US1455028A - Air-cooled engine cylinder and method of making same - Google Patents

Air-cooled engine cylinder and method of making same Download PDF

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US1455028A
US1455028A US500252A US50025221A US1455028A US 1455028 A US1455028 A US 1455028A US 500252 A US500252 A US 500252A US 50025221 A US50025221 A US 50025221A US 1455028 A US1455028 A US 1455028A
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cylinder
jacket
metal
members
block
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/02Cylinders; Cylinder heads  having cooling means
    • F02F1/04Cylinders; Cylinder heads  having cooling means for air cooling
    • F02F1/06Shape or arrangement of cooling fins; Finned cylinders
    • F02F1/08Shape or arrangement of cooling fins; Finned cylinders running-liner and cooling-part of cylinder being different parts or of different material
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S29/00Metal working
    • Y10S29/012Method or apparatus with electroplating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/4927Cylinder, cylinder head or engine valve sleeve making
    • Y10T29/49272Cylinder, cylinder head or engine valve sleeve making with liner, coating, or sleeve
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49936Surface interlocking
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12361All metal or with adjacent metals having aperture or cut
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12986Adjacent functionally defined components

Definitions

  • ALVIN C MCCORD, OF CHICAGO, ILLINOIS.
  • This invention relates to a method of providing cylinders of internal combustion engines with heat radiating fins or members and also to the engine cylinders so made.
  • One object of my invention is to make the heat radiating fins or members oi' a metal having a heat conductivity greater than that ofthe metal of which the cylinder is made.l and to have parts of said members extending into the cylinder wall to be close to the heat produced in the cylinder so that the heat need not traverse the full thickness oi' the cylinder wall in order to reach said members or ins,..and thus allow for a rapid and effective dissipation of heat from the cylinder.
  • Another object of my invention is to jacket the cylinder wall with a metal having a tensile strength greater than that of the metal of which the cylinder is made, and thus enable the thickness of both the jacket and the cylinder wall to be reduced to the minimum for lessening the weight oi the completed cylinder.
  • a further object of the invention is to make said jacket of a relatively non-porous metal and fit the same tight about said cylinder wall for preventing leakage therethrough and thus make possible the use of practically all cyli-nder castings.
  • a still further object of the invention is to provide said jacket with heat radiating fins or members made integral therewith.
  • a further object of the invention is to make said fins or members as well as the jacket of copper and apply the same to the engine cylinder by an electrolytic process whereby the copper is deposited on the cylinder in a manner to form the jacket and the fins.
  • Fig. l is a vertical sectional view of an engine cylinder casting provided with a plurality of holes extended therethrough in accordance with the first step of the method ot my invention
  • Fig. 2 is a like View showing a mold block applied about said cylinder for making the heat radiating fins or members and the jacket;
  • Fig. 3 is a horizontal sectional view taken on line 3--3 of Fig. 2;
  • Fig. a is a view similar to Fig. 2 and showing the jacket and heat radiating members formed on the cylinder by an electrolytic process;
  • Fig. 5 is a horizontal sectional view taken on line 5 5 of Fig. 4;
  • Fig. 6 is a side elevational view of the cylinder with jacket and members so formed, after the mold block has been removed;
  • F ig. 6 is an enlarged fragmentary vertical sectional View of a portion of the cylinder wall after the jacket and members have been deposited;
  • Figs. 7 and 8 show modifications to be hereinafter described.
  • the inner ends of the holes 2 are preferably made diamond shape, while the remaining portions of the holes 2 may be made circular in cross-section.
  • a mold block 3 made of lead or other desired material.
  • said block 3 is solid and has a length to extend the full length or' the cylinder l.
  • the inside diameter of the block 3 slightly greater than the outside diameter of the cylinder l, so that when the block 3 is placed about the same in concentric relation there is an annular space l provided between the block and the cylinder l, as shown in Fig. 2.
  • the block has depending pins in the bolt holes in the base flange of the cylinder for centering the block and holding it spaced from the cylinder wall.
  • the parts when thus assembled are clamped together in any desired way and the outer surface of the block 3 is coated with grease or other material on which copper will not deposit.
  • the open ends ot the c vlinder are plugged to close them and the inner ends ol' the holes 2 are also closed to prevent copper depositing in the bore of the cylinder.
