US1763082A - Air-cooled cylinder - Google Patents

Air-cooled cylinder Download PDF

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Publication number
US1763082A
US1763082A US356241A US35624129A US1763082A US 1763082 A US1763082 A US 1763082A US 356241 A US356241 A US 356241A US 35624129 A US35624129 A US 35624129A US 1763082 A US1763082 A US 1763082A
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United States
Prior art keywords
filler
cylinder
space
liner
air
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Expired - Lifetime
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US356241A
Inventor
Charles A Bauer
Carl B Gustafson
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INDIAN MOTOCYCLE Co
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INDIAN MOTOCYCLE Co
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Priority to US356241A priority Critical patent/US1763082A/en
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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

Definitions

  • This invention relates to an improvement I 'in heat dissipating means for the cooling of internal combustion engine cylinders and the like, and more particularly cylinders which comprise a liner and shell of different metals.
  • a liquid filler furnishes a more'intimate contact with the surfaces of the cylinder members for the eflicient conduction of heat than would a solid filler.
  • the latter even if in itselfan excellent heat conductor, would not be so satisfactory since, due to the different expansion of such a solid filler material and the two cylinder members, fissures or voids would form to' considerably impair the thermal conduction.
  • Fig. 1. shows in cross-section an im roved cylinder construction according to t is invention
  • Fig. 2 is a horizontal section on line 2-2 of Fig. 1;.and
  • Fig. 3 is a fragmentary enlarged view in section of the shoulder abutting joint between the liner and shell.
  • Fig. 1 H and C indicate the head end and the crank end of the cylinder, respectively.
  • the liner which may be of iron, steel or kindred product
  • 3 is the shell having cooling ribs 4 and usually of lighter material, such as aluminum or the like, than the liner
  • 2 is a relatively narrow cylindrical space left between the liner and shell adapted to be filled up to the level 11 with a liquid filler. It will be understood that ,the space 2 will extend entirely around the cylinder and axially substantially the full length of the cylinder. Butthis space 2 is much narrower than the usual water jacket space of water cooled cylinders.
  • the liner at its head end is provided with a shoulder.
  • the space 2 between the liner and shell is to be hermetically sealed. against the ingress of air or egress of filler material.
  • the butt joint at the upper end of the cylinder will for this purpose be made air tight, and the lower joint at F can also be made both air tight and flexible by suitable mechanical means (not shown) F (such as shown in the drawings) would,
  • the lower joint F may be kept sealed at all times without the necessity of any special mechanical means, and thus simplicity and economy of construction is attained.
  • a filler which, during the operation of the engine, will be liquid in the hotter head-end ortions of the cylinder and substantially solid in the cooler crank-end portions, whereby a lower small portion of the filler acts automatically as a perfect seal for the lap joint F and the remainder of the filler acts as a good heat conducting bridge.
  • almost the entire vertical length of the filler will be liquid with its solid portion extending only a short distance from the bottom. This has been roughly indicated 1) wherein the dotted line (1. indicates the lower end of the solid portion, b the upper end of the solid portion, and c the upper end of the liquid portion of the filler.
  • the temperature distribution on the outer wall of the liner will be one of rising derees from the crank end to the head end.
  • crank end ortion is not under the direct influence of t e high temperatures of the exploding and expanding mixtures, but in close contact with the surrounding air.
  • a low melting com osition of potassium nitrate and sodium nitrate has been found tobe very suitable in motorcycle engines to meet the aforementioned requirements for the filler material. It is well known that such and similar compositions of two salts may have a very wide continuous range of freezing temperatures, varying with proortions of the constituents, the lowest reezing or so-called eutectic temperature lying far below the freezing temperatures of the constituents. By mixing the two constituents in the proper ratio, any desired freezing temperature between the eutectic and the highest constituent freezing temperature can be obtained.
  • a composition may be readily selected which will be normally solid and remain so up to the temperatures experienced at the lower end of an operating cylinder, but which liquefies at higher temperatures although it does not boil at any temperature in t e operating cylinder.
