US2966145A - Piston or cylinder head structure - Google Patents

Piston or cylinder head structure Download PDF

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US2966145A
US2966145A US805943A US80594359A US2966145A US 2966145 A US2966145 A US 2966145A US 805943 A US805943 A US 805943A US 80594359 A US80594359 A US 80594359A US 2966145 A US2966145 A US 2966145A
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piston
cylinder head
combustion
combustion chamber
slots
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Froehlich Kurt
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Nordberg Manufacturing Co
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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 
    • F02F1/24Cylinder heads
    • 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
    • F02F3/00Pistons 
    • F02F3/28Other pistons with specially-shaped head
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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 
    • F02F2001/008Stress problems, especially related to thermal stress

Definitions

  • the parts that make up the combustion chamber of an engine may be cracked or otherwise damaged due to excessive stresses. These stresses may be due either to the gas load or the heat load.
  • the parts that make up or define the combustion chamber must be suificiently heavy or thick to withstand the increased gas load. But this creates a heat problem since the thicker walls, sections, etc. will not transfer heat as rapidly. Since larger engines must necessarily have thicker Walls around or defining the combustion chamber, the heat stresses become especially troublesome.
  • My invention is concerned with a combustion chamber primarily for larger engines which is constructed to handle the heat stresses.
  • One purpose of the invention is a piston or cylinder head which will not crack or damage due to heat stresses formed therein.
  • Another purpose is a piston construction which will not cause the piston rings to scrape or rub unevenly against the cylinder walls.
  • Another purpose is an engine cylinder construction in which the piston or cylinder head have their opposing surfaces slotted to reduce heat stresses formed therein.
  • Another object is a combustion chamber for large engines constructed for long life.
  • Another object is a combustion chamber of the above type which provides differential thermal expansion between the inner and outer parts thereof.
  • Another object is a formation for a combustion chamher which, while it relieves thermal stresses, is nevertheless inexpensive to manufacture.
  • Figure l is a vertical section through a cylinder, der head and piston, with some parts in full;
  • Figure 2 is a partial top plan view of the piston of Figure 1;
  • Figure 3 is an enlarged elevation of a portion of the edge of the piston in Figure 1;
  • Figure 4 is a vertical section, similar to Figure 1, of a variant form.
  • a piston indicated generally at 10 reciprocates in the usual manner in a cylinder 12 and, at top dead center, defines a combustion chamber 14 with a cylinder head '16.
  • the interior of the piston, indicated generally at 18, is preferably liquid cooled although it might be otherwise.
  • the upper surface of the piston is dished somewhat as at 20 while the lower surface of the cylinder head may be correspondingly domed as at 22, so that together, they define a combustion space or chamber which is semielliptical or flattened in cross-section with the major axis or vertical dimension substantially less than its lateral dimension or diameter.
  • the shape, design and makeup of combustion chambers has received considerable attention in the past and the factors that go to make up the contouring of a combustion chamber are not, in and of themselves, important to this invention.
  • a suitable fuel supplying device shownin Figure 1, has an injector 24 for diesel fuel, sprays liquid fuel or oil into the combustion chamber from a generally centrally located position in a fan-shaped or diverging pattern, indicated generally at 26. It will be noted that the spray or jets of fuel from the injector are directed more or less at what has reference to as an annular mass 28 which, in this case, is the upper, outer edge of the piston. Note in Figure 1 that the fuel pattern is directed toward and possibly impinges against the inner surface of this mass since the mass defines a portion of the exterior of the combustion chamber.
  • the wall temperatures around the combustion chamber are higher than in the center.
  • the problem is further aggravated by the fuel pattern.
  • the spray or jets come in contact with the surface of the combustion chamber toward the outside. This causes comparatively high localized temperatures at the points of contact, since the main combustion will start and take place close to the surface of the combustion chamber in the direction of the fuel spray.
  • the exterior of the piston shown in Figure 1 will expand at a greater rate than the center, and stresses will be set up in the piston.
  • the slots are “eight such slots cylinspaced around the piston, however, the exact number is not important. There may be any number of slots as will best lit the particular application. Additionally, the slots do not have to be evenly spaced. There may be situations where it is advantageous to have the slots unevenly spaced around the circumference. As shown in the drawings,'the slots extend straight from the center toward theoutside, however, the slots may be arcuate or curved or formed in any other manner. The important thing is that the slots divide the exterior of the combustion chamber into a series of segments. The segments divide the total expansion by the number of segments and further provide an area into which the piston may expand. The bottom of the slots should follow an isothermal temperature line as closely as possible.