  • the asseinblcuieut is submerged or placed in an electrolytic, hath containing copper in solution and allowed to remain in the bath until copper ⁇ by the depositing process, has filled the holes ⁇ Q, the annular space -t between the c vliuder l and the block 3, and the annular channels 5 in the block.
  • V-shapc so that copper deposited in them is given like form and thus provides on the outside ol the cylindel ⁇ wall a plurality of outwardly projecting, V-shaped, heat radiating lins or members G connected together on the outside of the cylinder by the coating l' Vformed in the space -l and constituting a jacket litting tightly about the cylinder with the parts 8 filling ⁇ the holes 2.
  • the assemblenient is removed from the bath and heat applied to the lead block 3 to melt it and cause it to run olf, leaving a copper jacket 7 about the cylinder and made fast thereto with a plurality ot' copper fins or members G on the outside thereof.
  • a copper jacket 7 about the cylinder and made fast thereto with a plurality ot' copper fins or members G on the outside thereof.
  • the heat must travel from the insidegof the cylinder to reach the heat radiating fins or members. This is further aided by having the parts 8 extend into the cylinder Wall and thus be near the zone of greatest heat so that, the heat need not travel through the full thickness ot the cylinder Wall before reaching the fins 6.
  • Fig. 7 I may make the construction as shown in Fig. 7, wherein the cylinder wall Sl is provided on its outside with a plurality ol' relatively shallow recesses 10, which terminate short of the inside or bore of the cylinder.
  • copper is deposited on the cylinder wall S) to Jorm tins 11 and a jacket l2 with parts 13 filling the recesses lo. liy having the parts 13 extended into the cylinder wall, such parts are brought nearer the bore ofthe cylinder than the jacket 12 and therefore are nearer the zone ol' greatest heat.
  • a copper jacket 14 is d'eposited about the cylinder wall 15 and at the same time integral fins 16 are formed on the jacket, as shown.
  • such parts could be cast on the cylinder wall 15 and be secured in tight contact therewith.
  • I may provide the saine with a plurality of holes 17, as shown in Fig. (3, This permits a circulation ot' air through the tins and thus enables heat to be carried ofi' with much more rapidity than is likely possible with fins having no apertures through them.
  • the cylinder wall is made ot a metal which has suitable hardness and strength for withstanding the pressure produced within it and also to stand the wear of the piston as it moves endwise o f the cylinder, and the fins which carry off the heat ol the explosions are made of a metal having a heat conductivity of a degree much greatcrthan that of the metal of which the cylinder is formed.
  • Gray iron is porous and heretofore considerable loss occurred in the manufacture ot' engine cylinders due to that fact, because the porosity of the material produced defective cylinders and made scrapping of them necessary.
  • Copper ⁇ on the other hand, is relatively non-porous. and providing a jacket of that metal about a cylinder wall, as described ⁇ prevents leakage through the cylinder wall. l ⁇ lanifestly, by the use of copper jackets, the percentage of scrappage of gray iron cylinders is greatly reduced and the cost of manufacture lessened and losses due to the porosity ot gray iron markedly overcome.
  • said jacket haviner parts extending into said cylinder wall an terminating short ofthe inner wearing surface thereof, and said jacket, members and,J parts being made of a metal of a greater heat conductivity than the metal of which the cylinder wall is made.
  • An engine cylinder having its innerV surface continuous and unbroken and constituting the wearing surface of the cylinder, a jacket tting about the outside of said cylinder, heat radiating members on said jacket and projecting outward'therefrom, said acket having parts extending into said cylinder Wall and terminating short of the inner Wearing surface thereof, and said jacket, members and parts being made integral and of a metal of a greater heat conductivity than the metal of which the cylinder Wall is made and made fast to said cylinder wall in the process of forming the same.
  • An engine cylinder having its inner surface continuons and unbroken and constituting the. wearing surface of the cylinder, a jacket fitting about the outside of said cylinder, vertically spaced, horizontal, heat radiating fins on said jacket projecting outward therefrom and extending circumferentially about the same, said jacket having parts extending into said cylinder Wall and terminatingr shoit of the inner Wearing surface thereof, and said jacket, members and parts being made integral and of a metal of greater heat conductivity than the' metal of which the cylinder wall is made and made fastfo said cylinder wall in the process of forming the same.