  • the filler space 2 Inasmuch as the filler space 2 is to be hermetically sealed, this space should not be completely filled with the filler material at low temperatures so as to give room for expansion thereof at the higher temperatures of operation. Also to prevent setting up of any undue pressure within the filler space due to expansion of the filler, we prefer to evacuate the air from said space to a considerable extent so that a highly rarefied condition will obtain therein. We find that a very suitable way of accomplishing these results is to introduce the filler into the filler space when in a highly heated condition, viz., at a much higher temperature than will be experienced in any operation of the cylinder. For example, the cylinder with the sealing plugs 10 removed may be immersed in a tank of the highly heated filler material so as.to completely is not, for other reasons, too far above the temperature ofthe surrounding atmosphere.
  • the inherent conductivity of the filler will be of minor importance as long as ,the distance between the walls of the liner and the shell is kept very small, as described.
  • the ease of heat transfer between two metallic walls separated by a thin layer of liquid filler is almost exclusively determined by the thermal resistance of a very thin film formed by the liquid on themetallic surfaces. Compared to the resistance of the film, the resistance of the remaining layer portions is negligible.
  • This film resistance will assume very high values in liquids that communicate with the air. Any air absorbed by the liquid forms a gaseous film on the surrounding walls of very high thermal resistance. This furnishes a still further advantage in having the filler space 2 in the present construction rarefied of air and then hermetically sealed.
  • N is our invention confined to air-cooled cylinders or cylinders of the structural details, shown in the illustrations. It may be found valuable to apply our principle to devices or apparatus outside the field of internal combustion engines. For instance, in a heating apparatus in which heat is transmitted from one body to another body Alb contained in the cylindrical by means of a wall separating these two bodies, it may be desirable to have differentmaterial body-contacting surfaces on the two sides, ofthe separating wall, and our invention would readily lend itself to the employment of such different-material contact- 1ng surfaces with excellent heat-transmitting-qualities.
  • a heat conducting wall for internal .combustion engine cylinders and the like comprising inner and outer members of different metal with an air tight space between said members containing a filler which will be liquid and not boil at the operating temperatures of said cylinder.
  • a heat conducting Wall for internal combustion engine cylinders and the like comprising inner and outer members of different metal with an air tight, air rarefied space between said members containin a filler which will be liquid and not boil at the operating temperatures of said cylinder.
  • An internal combustion engine cylinder comprising a liner of one metal and a shell of different and lighter metal with an airtight space between said members, said space containing a filler which will beliquid and not boilat the operating temperatures of said cylinder.
  • An internal combustion engine cylinder comprising a liner and a shell with a space between them and joined at their headends in fixed relation and at their crank ends in yieldable relation, and a filler contained in said space, this-filler during operation of the cylinder being liquid in the head-end port1ons and solid in the crank-end portions.
  • An internal combustion engine cylinder comprising a liner and a shell with a space etween them and joined at their head ends in fixed and hermetically sealing relation crank ends by a concentric lap joint, and a of the cylinder for hermetically sealing the yieldable join-' filler contained in the space, this filler during operation of the cylinder being liquid in the head end portions and substantially solid in the crank-end portions for hermetically sealing the lap joint.
  • An internal combustion engine cylinder comprising a liner and shell of difierent metals with a hermetically sealed space therebetween and a filler in said space consisting of an easily fusible mixturevof salts which will be liquid and not boil at operat ing temperatures of said cylinder.

Description

Patented June 10, 1930 UNITED STATES" PATIENT OFFICE Lamas-mm CHARLES A. BAUER AND CARL 1B. GUSTAFSON, OF SPRINGFIELD, MASSACHUSETTS, A3-
SIGNORS T INDIAN MOTOCYCLE COMPANY, OF
A CORPORATION OF MASSACHUSETTS SPRINGFIELD, mAssAcmIsm'rs',
AIR-COOLED CYLINDER Application filed April 18,
This invention relates to an improvement I 'in heat dissipating means for the cooling of internal combustion engine cylinders and the like, and more particularly cylinders which comprise a liner and shell of different metals.
