US20030037671A1 - Monobloc piston for diesel engines - Google Patents
Monobloc piston for diesel engines Download PDFInfo
- Publication number
- US20030037671A1 US20030037671A1 US09/939,195 US93919501A US2003037671A1 US 20030037671 A1 US20030037671 A1 US 20030037671A1 US 93919501 A US93919501 A US 93919501A US 2003037671 A1 US2003037671 A1 US 2003037671A1
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- United States
- Prior art keywords
- piston
- pin
- skirt
- lower edge
- pin bores
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—Pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J1/00—Pistons; Trunk pistons; Plungers
- F16J1/04—Resilient guiding parts, e.g. skirts, particularly for trunk pistons
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—Pistons
- F02F3/0015—Multi-part pistons
- F02F3/003—Multi-part pistons the parts being connected by casting, brazing, welding or clamping
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
Definitions
- This invention relates generally to monobloc pistons for diesel engine applications in which the piston skirt is formed as one integral piece with the piston body, and more particularly to the construction of the piston skirt.
- Monobloc pistons for diesel engine applications are known wherein the piston skirt is formed as an integral portion of the piston body, as opposed as being articulated.
- Such pistons are known to have piston skirts that are of such length and/or are positioned such that the lower edge of the skirt extends well below the bottom of the pin bosses to provide the desired support and guidance to the piston as it reciprocates within the cylinder of the engine.
- Such low lying skirts can extend outside of the cylinder liner at bottom dead center position of the piston and can lead to scuffing of the piston skirt and/or liner due to the sudden change in load and direction as the piston returns upwardly in the cylinder.
- the low lying skirt interferes with the location of oil injection nozzles which direct cooling oil up into the piston, requiring the skirt to be notched in the area of the nozzle to provide clearance.
- Examples of such monobloc pistons are disclosed in U.S. Pat. Nos., 4,161,165 and 4,286,505, as well as published international application WO 9620340.
- the piston disclosed in the latter publication has a short, low lying piston skirt which is uncoupled from the ring belt and, due to the wide gap between the bottom of the ring belt and the top of the skirt as well as the low, remote positioning of the skirt, transfers some of the piston guidance duties to the ring lands near the top of the piston, which is less efficient and could cause damage to the ring lands as well as decrease the performance of the piston.
- U.S. Pat. No. 4,704,950 discloses a high performance automotive piston for gasoline engines which is manufactured entirely of aluminum and would be unsuitable for high compression diesel applications to which the present invention is directed.
- a piston for diesel engines constructed according to a presently preferred embodiment of the invention comprises a piston body fabricated of steel having an outer wall and a closed oil gallery.
- a pair of pin bosses have axially aligned pin bores and a lowest tangency point of the pin bores.
- the piston body has a skirt that is formed as one piece with the pin bosses and is coupled at its upper end to the outer wall so as to form a continuous extension of the outer wall.
- the piston skirt has a lower edge spaced below the pin bore axis, but located at or above the lowest tangency point of the pin bores.
- the invention also contemplates a diesel engine which includes an engine block having at least one cylinder bore and a monobloc piston disposed in the cylinder bore having a piston body fabricated of steel and including a pair of pin bosses with aligned pin bores disposed about a pin bore axis and having a lowest tangent point to the pin bores.
- a piston skirt is formed as one piece with the pin bosses and has a lower edge disposed below the pin bore axis at or above the lowest tangent point of the pin bores.
- the invention has the advantage of providing a steel monobloc piston for diesel engine applications fitted with a short skirt made of the same steel material of such size and location relative to the remainder of the piston body to provide efficient guidance to the piston during reciprocation in the cylinder bore to reduce loading on the ring lands due to its high location relative to the pin bores.
- the high location of the lower edge of the skirt prevents the skirt from extending from the bottom of the cylinder bore at bottom dead center of the piston, and thus minimizes or eliminates scuffing of the skirt caused by a sudden change in load or direction when the piston returns upwardly.
- the relatively high location of the lower edge of the skirt also provides ample clearance for the oil jet nozzles, eliminating the need for clearance notches in the lower edge of the skirt so as to present a continuous, non-interrupted lower leading edge of the skirt which is stronger and easier to manufacture than notched skirts.
- the overall reduction and the height of the skirt further has the advantage of simplifying the manufacture of forged steel pistons.