  • An engine cylinder provided with heat radiating members made of a metal having a heat conductivity greater than that of the metal of which thecylinder Wall is made, said members being applied to the cylinder Wall by an electrolytic process.
  • An engine cylinder having a jacket surrounding the same, heat ⁇ radiating menibers integral With said jacket and projecting outward therefrom, and said jacket and members being made of a metal having a heat conductivity greater than that of the metal of which the cylinder Wall is made and formed on said cylinder wall by an elec-- trolytic process.
  • An engine cylinder having its inner surface continuous and unbroken and constituting the Wearin surface of the cylinder, a jacket tting a out the outside of said cylinder, heat radiating members on said jacket and projecting outward therefrom', said jacket having parts extending into said cylinder Wall and terminating short of the inner Wearing surface thereof, and said jacket, members and parts being made integral and of a metal of a greater heat-conductivity than the metal of Which the cylinder Wall is made and made fast to said cylvinder Wall by an electrolytic process.
  • An engine cylinder provided with a plurality of transverse apertures, a ,jacket tting about said c vlinder, heat radiating members on said jac et and projecting out- Ward therefrom, said jacket having parts filling said apertures and terminating substantially flush with the inner surface of said cylinder, and said jacket, members and parts being made integral and of a metal of" a greater heat conductivityy than the metal of which the cylinder Wall is made and being formed on said Wall by an electrolytic process.
  • the method o providing ⁇ air-:engine cylinder with a surrounding jacket and outwardly projecting, heat radiatinfr finsof a., metal having a heat conductivity greater a therethrough, second, placing finsl andprovidin an annular s ace between the block and sai cylinder Wal third, plac.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

May 15, 1923.
A. CE MCCORD AIR` COOLED ENGINE CYLINDER AND METHOD OF MAKING SAME Filed Sept. l2 1921 .l W W w Mm f.
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JZ* ard; 739
Patented May 15, 1923.
ALVIN C. MCCORD, OF CHICAGO, ILLINOIS.
.AIR-COOLED ENGINE CYLINDER AND METHOD OF MAKING SAME.
Application led September 12, 1921. Serial No. 500,252.
To all whom t may concern Be it known that I, ALviNC. MCCORD, .a citizen ot' the United States, residing at Chicago, in the county of'ook and State of Illinois, have invented new and useful Improvements in Air-Cooled Engine A(Jylinders and Methods of Making Same, of which the following is a speciication.
This invention relates to a method of providing cylinders of internal combustion engines with heat radiating fins or members and also to the engine cylinders so made.
One object of my invention is to make the heat radiating fins or members oi' a metal having a heat conductivity greater than that ofthe metal of which the cylinder is made.l and to have parts of said members extending into the cylinder wall to be close to the heat produced in the cylinder so that the heat need not traverse the full thickness oi' the cylinder wall in order to reach said members or ins,..and thus allow for a rapid and effective dissipation of heat from the cylinder.
Another object of my invention is to jacket the cylinder wall with a metal having a tensile strength greater than that of the metal of which the cylinder is made, and thus enable the thickness of both the jacket and the cylinder wall to be reduced to the minimum for lessening the weight oi the completed cylinder.
A further object of the invention is to make said jacket of a relatively non-porous metal and fit the same tight about said cylinder wall for preventing leakage therethrough and thus make possible the use of practically all cyli-nder castings.
A still further object of the invention is to provide said jacket with heat radiating fins or members made integral therewith.
A further object of the invention is to make said fins or members as well as the jacket of copper and apply the same to the engine cylinder by an electrolytic process whereby the copper is deposited on the cylinder in a manner to form the jacket and the fins.
The invention consists further in the matters hereinafter described and more particularly set forth in the appended claims.