  • the depth of the slot be such that it will weaken the piston. If the circumferential mass or outer portion of the combustion chamber is too thin to permit sufficiently deep slots or divisions, I may nevertheless make the slots sufliciently deep to relieve the thermal stresses. Then the gas load or pressure stresses may be taken care of by reinforcing or thickening the piston along the inside under the slots, as at 36.
  • the outside of the piston may have a plurality of suitable piston ring grooves 38 formed therein. I have found that when the grooves 38 are placed near the top or combustion end of the piston when the outer portion of the piston expands the piston rings will be twisted in the piston ring grooves. The expansion of the combustion surface will cause the top of the piston to be canted outwardly toward the cylinder walls. This will cause the piston ring to unevenly rub or scrape the cylinder walls. This is an undesirable feature as it causes uneven wear on both the rings and cylinder walls and breakage of the rings.
  • FIG 4 I have shown a variant form in which the cylinder head, indicated generally at 40, has a downwardly disposed circumferential lip or shoulder. or mass 42 which extends somewhat inside of the cylinder liner 44.
  • the cylinder head forms a combustion chamber 46 with the piston 48 and a suitable fuel supplying device, such as an injection nozzle 50 may be mounted in the cylinder head at or adjacent the center thereof.
  • the upper surface 52 of the piston is truncated upwardly somewhat, instead of being dished or concave, as in Figure 1.
  • the parts define what I shall refer to as a combustion chamber which is axially flattened somewhat and extending radially and circurnferentially outwardly.
  • the mass or depending circumferential shoulder 42 forms the outer portion that defines the outside of the combustion chamber. It is in this area that the heat stresses will be set up since the spray pattern from the injector 50, shown generally at 54, will impinge or be aimed at the depending portion 42.
  • I therefore place a plurality of slots 56, each disposed radially, and spaced about the cylinder head to divide the mass into a plurality of separate or independent arcuate segments, each of which is free to independently expand and contract. But at the same time the segments combine to define a combustion chamber with the proper geometry.
  • the slots may end in an enlarged channel or opening 58 to avoid stress concentration in the bottom of the slots.
  • the number and placement of the slots is not essential. However, in preferred form the slots will be evenly spaced around the circumference of the cylinder head.
  • My invention then comprises a piston and cylinder head either of which or both may have their opposing faces or combustion surfaces radially slotted to reduce heat stresses normally formed therein. In some applications it may be desirable to only slot the piston whereas in others it may be desirable to slot the cylinder head. There-also might be applications wherein it was advantageous to slot 'boththe cylinder head and piston.
  • the stresses in the top of the piston are similar to those of a clamped plate. There are high radial stresses and relatively minute tangential stresses.
  • the radial slots of the invention provide all the advantages setforth herein on engines having a high gas load, but do not increase the radial stresses.
  • my invention is a particular form of combustion chamber or the parts or elements that go to define or make up the combustion chamber.
  • the outer portion of the combustion chamber be it a part of the piston as in Figure 1 or in the cylinder head, as in Figure 4, is subjected to the highest temperature. If the outside of the piston, for example, is substantially hotter than the central portion, the piston may pull itself apart. I sub-divide or otherwise form the outer mass or outer formation into a plurality of segments, each being free to independently expand and contract, so the inner and outer portions of therpiston are free to expand and contract on their own.
  • the mixture is ignited by a spark plug which normally is somewhat centrally located.
  • the flame starts generally at center and works its way out.
  • the annular mass such as at 28 in Figure 1, will therefore be cooler than the mixture directly next to it. Heat will therefore flow from the mixture into the mass.
  • the slots or divisions through the mass create more surface area and, accordingly, the rate of heat transfer from the mixture to the mass and through the walls of the combustion chamber will be increased. Therefore, the combustion chamber will reduce the tendency of an engine to det onate, since the rate of combustion will be slowed up.
  • An engine cylinder member having a combustion surface, said combustion surface having a raised outer edge and a generally recessed center area, said surface further having at least one radial slot formed therein.
  • An engine cylinder member having a combustion surface, said combustion surface having a plurality of radial slots formed therein, and a radial bore aligned with and forming the bottom of each of said radial slots.