- the shorter length enables production of a relatively thinner, more uniform thickness skirt wall as compared to forged skirts of greater length which are generally thicker due to the required draft angle to enable forging of the piston skirt.
- FIG. 1 is a bottom perspective view of a piston constructed according to the invention
- FIG. 2 is a side elevation view of the piston of FIG. 1;
- FIG. 3 is a fragmentary elevation view like FIG. 2, but shown partly in section;
- FIG. 4 is a schematic, fragmentary sectional view of a diesel engine shown equipped with the piston of FIGS. 1 - 3 .
- a piston constructed according to the invention is shown generally at 10 in FIGS. 1 - 3 and is shown installed as part of a diesel engine 12 in FIG. 4.
- the piston 10 includes a piston body 14 having a top wall 16 formed with a combustion bowl or crater 18 extending downwardly from a top surface 20 of the top wall 16 .
- the piston body 14 includes an outer annular wall or ring belt 22 having an outer surface 24 formed with a plurality of ring grooves 26 for receiving piston rings (not shown).
- the outer wall 22 includes an annular inner surface 28 facing radially inwardly of the piston body 14 opposite the outer surface 24 .
- the piston body 14 includes an annular inner wall 30 extending downwardly from the combustion bowl 18 having a radially outwardly facing annular surface 32 spaced radially inwardly from the inner surface 28 of the outer wall 22 .
- the piston body 14 preferably includes a bottom wall 34 which extends between and interconnects the lower end regions of the outer wall 22 and inner wall 30 in spaced relation to the top wall 16 .
- the top wall 16 and outer wall 22 and inner walls 30 bound an annular cooling chamber or gallery 36 for receiving cooling oil which is preferably closed at the bottom by the bottom wall 34 .
- closed it is not meant that the gallery is entirely self contained, but includes provision for openings and passages for introducing oil into and draining oil from the gallery 36 .
- a representative oil inlet opening 38 is shown in FIG. 3, as is a representative oil drainage passage 40 according to convention.
- the bottom wall 34 is formed as one piece with the lower regions of the outer wall 22 and inner wall 30 and serves, in addition to closing the gallery 36 , as a structural web or bridge between the outer and inner walls 22 , 30 .
- the piston body 14 includes a pair of pin bosses 42 .
- the pin bosses 42 are formed of one piece with the inner wall 30 and preferably extend downwardly from the bottom wall 34 and are set radially inwardly from the outer surface 24 of the outer wall 22 .
- the pin bosses 42 are formed with pin bores 44 which receive a wrist pin (not shown) for connecting the piston 10 to a connecting rod (not shown) of the engine 12 .
- the pin bores 44 are aligned about a common pin bore axis A, which represents a center line of the pin bores with respect to a longitudinal axis B of the piston body 14 .
- the pin bores 14 have a lowest tangent point 46 , which represents the lowest part of the pin bores 44 in the longitudinal direction, with the tangency point 46 determined by passing a plane P through the piston body 14 perpendicular to the longitudinal axis B which contains the lowest point of the pin bore surfaces 48 of the pin bores 44 , as illustrated in FIG. 2.
- the piston body 14 includes a piston skirt 50 that is formed as one piece with the pin bores 44 , such that the piston body 14 has a monobloc structure with a fixed skirt, rather than a separate skirt articulated to the pin bosses by the wrist pin (not shown).
- the skirt 50 is further preferably formed with an upper end region 52 coupled directly to the outer wall 22 , such that the piston skirt 50 is formed as continuous downward extension of the outer wall 22 below the bottom wall 34 .
- the piston skirt 50 is also interconnected as one piece with the bottom wall 34 , as illustrated best in FIG. 3.
- the piston skirt 50 has a lower, marginal free edge 54 which defines the lowest part of the skirt 50 in the longitudinal direction of the piston body 14 .
- the location of the lower edge 54 is such that is provides a relatively short piston skirt 50 as compared to conventional piston skirts.
- the lower edge 54 of the piston skirt 50 is disposed at a location which is below the level of the pin bore axis A but which is at or above the lowest tangent point 46 of the pin bores 44 , and more preferably above the lowest tangent point 46 .
- the lower edge 54 of the piston skirt 50 is relatively smooth and continuous and free of any clearance notches for oil nozzles or the like.
- the piston body 14 is preferably fabricated of at least two separate parts which are separately formed and then subsequently joined to one another across a joint or joints 56 .