In the accompanying drawings- Fig. l is a vertical sectional view of an engine cylinder casting provided with a plurality of holes extended therethrough in accordance with the first step of the method ot my invention; j
Fig. 2 is a like View showing a mold block applied about said cylinder for making the heat radiating fins or members and the jacket;
Fig. 3 is a horizontal sectional view taken on line 3--3 of Fig. 2;
Fig. a is a view similar to Fig. 2 and showing the jacket and heat radiating members formed on the cylinder by an electrolytic process;
Fig. 5 is a horizontal sectional view taken on line 5 5 of Fig. 4;
Fig. 6 is a side elevational view of the cylinder with jacket and members so formed, after the mold block has been removed;
F ig. 6 is an enlarged fragmentary vertical sectional View of a portion of the cylinder wall after the jacket and members have been deposited; and
Figs. 7 and 8 show modifications to be hereinafter described.
ln carrying out the method of my invention, I take an engine cylinder casting l, as shown in Fig. l, made of gray iron, and provide it with a plurality of holes 2 extending through the cylinder wall into the bore thereof and arranged in horizontal rows, vertically spaced apart. The inner ends of the holes 2 are preferably made diamond shape, while the remaining portions of the holes 2 may be made circular in cross-section.
Placed about the cylinder 1 is a mold block 3 made of lead or other desired material. As shown herein7 said block 3 is solid and has a length to extend the full length or' the cylinder l. The inside diameter of the block 3 slightly greater than the outside diameter of the cylinder l, so that when the block 3 is placed about the same in concentric relation there is an annular space l provided between the block and the cylinder l, as shown in Fig. 2. As there illustrated, the block has depending pins in the bolt holes in the base flange of the cylinder for centering the block and holding it spaced from the cylinder wall. Provided in the block 3 are a plurality of horizontally arranged, vertically spaced, annular channels 5 opening into the inside of the block, and these are arranged in line with the horizontal rows of holes 2, as shown. The parts when thus assembled are clamped together in any desired way and the outer surface of the block 3 is coated with grease or other material on which copper will not deposit. The open ends ot the c vlinder are plugged to close them and the inner ends ol' the holes 2 are also closed to prevent copper depositing in the bore of the cylinder.
l/Vhen so arranged, the asseinblcuieut is submerged or placed in an electrolytic, hath containing copper in solution and allowed to remain in the bath until copper` by the depositing process, has filled the holes` Q, the annular space -t between the c vliuder l and the block 3, and the annular channels 5 in the block. These, as shown in the drawings, are made V-shapc so that copper deposited in them is given like form and thus provides on the outside ol the cylindel` wall a plurality of outwardly projecting, V-shaped, heat radiating lins or members G connected together on the outside of the cylinder by the coating l' Vformed in the space -l and constituting a jacket litting tightly about the cylinder with the parts 8 filling` the holes 2.
After the copper depositinghas been completed` the assemblenientis removed from the bath and heat applied to the lead block 3 to melt it and cause it to run olf, leaving a copper jacket 7 about the cylinder and made fast thereto with a plurality ot' copper fins or members G on the outside thereof. horizontally disposed and extending circumferentially about the cylinder 1, as shown in Fig. 5 and vertically 'spaced apart as shown in Fig. 6.
Internal combustion engine cylinders are usually made oi gray 'iron as this material has suflicient strength to withstand the pressures to which the cylinders are subjected when in use, and also has suiiicient hardness to provide proper working surfaces for the reciprocating pistons. rl`he tensile strength of gray iron is much less than that of copper and when a copper jacket is made fast about the cylinder wall, as above described, it is apparent that the combined tensile strength of the two metals is Jar greater than would be the tensile strength of a gray iron wall of that thickness. Consequently, by the use of a copper jacket, the thickness ot the cylinder wall may be reduced to the minimum and thus lessen the weight of the engine, yet gaining a. cylinder which will withstand the duties imposed upon it. Moreover, re-
ducing the thickness of the cylinder Wall lessens the distance. the heat must travel from the insidegof the cylinder to reach the heat radiating fins or members. This is further aided by having the parts 8 extend into the cylinder Wall and thus be near the zone of greatest heat so that, the heat need not travel through the full thickness ot the cylinder Wall before reaching the fins 6.
Instead of having the parts 8 extended through the cylinder wall into the bore as described above, I may make the construction as shown in Fig. 7, wherein the cylinder wall Sl is provided on its outside with a plurality ol' relatively shallow recesses 10, which terminate short of the inside or bore of the cylinder. Following the saine method as heretofore descrilwd, copper is deposited on the cylinder wall S) to Jorm tins 11 and a jacket l2 with parts 13 filling the recesses lo. liy having the parts 13 extended into the cylinder wall, such parts are brought nearer the bore ofthe cylinder than the jacket 12 and therefore are nearer the zone ol' greatest heat.