  • An engine cylinder member having a combustion surface, said combustion surface having a plurality of evenly spaced radial slots formed therein, and a radial bore aligned with and forming the bottom of each of said radial slots.
  • a means for reducing heat stresses caused by uneven temperature distribution in the combustion surfaces of engine pistons including a plurality of radial slots formed in said combustion surface.
  • a means for reducing heat stresses caused by uneven temperature distribution in the combustion surface of engine pistons including a plurality of radial slots formed in said combustion surface, a radial bore aligned with and forming the bottom of each of said radial slots and having a diameter slightly greater than the width of said slots, said slots being evenly spaced around the circumference of said piston.
  • a piston including a combustion surface having a raised outer edge and a generally spherical center area, said surface having a plurality of radial slots spaced evenly therearound.
  • a piston including a combustion surface having a raised outer edge and a generally spherical center area, said surface having a plurality of radial slots, and a radial bore aligned with and forming the bottom of each of said radial slots.
  • a cylinder head including a combustion surface having a raised outer edge and a generally recessed center area, said surface having a plurality of radial slots, and a radial bore aligned with and forming the bottom of each of said radial slots.
  • a plurality of elements defining a combustion chamber and including a cylinder head and piston, the combustion chamber being somewhat flattened in an axial direction and extending circumferentially outwardly from the axis of the cylinder head and piston, at least one of the elements having an annular mass surrounding and defining an exterior portion of the combustion chamber, and a radial formation in the annular mass causing differential thermal expansion between the inner and outer portions of the said one element.
  • the structure of claim 12 further characterized in that the annular mass is divided circumferentially into a plurality of segments.
  • a plurality of elements defining a somewhat symmetrical combustion chamber which extends circumferentially outwardly from a central axis and is somewhat flattened in an axial direction, at least one of the elements having an annular, exterior mass surrounding and defining an exterior portion of the combustion chamber, the mass being divided into a plurality of circumferential segments.

Description

Dec. 27, 1960 K. FROEHLICH PISTON OR CYLINDER HEAD STRUCTURE 2 Sheets-Sheet 1 Filed April 13, 1959 I N VEN TOR. flaw/12%, 30% Zia/fer X/fowreya.
Dec. 27, 1960 K. FROEHLICH 2,966,145
PISTON OR CYLINDER HEAD STRUCTURE Filed April 15, 1959 2 Sheets-Sheet 2 IN V EN TOR.
United States Patent PISTON OR CYLINDER HEAD STRUCTURE Kurt Froehlich, Milwaukee, Wis., assignor to Nordberg Manufacturing Company, Milwaukee, Wis., a corporation of Wisconsin Filed Apr. 13, 1959, Ser. No. 805,943
Claims. (Cl. 12332) This invention is in the field of internal combustion engines and is concerned with combustion chamber construction. The invention has to do with a temperature problem and is in the nature of an improvement that reduces the stresses in or around the structure of the combustion chamber caused by temperature differentials.
The parts that make up the combustion chamber of an engine, for example the cylinder head and piston, may be cracked or otherwise damaged due to excessive stresses. These stresses may be due either to the gas load or the heat load. In what I shall refer to as larger engines, the parts that make up or define the combustion chamber must be suificiently heavy or thick to withstand the increased gas load. But this creates a heat problem since the thicker walls, sections, etc. will not transfer heat as rapidly. Since larger engines must necessarily have thicker Walls around or defining the combustion chamber, the heat stresses become especially troublesome.
My invention is concerned with a combustion chamber primarily for larger engines which is constructed to handle the heat stresses.
The problem of heat stresses gets difficult when the outside of the piston and cylinder head surfaces which cooperate to form the combustion chamber are at a higher temperature than the interior. Such a situation is usually found in diesel engines, however, any heat engine might also have the problem. If the outside of the piston or cylinder head is at a higher temperature than the interior, the outside will expand more than the interior and the piston may pull itself apart. In operation, large radial cracks may develop in either the cylinder head or the piston from the uneven expansion. This, of course, makes the head or piston unsuitable for further use. In my invention I have placed a plurality of radial slots circumferentially around the piston or cylinder head to divide it into a series of segments. When the outside of the piston or cylinder head expande due to increased heat the total expansion will be divided among the segments and the slots will provide space into which the piston or cylinder head may expand without causing distortion or damage.