- the piston body 14 includes an upper part 58 and a lower part 60 which, when joined together, form the enclosed cooling gallery 36 .
- the joint 56 of the preferred embodiment is preferably a friction weld joint.
- the invention contemplates other approaches to joining separately formed piston parts, such as bonding, brazing, bolting, joint threads, etc. which would operate to unite the separately formed parts as a single, unified structure once joined for service as a piston body 14 .
- the lower part 60 includes the pin bosses 42 , piston skirt 50 , bottom wall 34 , and lower portions of the outer and inner walls 24 , 30 , with the friction weld joint 56 provided in the outer and inner walls 22 , 30 .
- the lower part 60 is preferably forged from steel.
- the upper part 60 includes the top wall 16 , the bowl 18 , and upper portions of the outer walls 22 and inner wall 30 which are joined across the joint 56 to the lower portions of the outer wall 22 and inner wall 30 to unite the structure.
- FIG. 4 illustrates the piston 10 described above installed in the diesel engine 12 for reciprocation within at least one associated cylinder 62 of the engine 12 .
- the piston 14 is illustrated in its bottom dead center position, which is the lowest point that the piston 10 travels in the cylinder 62 .
- the piston skirt 50 is contained within the cylinder 62 , such that the lower edge 52 of the skirt 50 does not extend below the lower edge 64 of the cylinder 62 in which it reciprocates.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Abstract
Description
- 1. Technical Field
- This invention relates generally to monobloc pistons for diesel engine applications in which the piston skirt is formed as one integral piece with the piston body, and more particularly to the construction of the piston skirt.
- 2. Related Art
- Monobloc pistons for diesel engine applications are known wherein the piston skirt is formed as an integral portion of the piston body, as opposed as being articulated. Such pistons are known to have piston skirts that are of such length and/or are positioned such that the lower edge of the skirt extends well below the bottom of the pin bosses to provide the desired support and guidance to the piston as it reciprocates within the cylinder of the engine. Such low lying skirts, however, can extend outside of the cylinder liner at bottom dead center position of the piston and can lead to scuffing of the piston skirt and/or liner due to the sudden change in load and direction as the piston returns upwardly in the cylinder. In addition, the low lying skirt interferes with the location of oil injection nozzles which direct cooling oil up into the piston, requiring the skirt to be notched in the area of the nozzle to provide clearance. Examples of such monobloc pistons are disclosed in U.S. Pat. Nos., 4,161,165 and 4,286,505, as well as published international application WO 9620340. The piston disclosed in the latter publication has a short, low lying piston skirt which is uncoupled from the ring belt and, due to the wide gap between the bottom of the ring belt and the top of the skirt as well as the low, remote positioning of the skirt, transfers some of the piston guidance duties to the ring lands near the top of the piston, which is less efficient and could cause damage to the ring lands as well as decrease the performance of the piston.
- U.S. Pat. No. 4,704,950 discloses a high performance automotive piston for gasoline engines which is manufactured entirely of aluminum and would be unsuitable for high compression diesel applications to which the present invention is directed.
- It is an object of the present invention to provide a monobloc piston for diesel engines that overcomes or greatly minimizes the deficiencies of the prior art pistons described above.
- A piston for diesel engines constructed according to a presently preferred embodiment of the invention comprises a piston body fabricated of steel having an outer wall and a closed oil gallery. A pair of pin bosses have axially aligned pin bores and a lowest tangency point of the pin bores. The piston body has a skirt that is formed as one piece with the pin bosses and is coupled at its upper end to the outer wall so as to form a continuous extension of the outer wall. The piston skirt has a lower edge spaced below the pin bore axis, but located at or above the lowest tangency point of the pin bores.
- The invention also contemplates a diesel engine which includes an engine block having at least one cylinder bore and a monobloc piston disposed in the cylinder bore having a piston body fabricated of steel and including a pair of pin bosses with aligned pin bores disposed about a pin bore axis and having a lowest tangent point to the pin bores. A piston skirt is formed as one piece with the pin bosses and has a lower edge disposed below the pin bore axis at or above the lowest tangent point of the pin bores.
