylinder block blank, breaking said core at an ambient temperature to remove it from said cylin-der block blank, and subjecting said cylinder block blank to an annealing treatment.

18. A process for manufacturing a siamese-type cylinder block according to claim 17, wherein said annealing treatment is carried out by holding said cylinder block blank at a temperature of 220°C for a period of 3.5 hours.

19. A process for manufacturing a siamese-type cylinder block according to claim 17 or 18, wherein said cylinder block is of an in-line type.

20. A process for manufacturing a siamese-type cylinder block according to claim 17 or 18, wherein said cylinder block is V-shaped.

21. A process for manufacturing a siamese-type cylinder block according to claim 17, wherein said breakable core is a sand core.

22. A process for manufacturing a siamese-type cylinder block according to claim 18, wherein said breakable core is a sand core.

23. A process for manufacturing a siamese-type cylinder block according to claim 21 or 22, wherein said sand core is shaped using a resin-coated sand.