One purpose of the invention is a piston or cylinder head which will not crack or damage due to heat stresses formed therein.
Another purpose is a piston construction which will not cause the piston rings to scrape or rub unevenly against the cylinder walls.
Another purpose is an engine cylinder construction in which the piston or cylinder head have their opposing surfaces slotted to reduce heat stresses formed therein.
Another object is a combustion chamber that will slow down the fuelburning rate in gas engines and speed it up in oil or diesel engines.
Another object is a combustion chamber for large engines constructed for long life.
Another object is a combustion chamber of the above type which provides differential thermal expansion between the inner and outer parts thereof.
' Another object is a formation for a combustion chamher which, while it relieves thermal stresses, is nevertheless inexpensive to manufacture.
Other purposes will appear in the ensuing specification and drawings and claims.
The invention is illustrated diagrammatically in the following drawings wherein:
Figure l is a vertical section through a cylinder, der head and piston, with some parts in full;
Figure 2 is a partial top plan view of the piston of Figure 1;
Figure 3 is an enlarged elevation of a portion of the edge of the piston in Figure 1; and
Figure 4 is a vertical section, similar to Figure 1, of a variant form.
In Figure l a piston indicated generally at 10 reciprocates in the usual manner in a cylinder 12 and, at top dead center, defines a combustion chamber 14 with a cylinder head '16. The interior of the piston, indicated generally at 18, is preferably liquid cooled although it might be otherwise.
The upper surface of the piston is dished somewhat as at 20 while the lower surface of the cylinder head may be correspondingly domed as at 22, so that together, they define a combustion space or chamber which is semielliptical or flattened in cross-section with the major axis or vertical dimension substantially less than its lateral dimension or diameter. The shape, design and makeup of combustion chambers has received considerable attention in the past and the factors that go to make up the contouring of a combustion chamber are not, in and of themselves, important to this invention.
A suitable fuel supplying device, shownin Figure 1, has an injector 24 for diesel fuel, sprays liquid fuel or oil into the combustion chamber from a generally centrally located position in a fan-shaped or diverging pattern, indicated generally at 26. It will be noted that the spray or jets of fuel from the injector are directed more or less at what has reference to as an annular mass 28 which, in this case, is the upper, outer edge of the piston. Note in Figure 1 that the fuel pattern is directed toward and possibly impinges against the inner surface of this mass since the mass defines a portion of the exterior of the combustion chamber.
Because of the limited amount of cooling surface at the outside edges of the combustion chamber in relation to the heating surface, the wall temperatures around the combustion chamber are higher than in the center. In addition, the problem is further aggravated by the fuel pattern. For example, in diesel engines where the fuel is injected in a pattern something along the lines of that shown in Figure l, the spray or jets come in contact with the surface of the combustion chamber toward the outside. This causes comparatively high localized temperatures at the points of contact, since the main combustion will start and take place close to the surface of the combustion chamber in the direction of the fuel spray. The exterior of the piston shown in Figure 1 will expand at a greater rate than the center, and stresses will be set up in the piston. These heat stresses may cause the piston to crack or to be otherwise damaged and so make the piston unsuitable for use. In order to alleviate the heat stresses, I have placed a plurality of radial slots 30 circumferentially around the piston thereby dividing the annular mass 28 into a number of separate circumferential segments. Each of the radial slots opens into and is aligned with a radial bore 32. The bores 32 open into the general center of the piston as at 34. The diameter of the radial bore 32 is greater than the width of the slots 30, as shown in Figure 3. By placing the bore at the bottom of the slot I remove any stress concentration which would normally be present at the bottom.
As shown in the drawings there are "eight such slots cylinspaced around the piston, however, the exact number is not important. There may be any number of slots as will best lit the particular application. Additionally, the slots do not have to be evenly spaced. There may be situations where it is advantageous to have the slots unevenly spaced around the circumference. As shown in the drawings,'the slots extend straight from the center toward theoutside, however, the slots may be arcuate or curved or formed in any other manner. The important thing is that the slots divide the exterior of the combustion chamber into a series of segments. The segments divide the total expansion by the number of segments and further provide an area into which the piston may expand. The bottom of the slots should follow an isothermal temperature line as closely as possible. However, in no case should the depth of the slot be such that it will weaken the piston. If the circumferential mass or outer portion of the combustion chamber is too thin to permit sufficiently deep slots or divisions, I may nevertheless make the slots sufliciently deep to relieve the thermal stresses. Then the gas load or pressure stresses may be taken care of by reinforcing or thickening the piston along the inside under the slots, as at 36.