- The invention has the advantage of providing a steel monobloc piston for diesel engine applications fitted with a short skirt made of the same steel material of such size and location relative to the remainder of the piston body to provide efficient guidance to the piston during reciprocation in the cylinder bore to reduce loading on the ring lands due to its high location relative to the pin bores. The high location of the lower edge of the skirt prevents the skirt from extending from the bottom of the cylinder bore at bottom dead center of the piston, and thus minimizes or eliminates scuffing of the skirt caused by a sudden change in load or direction when the piston returns upwardly. The relatively high location of the lower edge of the skirt also provides ample clearance for the oil jet nozzles, eliminating the need for clearance notches in the lower edge of the skirt so as to present a continuous, non-interrupted lower leading edge of the skirt which is stronger and easier to manufacture than notched skirts.
- The overall reduction and the height of the skirt further has the advantage of simplifying the manufacture of forged steel pistons. The shorter length enables production of a relatively thinner, more uniform thickness skirt wall as compared to forged skirts of greater length which are generally thicker due to the required draft angle to enable forging of the piston skirt.
- These and other features and advantages of the present invention will become more readily appreciated when considered in connection with the following detailed description and appended drawings, wherein:
- FIG. 1 is a bottom perspective view of a piston constructed according to the invention;
- FIG. 2 is a side elevation view of the piston of FIG. 1;
- FIG. 3 is a fragmentary elevation view like FIG. 2, but shown partly in section; and
- FIG. 4 is a schematic, fragmentary sectional view of a diesel engine shown equipped with the piston of FIGS.1-3.
- A piston constructed according to the invention is shown generally at10 in FIGS. 1-3 and is shown installed as part of a
diesel engine 12 in FIG. 4. - The
piston 10 includes apiston body 14 having atop wall 16 formed with a combustion bowl orcrater 18 extending downwardly from atop surface 20 of thetop wall 16. - The
piston body 14 includes an outer annular wall orring belt 22 having anouter surface 24 formed with a plurality ofring grooves 26 for receiving piston rings (not shown). Theouter wall 22 includes an annularinner surface 28 facing radially inwardly of thepiston body 14 opposite theouter surface 24. - The
piston body 14 includes an annularinner wall 30 extending downwardly from thecombustion bowl 18 having a radially outwardly facingannular surface 32 spaced radially inwardly from theinner surface 28 of theouter wall 22. - The
piston body 14 preferably includes abottom wall 34 which extends between and interconnects the lower end regions of theouter wall 22 andinner wall 30 in spaced relation to thetop wall 16. Thetop wall 16 andouter wall 22 andinner walls 30 bound an annular cooling chamber orgallery 36 for receiving cooling oil which is preferably closed at the bottom by thebottom wall 34. By “closed”, it is not meant that the gallery is entirely self contained, but includes provision for openings and passages for introducing oil into and draining oil from thegallery 36. A representative oil inlet opening 38 is shown in FIG. 3, as is a representativeoil drainage passage 40 according to convention. Thebottom wall 34 is formed as one piece with the lower regions of theouter wall 22 andinner wall 30 and serves, in addition to closing thegallery 36, as a structural web or bridge between the outer andinner walls - The
piston body 14 includes a pair ofpin bosses 42. Thepin bosses 42 are formed of one piece with theinner wall 30 and preferably extend downwardly from thebottom wall 34 and are set radially inwardly from theouter surface 24 of theouter wall 22. Thepin bosses 42 are formed withpin bores 44 which receive a wrist pin (not shown) for connecting thepiston 10 to a connecting rod (not shown) of theengine 12. Thepin bores 44 are aligned about a common pin bore axis A, which represents a center line of the pin bores with respect to a longitudinal axis B of thepiston body 14. Thepin bores 14 have a lowesttangent point 46, which represents the lowest part of thepin bores 44 in the longitudinal direction, with thetangency point 46 determined by passing a plane P through thepiston body 14 perpendicular to the longitudinal axis B which contains the lowest point of thepin bore surfaces 48 of thepin bores 44, as illustrated in FIG. 2. - The