In air cooled engines, such as for motorcycles and aircraft, the outside shells of the cylinders are frequently made of aluminum or one of its alloys in order to obtain llght weight and because such metals possess very satisfactory heat dissipating qualities,
while the liner or inside shell of such 0 linders is usually a ferrous product or wearing purposes. 1 Heretofore, various constructions of such cylinders assembled from two such separate and different ma- "terials have been attempted and no thor oughly satisfactory product has yet been at-' tained. The present improvement aims at overcoming the difliculties which have been encounteredv in' such structures.
A cylinder of two piece construction wherein the shellis of one metal and the liner of another should provide for the easy flow of heatfrom the interior to the exterior of the cylinder, and 7 one of the ,chief difiiculties heretofore met with is in securing good conduction of heat across the joint or contacting surfaces between the inner and outer members of the cylinder. Abutting contact between the metal, surfaces even under high pressure does notprovide a high degree of efiiciency for heat flow and when, as is often the case, the metals have a different coefficient of expansion, an air gap occurring between 'the surfaces will become more efficient as an insulator for heat than as a conductor therefor.
In order to secure low thermal resistance between the liner and theshell, we have found it desirable to provide a relatively narrow space, substantially cylindrical, be-
tween the two members and to fill this space with a liquid substance such as an easily fusible metal or a salt of low melting but culation of the filler within its space, which 1929. Serial No. 356,241?
in depthis made as small as is practicable and yet provide room for the different expansion of the liner and shell. A liquid filler furnishes a more'intimate contact with the surfaces of the cylinder members for the eflicient conduction of heat than would a solid filler. The latter, even if in itselfan excellent heat conductor, would not be so satisfactory since, due to the different expansion of such a solid filler material and the two cylinder members, fissures or voids would form to' considerably impair the thermal conduction. 1
In the drawings which show-a preferred-1 embodiment of our invention:
Fig. 1. shows in cross-section an im roved cylinder construction according to t is invention;
Fig. 2 is a horizontal section on line 2-2 of Fig. 1;.and
Fig. 3 is a fragmentary enlarged view in section of the shoulder abutting joint between the liner and shell.
Referring to the drawings in detail, in Fig. 1 H and C indicate the head end and the crank end of the cylinder, respectively. 1 is. the liner which may be of iron, steel or kindred product, 3 is the shell having cooling ribs 4 and usually of lighter material, such as aluminum or the like, than the liner, and 2 is a relatively narrow cylindrical space left between the liner and shell adapted to be filled up to the level 11 with a liquid filler. It will be understood that ,the space 2 will extend entirely around the cylinder and axially substantially the full length of the cylinder. Butthis space 2 is much narrower than the usual water jacket space of water cooled cylinders. It need only be wide enough to insure a clearance between the two surfaces of the'liner and Elfifill, which will be bridged by the liquid The liner and the slfell of the cylinder are subjected to different temperatures and they have besides different expansion coefficients. This is usually taken care of by a flexible joint between the two members atone of their ends. For mechanical and other rea- 7 sons, this flexible joint is preferably located while the head or upper end connection the two members may be by some sort .of
' on the drawings (Fig.
. However,
fixedjoint.
In the present embodiment, the liner at its head end is provided with a shoulder.
ortion 5 which forms a butt joint with a ange of the shell 3 at 6. Bores 9, of which several may be circumferentially disposed in the flange 8 of the shell, serve for pouring the filler in place and may be hermetically sealed after the filling procedure by plugs or other suitable means, as indicated at 10. The liner and shell are preferably joined at their lower portions b a concentric lap joint, as shown at F. his concentricdap joint permits the lower portions of the shell to freely expand or contract in axial direction. p
It is contemplated that the space 2 between the liner and shell is to be hermetically sealed. against the ingress of air or egress of filler material. The butt joint at the upper end of the cylinder will for this purpose be made air tight, and the lower joint at F can also be made both air tight and flexible by suitable mechanical means (not shown) F (such as shown in the drawings) would,
due to the unequal expanson of the materials, not remain tight under all conditions of operation. Further mechanical means, well known in the art but not here shown, would be required to keep such a joint tight.