The outside of the piston may have a plurality of suitable piston ring grooves 38 formed therein. I have found that when the grooves 38 are placed near the top or combustion end of the piston when the outer portion of the piston expands the piston rings will be twisted in the piston ring grooves. The expansion of the combustion surface will cause the top of the piston to be canted outwardly toward the cylinder walls. This will cause the piston ring to unevenly rub or scrape the cylinder walls. This is an undesirable feature as it causes uneven wear on both the rings and cylinder walls and breakage of the rings.
In Figure 4, I have shown a variant form in which the cylinder head, indicated generally at 40, has a downwardly disposed circumferential lip or shoulder. or mass 42 which extends somewhat inside of the cylinder liner 44. The cylinder head forms a combustion chamber 46 with the piston 48 and a suitable fuel supplying device, such as an injection nozzle 50 may be mounted in the cylinder head at or adjacent the center thereof.
It will be noted in this case that the upper surface 52 of the piston is truncated upwardly somewhat, instead of being dished or concave, as in Figure 1. But nevertheless the parts define what I shall refer to as a combustion chamber which is axially flattened somewhat and extending radially and circurnferentially outwardly. In this case the mass or depending circumferential shoulder 42 forms the outer portion that defines the outside of the combustion chamber. It is in this area that the heat stresses will be set up since the spray pattern from the injector 50, shown generally at 54, will impinge or be aimed at the depending portion 42.
I therefore place a plurality of slots 56, each disposed radially, and spaced about the cylinder head to divide the mass into a plurality of separate or independent arcuate segments, each of which is free to independently expand and contract. But at the same time the segments combine to define a combustion chamber with the proper geometry. As before, the slots may end in an enlarged channel or opening 58 to avoid stress concentration in the bottom of the slots. As was also true in the piston the number and placement of the slots is not essential. However, in preferred form the slots will be evenly spaced around the circumference of the cylinder head.
My invention then comprises a piston and cylinder head either of which or both may have their opposing faces or combustion surfaces radially slotted to reduce heat stresses normally formed therein. In some applications it may be desirable to only slot the piston whereas in others it may be desirable to slot the cylinder head. There-also might be applications wherein it was advantageous to slot 'boththe cylinder head and piston.
The use, operation and function of my invention is as follows:
Shown and described herein is a means for reducing heat stresses normally formed in the combustion surfaces of cylinder members. The particular construction shown could be applicable to a diesel engine, however, there are numerous other types of engines to which the construction is equally applicable. .In a diesel engine cylinder the interior of the piston and cylinder head combustion surfaces are at a lower temperature than the outside. This causes heat stresses to be formed in the cylinder head and piston which in turn may cause distortion or cracking of these-members after short use. By slotting the opposed surfaces or combustion surfaces of the cylinder head and piston I have reduced the amount of expansion and have provided an area into which these members may expand.
When the piston has a depending skirt, such as shown in the drawings, the stresses in the top of the piston are similar to those of a clamped plate. There are high radial stresses and relatively minute tangential stresses. The radial slots of the invention provide all the advantages setforth herein on engines having a high gas load, but do not increase the radial stresses.
I have placed a radial bore in alignment with each slot at the bottom thereof to reduce the stress concentration which is normally formed at the bottom of a slot. The particular depth of the slot is not important, however generally the bottom should follow an isothermal temperature line. It should be understood that neither the piston nor cylinder head should be slotted to a depth which would materially reduce the strength of these members. It is important that the strength not be reduced below load requirement as by so doing any advantage secured by slotting these members would be lost.
Another cause of damage in cylinders is the uneven rubbing of the piston rings on the wall of the cylinder. This is caused by the fact that the rings closest to the combustion surface of the piston will be flexed or bent outward due to the expansion of the combustion surface. These rings then will rub on the cylinder wall more than the rings further away from the combustion surface. The uneven rubbing of the piston rings will damage 'both the cylinder wall and the piston rings. By reducing the expansion I have all but eliminated this problem.