Instead of having copper deposited in holes or recesses as heretofore described, the construction could be made as shown in Fig. S. In this figure, a copper jacket 14 is d'eposited about the cylinder wall 15 and at the same time integral fins 16 are formed on the jacket, as shown. Instead of depositing the copper jacket 14 and its tins on the cylinder wall 1.5, such parts could be cast on the cylinder wall 15 and be secured in tight contact therewith.
As a means for enhancing or increasing the heat radiation of the fins, I may provide the saine with a plurality of holes 17, as shown in Fig. (3, This permits a circulation ot' air through the tins and thus enables heat to be carried ofi' with much more rapidity than is likely possible with fins having no apertures through them.
In all the several forms ot my invention as shown, it is to be observed that the cylinder wall is made ot a metal which has suitable hardness and strength for withstanding the pressure produced within it and also to stand the wear of the piston as it moves endwise o f the cylinder, and the fins which carry off the heat ol the explosions are made of a metal having a heat conductivity of a degree much greatcrthan that of the metal of which the cylinder is formed.
Gray iron is porous and heretofore considerable loss occurred in the manufacture ot' engine cylinders due to that fact, because the porosity of the material produced defective cylinders and made scrapping of them necessary. Copper` on the other hand, is relatively non-porous. and providing a jacket of that metal about a cylinder wall, as described` prevents leakage through the cylinder wall. l\lanifestly, by the use of copper jackets, the percentage of scrappage of gray iron cylinders is greatly reduced and the cost of manufacture lessened and losses due to the porosity ot gray iron markedly overcome.
While I have shown and described herein my method applied to one cylinder, it is ot course to be understood that it may be applied to a plurality or block of cylinders jacket and projecting outward therefrom,
said jacket haviner parts extending into said cylinder wall an terminating short ofthe inner wearing surface thereof, and said jacket, members and,J parts being made of a metal of a greater heat conductivity than the metal of which the cylinder wall is made.
2. An engine cylinder having its innerV surface continuous and unbroken and constituting the wearing surface of the cylinder, a jacket tting about the outside of said cylinder, heat radiating members on said jacket and projecting outward'therefrom, said acket having parts extending into said cylinder Wall and terminating short of the inner Wearing surface thereof, and said jacket, members and parts being made integral and of a metal of a greater heat conductivity than the metal of which the cylinder Wall is made and made fast to said cylinder wall in the process of forming the same.
3. An engine cylinder having its inner surface continuons and unbroken and constituting the. wearing surface of the cylinder, a jacket fitting about the outside of said cylinder, vertically spaced, horizontal, heat radiating fins on said jacket projecting outward therefrom and extending circumferentially about the same, said jacket having parts extending into said cylinder Wall and terminatingr shoit of the inner Wearing surface thereof, and said jacket, members and parts being made integral and of a metal of greater heat conductivity than the' metal of which the cylinder wall is made and made fastfo said cylinder wall in the process of forming the same.
4. An engine cylinder, provided with heat radiating members made of a metal having a heat conductivity greater than that of the metal of which thecylinder Wall is made, said members being applied to the cylinder Wall by an electrolytic process.
5. An engine cylinder, having a jacket surrounding the same, heat` radiating menibers integral With said jacket and projecting outward therefrom, and said jacket and members being made of a metal having a heat conductivity greater than that of the metal of which the cylinder Wall is made and formed on said cylinder wall by an elec-- trolytic process.
6. An engine cylinder having its inner surface continuous and unbroken and constituting the Wearin surface of the cylinder, a jacket tting a out the outside of said cylinder, heat radiating members on said jacket and projecting outward therefrom', said jacket having parts extending into said cylinder Wall and terminating short of the inner Wearing surface thereof, and said jacket, members and parts being made integral and of a metal of a greater heat-conductivity than the metal of Which the cylinder Wall is made and made fast to said cylvinder Wall by an electrolytic process.
j 7. An engine cylinder provided with a plurality of transverse apertures, a ,jacket tting about said c vlinder, heat radiating members on said jac et and projecting out- Ward therefrom, said jacket having parts filling said apertures and terminating substantially flush with the inner surface of said cylinder, and said jacket, members and parts being made integral and of a metal of" a greater heat conductivityy than the metal of which the cylinder Wall is made and being formed on said Wall by an electrolytic process.