piston body 14 includes apiston skirt 50 that is formed as one piece with thepin bores 44, such that thepiston body 14 has a monobloc structure with a fixed skirt, rather than a separate skirt articulated to the pin bosses by the wrist pin (not shown). Theskirt 50 is further preferably formed with anupper end region 52 coupled directly to theouter wall 22, such that thepiston skirt 50 is formed as continuous downward extension of theouter wall 22 below thebottom wall 34. As such, thepiston skirt 50 is also interconnected as one piece with thebottom wall 34, as illustrated best in FIG. 3. - The
piston skirt 50 has a lower, marginalfree edge 54 which defines the lowest part of theskirt 50 in the longitudinal direction of thepiston body 14. According to the invention, the location of thelower edge 54 is such that is provides a relativelyshort piston skirt 50 as compared to conventional piston skirts. Particularly, thelower edge 54 of thepiston skirt 50 is disposed at a location which is below the level of the pin bore axis A but which is at or above the lowesttangent point 46 of thepin bores 44, and more preferably above the lowesttangent point 46. - In addition to the longitudinal relationship of the
lower edge 54 of thepiston skirt 50 relative to thepin bores 44, thepiston body 14 has the following dimensional ratios: H/D=0.5-0.75, A/D=0.3-0.6, and A/H=0.7-1.2, where H is the compression height of thepiston body 14 measured between thetop surface 20 of the piston body and the axis A of thepin bores 44, D equals the piston diameter and A equals the axial length between thelowest ring groove 26 and thelower edge 54 of thepiston skirt 50, as shown best in FIG. 2. - As shown best in FIGS. 1 and 2, the
lower edge 54 of thepiston skirt 50 is relatively smooth and continuous and free of any clearance notches for oil nozzles or the like. - The
piston body 14 is preferably fabricated of at least two separate parts which are separately formed and then subsequently joined to one another across a joint orjoints 56. In the illustrated embodiment, thepiston body 14 includes anupper part 58 and alower part 60 which, when joined together, form the enclosedcooling gallery 36. Thejoint 56 of the preferred embodiment is preferably a friction weld joint. However, the invention contemplates other approaches to joining separately formed piston parts, such as bonding, brazing, bolting, joint threads, etc. which would operate to unite the separately formed parts as a single, unified structure once joined for service as apiston body 14. In the present embodiment, thelower part 60 includes thepin bosses 42,piston skirt 50,bottom wall 34, and lower portions of the outer andinner walls friction weld joint 56 provided in the outer andinner walls lower part 60 is preferably forged from steel. Theupper part 60 includes thetop wall 16, thebowl 18, and upper portions of theouter walls 22 andinner wall 30 which are joined across thejoint 56 to the lower portions of theouter wall 22 andinner wall 30 to unite the structure. - FIG. 4 illustrates the
piston 10 described above installed in thediesel engine 12 for reciprocation within at least one associatedcylinder 62 of theengine 12. Thepiston 14 is illustrated in its bottom dead center position, which is the lowest point that thepiston 10 travels in thecylinder 62. It will be seen that thepiston skirt 50 is contained within thecylinder 62, such that thelower edge 52 of theskirt 50 does not extend below thelower edge 64 of thecylinder 62 in which it reciprocates. - Obviously, many modifications and variation of the present invention are possible in light of the above teachings. It is, therefore, to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described. The invention is defined by the claims.
Claims (8)
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/939,195 US6526871B1 (en) | 2001-08-24 | 2001-08-24 | Monobloc piston for diesel engines |