In a sense my invention is a particular form of combustion chamber or the parts or elements that go to define or make up the combustion chamber. The outer portion of the combustion chamber, be it a part of the piston as in Figure 1 or in the cylinder head, as in Figure 4, is subjected to the highest temperature. If the outside of the piston, for example, is substantially hotter than the central portion, the piston may pull itself apart. I sub-divide or otherwise form the outer mass or outer formation into a plurality of segments, each being free to independently expand and contract, so the inner and outer portions of therpiston are free to expand and contract on their own.
This arrangement has advantage in both a diesel or oil and a gas engine. For example, in a diesel engine it is well known that the rate of combustion or fuel burning is too slow, and engineers are always seeking ways and means to speed it .up. In Figure l, the annular mass 28 will be hotter than the jets or spray 26 while moving out toward it. Burning starts on the outside of the spray of fuel and works in toward the center. Heat will therefore flow from the annular mass 28 to the spray and will speed up the rate of combustion. But at the same time, the mass will not pull the piston apart since the load segments expand and contract on their own, The result is a combustion chamber that will speed up the rate of combustion but will .not pull itself apart.
Ina gas engine, the situation is somewhat reversed.
The mixture is ignited by a spark plug which normally is somewhat centrally located. The flame starts generally at center and works its way out. The annular mass, such as at 28 in Figure 1, will therefore be cooler than the mixture directly next to it. Heat will therefore flow from the mixture into the mass. The slots or divisions through the mass create more surface area and, accordingly, the rate of heat transfer from the mixture to the mass and through the walls of the combustion chamber will be increased. Therefore, the combustion chamber will reduce the tendency of an engine to det onate, since the rate of combustion will be slowed up.
The invention is not limited to the specific details of construction described and illustrated in the accompanying drawings, but covers all modifications coming within the scope of the following claims.
I claim:
1. An engine cylinder member having a combustion surface, said combustion surface having a raised outer edge and a generally recessed center area, said surface further having at least one radial slot formed therein.
2. An engine cylinder member having a combustion surface, said combustion surface having a plurality of radial slots formed therein, and a radial bore aligned with and forming the bottom of each of said radial slots.
3. An engine cylinder member having a combustion surface, said combustion surface having a plurality of evenly spaced radial slots formed therein, and a radial bore aligned with and forming the bottom of each of said radial slots.
4. A means for reducing heat stresses caused by uneven temperature distribution in the combustion surfaces of engine pistons including a plurality of radial slots formed in said combustion surface.
5. A means for reducing heat stresses caused by uneven temperature distribution in the combustion surface of engine pistons including a plurality of radial slots formed in said combustion surface, a radial bore aligned with and forming the bottom of each of said radial slots and having a diameter slightly greater than the width of said slots, said slots being evenly spaced around the circumference of said piston.
6. A piston including a combustion surface having a raised outer edge and a generally spherical center area, said surface having a plurality of radial slots spaced evenly therearound.
7. A piston including a combustion surface having a raised outer edge and a generally spherical center area, said surface having a plurality of radial slots, and a radial bore aligned with and forming the bottom of each of said radial slots.
8. The structure of claim 7 in which the diameter of the bore is greater than the width of the slot.
9. A cylinder head including a combustion surface having a raised outer edge and a generally recessed center area, said surface having a plurality of radial slots spaced evenly therearound.
10. A cylinder head including a combustion surface having a raised outer edge and a generally recessed center area, said surface having a plurality of radial slots, and a radial bore aligned with and forming the bottom of each of said radial slots.
11. The structure of claim 10 in which the diameter of the bore is greater than the width of the slot.
12. 'For use in an engine, a plurality of elements defining a combustion chamber and including a cylinder head and piston, the combustion chamber being somewhat flattened in an axial direction and extending circumferentially outwardly from the axis of the cylinder head and piston, at least one of the elements having an annular mass surrounding and defining an exterior portion of the combustion chamber, and a radial formation in the annular mass causing differential thermal expansion between the inner and outer portions of the said one element.
13. The structure of claim 12 further characterized in that the annular mass is divided circumferentially into a plurality of segments.
14. The structure of claim 13 in which all of the seg ments are approximately equal in circumferential extent.
15. For use in an engine, a plurality of elements defining a somewhat symmetrical combustion chamber which extends circumferentially outwardly from a central axis and is somewhat flattened in an axial direction, at least one of the elements having an annular, exterior mass surrounding and defining an exterior portion of the combustion chamber, the mass being divided into a plurality of circumferential segments.