if a filler material of proper characteristics is chosen, the lower joint F may be kept sealed at all times without the necessity of any special mechanical means, and thus simplicity and economy of construction is attained. For this purpose, we provide a filler which, during the operation of the engine, will be liquid in the hotter head-end ortions of the cylinder and substantially solid in the cooler crank-end portions, whereby a lower small portion of the filler acts automatically as a perfect seal for the lap joint F and the remainder of the filler acts as a good heat conducting bridge. In practice, almost the entire vertical length of the filler will be liquid with its solid portion extending only a short distance from the bottom. This has been roughly indicated 1) wherein the dotted line (1. indicates the lower end of the solid portion, b the upper end of the solid portion, and c the upper end of the liquid portion of the filler.
The temperature distribution on the outer wall of the liner will be one of rising derees from the crank end to the head end.
he temperature near the head end varies considerably with changing loads, while the temperature near the crank end is comparatively little variable and always lower than even the lowest head end operating temper- Ordinarily a simple lap joint When the cylinder is set in operation,
ature. This is readily explained by the fact that the crank end ortion is not under the direct influence of t e high temperatures of the exploding and expanding mixtures, but in close contact with the surrounding air.
A low melting com osition of potassium nitrate and sodium nitrate has been found tobe very suitable in motorcycle engines to meet the aforementioned requirements for the filler material. It is well known that such and similar compositions of two salts may have a very wide continuous range of freezing temperatures, varying with proortions of the constituents, the lowest reezing or so-called eutectic temperature lying far below the freezing temperatures of the constituents. By mixing the two constituents in the proper ratio, any desired freezing temperature between the eutectic and the highest constituent freezing temperature can be obtained. A composition may be readily selected which will be normally solid and remain so up to the temperatures experienced at the lower end of an operating cylinder, but which liquefies at higher temperatures although it does not boil at any temperature in t e operating cylinder.
Inasmuch as the filler space 2 is to be hermetically sealed, this space should not be completely filled with the filler material at low temperatures so as to give room for expansion thereof at the higher temperatures of operation. Also to prevent setting up of any undue pressure within the filler space due to expansion of the filler, we prefer to evacuate the air from said space to a considerable extent so that a highly rarefied condition will obtain therein. We find that a very suitable way of accomplishing these results is to introduce the filler into the filler space when in a highly heated condition, viz., at a much higher temperature than will be experienced in any operation of the cylinder. For example, the cylinder with the sealing plugs 10 removed may be immersed in a tank of the highly heated filler material so as.to completely is not, for other reasons, too far above the temperature ofthe surrounding atmosphere.
liquefaction of the head-end portions of the filler will begin, and this liquefaction will gradually proceed to the crank-end portions, the
under a l.
axial extent of the liquefied portion mainl dependin upon the load carried. But, possible operating conditions, there will always remain a broad enough solid portion near the crank end to'insure a perfect hermetic seal for the liquid portions of the filler.
expanding adjacent walls, fissures should be formed in the solid filler portion, the
liquid portion. will quickly enter and per- If, under the action of the" fectly clog the same by welding action and ensuing solidification. Thus the filler material coacts with the lap joint in providing a perfect hermetic seal.
The inherent conductivity of the filler will be of minor importance as long as ,the distance between the walls of the liner and the shell is kept very small, as described. The ease of heat transfer between two metallic walls separated by a thin layer of liquid filler is almost exclusively determined by the thermal resistance of a very thin film formed by the liquid on themetallic surfaces. Compared to the resistance of the film, the resistance of the remaining layer portions is negligible. This film resistance will assume very high values in liquids that communicate with the air. Any air absorbed by the liquid forms a gaseous film on the surrounding walls of very high thermal resistance. This furnishes a still further advantage in having the filler space 2 in the present construction rarefied of air and then hermetically sealed.