AT02757029T ATE365864T1 (en) | 2001-08-24 | 2002-08-08 | ONE-PIECE PISTON FOR DIESEL ENGINES |
KR10-2004-7002668A KR20040041583A (en) | 2001-08-24 | 2002-08-08 | Momobloc piston for diesel engins |
EP02757029A EP1419328B1 (en) | 2001-08-24 | 2002-08-08 | Monobloc piston for diesel engines |
JP2003523870A JP2005501197A (en) | 2001-08-24 | 2002-08-08 | Monoblock piston for diesel engine |
MXPA04001580A MXPA04001580A (en) | 2001-08-24 | 2002-08-08 | Monobloc piston for diesel engines. |
PCT/US2002/025147 WO2003019049A1 (en) | 2001-08-24 | 2002-08-08 | Monobloc piston for diesel engines |
ES02757029T ES2289129T3 (en) | 2001-08-24 | 2002-08-08 | MONOBLOCK PISTON FOR DIESEL ENGINES. |
DE60220925T DE60220925T2 (en) | 2001-08-24 | 2002-08-08 | ONE PIECE PISTON FOR DIESEL ENGINES |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/939,195 US6526871B1 (en) | 2001-08-24 | 2001-08-24 | Monobloc piston for diesel engines |
Publications (2)
Publication Number | Publication Date |
---|---|
US20030037671A1 true US20030037671A1 (en) | 2003-02-27 |
US6526871B1 US6526871B1 (en) | 2003-03-04 |
Family
ID=25472714
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/939,195 Expired - Lifetime US6526871B1 (en) | 2001-08-24 | 2001-08-24 | Monobloc piston for diesel engines |
Country Status (9)
Country | Link |
---|---|
US (1) | US6526871B1 (en) |
EP (1) | EP1419328B1 (en) |
JP (1) | JP2005501197A (en) |
KR (1) | KR20040041583A (en) |
AT (1) | ATE365864T1 (en) |
DE (1) | DE60220925T2 (en) |
ES (1) | ES2289129T3 (en) |
MX (1) | MXPA04001580A (en) |
WO (1) | WO2003019049A1 (en) |
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US20100275861A1 (en) * | 2009-05-04 | 2010-11-04 | Norbert Schneider | Piston having a central cooling gallery with a contoured flange |
US20110107997A1 (en) * | 2009-11-06 | 2011-05-12 | Florin Muscas | Steel piston with cooling gallery and method of construction thereof |
US20120037112A1 (en) * | 2009-11-06 | 2012-02-16 | Florin Muscas | Steel piston with cooling gallery and method of construction thereof |
US20140202404A1 (en) * | 2013-01-21 | 2014-07-24 | Federal-Mogul Corporation | Piston and method of making a piston |
WO2015014779A1 (en) * | 2013-07-29 | 2015-02-05 | Federal-Mogul Nürnberg GmbH | Lightweight construction of a diesel piston |
US8973484B2 (en) | 2011-07-01 | 2015-03-10 | Mahle Industries Inc. | Piston with cooling gallery |
US9108274B2 (en) * | 2011-05-05 | 2015-08-18 | Mahle International Gmbh | Method for the production of a piston |
US9856820B2 (en) | 2010-10-05 | 2018-01-02 | Mahle International Gmbh | Piston assembly |
US20180119636A1 (en) * | 2016-10-28 | 2018-05-03 | Mahle International Gmbh | Method for manufacturing a piston |
US20180369955A1 (en) * | 2017-06-27 | 2018-12-27 | Mahle International Gmbh | Method for producing a piston for an internal combustion engine consisting of a piston upper part and of a piston lower part |
US20190107076A1 (en) * | 2017-10-10 | 2019-04-11 | Lombardini S.R.L. | Piston and method of manufacturing thereof |
US11131269B2 (en) * | 2016-11-28 | 2021-09-28 | Federal-Mogul Nurnberg Gmbh | Steel piston for an internal combustion engine |
CN114856852A (en) * | 2022-05-09 | 2022-08-05 | 安徽省恒泰动力科技有限公司 | Large-cylinder-diameter air-cooled diesel engine piston |
US20220316422A1 (en) * | 2021-03-30 | 2022-10-06 | Mahle International Gmbh | Piston for an internal combustion engine and method for producing the piston |
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US6825450B2 (en) * | 2002-11-06 | 2004-11-30 | Federal-Mogul World Wide, Inc. | Piston and method of manufacture |
US7086354B2 (en) * | 2003-10-29 | 2006-08-08 | Deere & Company | Cooling nozzle mounting arrangement |
US7005620B2 (en) * | 2003-11-04 | 2006-02-28 | Federal-Mogul World Wide, Inc. | Piston and method of manufacture |
US7063049B2 (en) * | 2004-03-03 | 2006-06-20 | Deere & Company | Directed spray jet and installation tool |
US20060086326A1 (en) * | 2004-10-25 | 2006-04-27 | Ipd, Inc. | One piece cast ferrous crown piston for internal combustion engine |
US20060086325A1 (en) * | 2004-10-25 | 2006-04-27 | Ipd, Inc. | Two piece cast ferrous crown piston for internal combustion engine |