References Cited in the file of this patent UNITED STATES PATENTS 1,320,064 Junkers Oct. 28, 1919 1,745,884 Barnaby Feb. 4, 1930 2,791,989 Dickson May 14, 1957
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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1272630B (en) * 1961-09-20 1968-07-11 Alcan Aluminiumwerke Piston with high thermal and mechanical loads
US4445467A (en) * 1982-08-10 1984-05-01 Howard Westerman Two-cycle stratified charge gas engine
EP0159429B1 (en) * 1982-08-10 1988-06-15 Howard G. Westerman Two-cycle stratified charge gas engine
US4898135A (en) * 1989-02-16 1990-02-06 Sonex Research, Inc. Piston and process for achieving controlled ignition and combustion of hydrocarbon fuels in internal combustion engines by generation and management of fuel radical species
US5322042A (en) * 1992-06-17 1994-06-21 Sonex Research, Inc. Combustion chamber for internal combustion engine and process of combustion using fuel radical species
US5544627A (en) * 1995-03-21 1996-08-13 Terziev; Nicola Engine design for gasoline/diesel engines
US6016739A (en) * 1995-06-07 2000-01-25 Sundstrand Corporation Piston and method for reducing wear
US6502540B1 (en) 1999-01-19 2003-01-07 Alvin J. Smith Internal combustion engine gas flow control
US6606970B2 (en) * 1999-08-31 2003-08-19 Richard Patton Adiabatic internal combustion engine with regenerator and hot air ignition
US6647950B2 (en) * 2000-05-10 2003-11-18 Bombardier Motor Corporation America Fuel-injected internal combustion engine with reduced squish factor
US20120037118A1 (en) * 2010-08-12 2012-02-16 C.R.F. Societa Consortile Per Azioni Combustion Chamber for Diesel Engines with Inclined Engine Valves
US20120107144A1 (en) * 2010-10-29 2012-05-03 Keifer Eric G Variable bore convertible compressor cylinder

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1320064A (en) * 1919-10-28 Piston eob
US1745884A (en) * 1927-12-30 1930-02-04 Worthington Pump & Mach Corp Internal-combustion engine
US2791989A (en) * 1954-09-29 1957-05-14 Gen Motors Corp Internal-combustion engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1320064A (en) * 1919-10-28 Piston eob
US1745884A (en) * 1927-12-30 1930-02-04 Worthington Pump & Mach Corp Internal-combustion engine
US2791989A (en) * 1954-09-29 1957-05-14 Gen Motors Corp Internal-combustion engine

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1272630B (en) * 1961-09-20 1968-07-11 Alcan Aluminiumwerke Piston with high thermal and mechanical loads
US4445467A (en) * 1982-08-10 1984-05-01 Howard Westerman Two-cycle stratified charge gas engine
EP0159429B1 (en) * 1982-08-10 1988-06-15 Howard G. Westerman Two-cycle stratified charge gas engine
US4898135A (en) * 1989-02-16 1990-02-06 Sonex Research, Inc. Piston and process for achieving controlled ignition and combustion of hydrocarbon fuels in internal combustion engines by generation and management of fuel radical species
US5322042A (en) * 1992-06-17 1994-06-21 Sonex Research, Inc. Combustion chamber for internal combustion engine and process of combustion using fuel radical species
US5544627A (en) * 1995-03-21 1996-08-13 Terziev; Nicola Engine design for gasoline/diesel engines
US6016739A (en) * 1995-06-07 2000-01-25 Sundstrand Corporation Piston and method for reducing wear
US6502540B1 (en) 1999-01-19 2003-01-07 Alvin J. Smith Internal combustion engine gas flow control
US6606970B2 (en) * 1999-08-31 2003-08-19 Richard Patton Adiabatic internal combustion engine with regenerator and hot air ignition
US6647950B2 (en) * 2000-05-10 2003-11-18 Bombardier Motor Corporation America Fuel-injected internal combustion engine with reduced squish factor
US20120037118A1 (en) * 2010-08-12 2012-02-16 C.R.F. Societa Consortile Per Azioni Combustion Chamber for Diesel Engines with Inclined Engine Valves
US9074519B2 (en) * 2010-08-12 2015-07-07 C.R.F. Società Consortile Per Azioni Combustion chamber for diesel engines with inclined engine valves
US20120107144A1 (en) * 2010-10-29 2012-05-03 Keifer Eric G Variable bore convertible compressor cylinder

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