Summing up,
such as the liner and the shell, of an internal combustion cylinder, said space being occupied by a filler that becomes and remains liquid or, in other words, never boils the present invention pro-' .vides a very narrow liquid and air-tight space between two heat exchanging walls under all operating temperature conditions,
so that the filler forms a very conductive short bridge between the walls and also ideal heat contacting surfaces at all times, thereby obtaining a great ease of heat trans mission. Furthermore, by rarefying the interspace-there will never exist in it excessive pressures whlch prevents undue stresses 1n the wall materials and allows'of employing sealing means otherwise impractical. though we have mentioned eutectic salt mix tures as being particularly suitable for our purposes, we do not mean to be confined to such or similar compositions. Any sub stance or composition of matter answering the purposes as described before may be used.
N or is our invention confined to air-cooled cylinders or cylinders of the structural details, shown in the illustrations. It may be found valuable to apply our principle to devices or apparatus outside the field of internal combustion engines. For instance, in a heating apparatus in which heat is transmitted from one body to another body Alb contained in the cylindrical by means of a wall separating these two bodies, it may be desirable to have differentmaterial body-contacting surfaces on the two sides, ofthe separating wall, and our invention would readily lend itself to the employment of such different-material contact- 1ng surfaces with excellent heat-transmitting-qualities.
What we'claim is:
' 1. A heat conducting wall for internal .combustion engine cylinders and the like comprising inner and outer members of different metal with an air tight space between said members containing a filler which will be liquid and not boil at the operating temperatures of said cylinder.
2. A heat conducting Wall for internal combustion engine cylinders and the likecomprising inner and outer members of different metal with an air tight, air rarefied space between said members containin a filler which will be liquid and not boil at the operating temperatures of said cylinder.
3. An internal combustion engine cylinder comprising a liner of one metal and a shell of different and lighter metal with an airtight space between said members, said space containing a filler which will beliquid and not boilat the operating temperatures of said cylinder.
4. An internal combustion engine cylinder comprising a liner and a shell with a space between them and joined at their headends in fixed relation and at their crank ends in yieldable relation, and a filler contained in said space, this-filler during operation of the cylinder being liquid in the head-end port1ons and solid in the crank-end portions.
5.- An internal combustion engine cylinder,
comprising a liner and a shell with a substantially cylindrical narrow space between them joined at their head ends by means of a butt joint and at their crank ends by means of a concentric lap joint, and a filler space, this filler during operation of the cylinder being liquid in thehead-end portions and solid in the crank-end portions. v
6; An internal combustion engine cylinder comprising a liner and a shell with a space etween them and joined at their head ends in fixed and hermetically sealing relation crank ends by a concentric lap joint, and a of the cylinder for hermetically sealing the yieldable join-' filler contained in the space, this filler during operation of the cylinder being liquid in the head end portions and substantially solid in the crank-end portions for hermetically sealing the lap joint.
8. An internal combustion engine cylinder comprising a liner and shell of difierent metals with a hermetically sealed space therebetween and a filler in said space consisting of an easily fusible mixturevof salts which will be liquid and not boil at operat ing temperatures of said cylinder.
In testimony whereof we have afiixed our signatures. 1
' CHARLES A. BAUER.
CARL B. GUSTAFSON.
US356241A 1929-04-18 1929-04-18 Air-cooled cylinder Expired - Lifetime US1763082A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2438114A (en) * 1946-02-28 1948-03-23 Seeger Refrigerator Co Refrigerator construction
US2554921A (en) * 1948-03-01 1951-05-29 Elaine B Pobjoy Internal-combustion engine
US2696200A (en) * 1951-05-02 1954-12-07 Torre Pier Luigi System for cooling the intermediate wall of vehicle engines
US3750842A (en) * 1969-11-20 1973-08-07 H Mccaffrey Housing for an air cooled engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2438114A (en) * 1946-02-28 1948-03-23 Seeger Refrigerator Co Refrigerator construction
US2554921A (en) * 1948-03-01 1951-05-29 Elaine B Pobjoy Internal-combustion engine
US2696200A (en) * 1951-05-02 1954-12-07 Torre Pier Luigi System for cooling the intermediate wall of vehicle engines
US3750842A (en) * 1969-11-20 1973-08-07 H Mccaffrey Housing for an air cooled engine

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