8. The method of providing an engine cylinder with outwardly projecting, heat radiating members of a metal having a heat conductivity greater than that of the metal of which the cylinder Wall is made, consisting in, first, placing about the cylinder a mold block provided with cavities shaped to form said members, second, filling the cavities With a metal of Which the members are to be made by an electrolytic process, and, third, removing the block from the cylinder after 'forming said members on the cylinder. f
9. The method of providing an engine cylinder With a surrounding jacket and out- Wardly projecting, heat radiating members formed of a metal having a heat conductivity greater than that of the metal of which the-cylinder Wall is made, consisting in, first, placing about said c linder a mold block having cavities shape to form said members and providing an annual space between said block and said cylinder, second, depositing a metal of which the jacket and members are 'to be made in said cavities and space by an electrolytic process, and, third, applying heat to the block for melting it for removing the block from the cylinder.
10. rihev method of providing an engine f cylinder with a surrounding jacket and outwardly projecting, heat radiating members formed of a metal having a heat conductivity greater than that of the metal of which the cylinder Wall is made, consisting in, first, placing about said cylinder a mold block having cavities shaped to form said members and providing an annular space between said block and said cylinder, second, placing the assembled block and cylinder in an electrolytic bath containing in solution the metal of which the jacket and members are to be made and allowing the cavities in the block and said annularspace tovbeI filledby a deposit of said metal, third, removing the assembled block and cylinder from` the bath after the. metal hasA been deF positcd to form said jacket and members, and, fourth, applying heat to-the block for melting it for removing the block from the cylinder.
11.*The method o providing` air-:engine cylinder with a surrounding jacket and outwardly projecting, heat radiatinfr finsof a., metal having a heat conductivity greater a therethrough, second, placing finsl andprovidin an annular s ace between the block and sai cylinder Wal third, plac.
ing the assembled cylinderv and Vblock in an electrolytic hath vcontaining; in solution the metal ofv which the jacket and fins are to be made and. fillingsaid annular space, the
channels-in .the block, and the holes in thel cylinder wall withsuch metal, fourth, -re-` moving the assembled block vand cylinder. from the bathrafter the .metal has. been cle- Eosited, and,vv fifth, applying heat to thej lock for melting thesame for removing it from the cylinder wall.
In testimony that I claim the foregoing as my invention, I afiix my signature this 9th day of September, A. D. 1921. i
ALVIN C. MCCORD. A,
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2533533A (en) * 1946-01-08 1950-12-12 Champion Paper & Fibre Co Method of forming a strongly adherent electrodeposit
US2696570A (en) * 1951-05-23 1954-12-07 Electro Tec Corp Element of mechanism for conducting electricity between relatively movable structures
US2761828A (en) * 1954-08-16 1956-09-04 Univ Leland Stanford Junior Method of forming internally flanged structures
US2775433A (en) * 1953-08-31 1956-12-25 William F Matheny Finned tube spacing supports
US2799228A (en) * 1951-05-22 1957-07-16 Borg Warner Vaned elements and method of making the same
US3112558A (en) * 1959-03-03 1963-12-03 Baldwin Lima Hamilton Corp Finned tubing manufacture
US3474709A (en) * 1967-09-28 1969-10-28 Us Navy Cylinder liner for barrel engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2533533A (en) * 1946-01-08 1950-12-12 Champion Paper & Fibre Co Method of forming a strongly adherent electrodeposit
US2799228A (en) * 1951-05-22 1957-07-16 Borg Warner Vaned elements and method of making the same
US2696570A (en) * 1951-05-23 1954-12-07 Electro Tec Corp Element of mechanism for conducting electricity between relatively movable structures
US2775433A (en) * 1953-08-31 1956-12-25 William F Matheny Finned tube spacing supports
US2761828A (en) * 1954-08-16 1956-09-04 Univ Leland Stanford Junior Method of forming internally flanged structures
US3112558A (en) * 1959-03-03 1963-12-03 Baldwin Lima Hamilton Corp Finned tubing manufacture
US3474709A (en) * 1967-09-28 1969-10-28 Us Navy Cylinder liner for barrel engine

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