US7386105B2 (en) * | 2005-05-27 | 2008-06-10 | Nice Systems Ltd | Method and apparatus for fraud detection |
US20070074695A1 (en) * | 2005-10-04 | 2007-04-05 | Mahle Technology, Inc. | Piston having improved cooling characteristics |
US7578229B2 (en) * | 2006-12-01 | 2009-08-25 | Karl Schmidt Unisia, Inc. | Piston produced from a single forged or cast piston blank |
US7918155B2 (en) * | 2007-12-12 | 2011-04-05 | Mahle International Gmbh | Piston with a cooling gallery |
KR200453369Y1 (en) * | 2009-05-06 | 2011-05-02 | 영화테크(주) | Terminal for inserting fuse or relay |
DE102009025691A1 (en) | 2009-06-20 | 2010-01-28 | Daimler Ag | Piston for internal combustion engine, particularly reciprocating internal combustion engine, has upper piston area, which has ring carrier with ring groove and piston bowl |
DE102009056917B4 (en) * | 2009-12-03 | 2018-12-20 | Mahle International Gmbh | Method for producing a piston for an internal combustion engine |
DE102011115639A1 (en) * | 2011-09-28 | 2013-03-28 | Mahle International Gmbh | Piston for an internal combustion engine |
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DE3542800C1 (en) | 1985-12-04 | 1987-05-14 | Mahle Gmbh | Two-part plunger, especially for internal combustion engines |
USD322969S (en) | 1988-10-21 | 1992-01-07 | Caterpillar Inc. | Piston or similar article |
BR9001859A (en) | 1990-04-17 | 1991-11-12 | Metal Leve Sa | EMBOLO AND EMBOLO MANUFACTURING PROCESS |
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IT1240526B (en) | 1990-07-31 | 1993-12-17 | Borgo Nova S.P.A. | IMPROVEMENT RELATING TO PISTONS, IN GENERAL. |
DE4446726A1 (en) | 1994-12-24 | 1996-06-27 | Mahle Gmbh | Process for producing a one-piece cooling channel piston |
DE19543359C1 (en) | 1995-11-21 | 1997-07-10 | Ae Goetze Gmbh | Pistons for internal combustion engines |
BR9601835A (en) * | 1996-06-14 | 1998-09-29 | Metal Leve Sa | Internal combustion engine piston |
US6131544A (en) | 1997-06-11 | 2000-10-17 | Zakharov; Evgeny Nikolaevich | Connecting-rod and piston assembly |
US6260472B1 (en) * | 1998-07-28 | 2001-07-17 | Federal-Mogul World Wide, Inc. | One-piece integral skirt piston and method of making the same |
US5934174A (en) | 1998-10-02 | 1999-08-10 | Cummins Engine Company, Inc. | Lightweight articulated piston head and method of making the piston head |
US6112642A (en) * | 1998-10-06 | 2000-09-05 | Caterpillar Inc. | Method and apparatus for making a two piece unitary piston |
DE19846152A1 (en) * | 1998-10-07 | 2000-04-13 | Mahle Gmbh | Piston with piston base made of forged steel and a cooling channel |
US6401595B1 (en) * | 2000-10-18 | 2002-06-11 | Caterpillar Inc. | Piston for an internal combustion engine and method of assembly |
-
2001
- 2001-08-24 US US09/939,195 patent/US6526871B1/en not_active Expired - Lifetime
-
2002
- 2002-08-08 KR KR10-2004-7002668A patent/KR20040041583A/en not_active Application Discontinuation
- 2002-08-08 MX MXPA04001580A patent/MXPA04001580A/en active IP Right Grant
- 2002-08-08 ES ES02757029T patent/ES2289129T3/en not_active Expired - Lifetime
- 2002-08-08 DE DE60220925T patent/DE60220925T2/en not_active Expired - Lifetime
- 2002-08-08 WO PCT/US2002/025147 patent/WO2003019049A1/en active IP Right Grant
- 2002-08-08 JP JP2003523870A patent/JP2005501197A/en active Pending
- 2002-08-08 AT AT02757029T patent/ATE365864T1/en not_active IP Right Cessation
- 2002-08-08 EP EP02757029A patent/EP1419328B1/en not_active Expired - Lifetime
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US20100275861A1 (en) * | 2009-05-04 | 2010-11-04 | Norbert Schneider | Piston having a central cooling gallery with a contoured flange |
WO2010129388A3 (en) * | 2009-05-04 | 2011-02-24 | Federal-Mogul Corporation | Piston having a central cooling gallery with a contoured flange |
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US20110107997A1 (en) * | 2009-11-06 | 2011-05-12 | Florin Muscas | Steel piston with cooling gallery and method of construction thereof |
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Also Published As
Publication number | Publication date |
---|---|
US6526871B1 (en) | 2003-03-04 |
EP1419328B1 (en) | 2007-06-27 |
EP1419328A1 (en) | 2004-05-19 |
ATE365864T1 (en) | 2007-07-15 |
JP2005501197A (en) | 2005-01-13 |
DE60220925D1 (en) | 2007-08-09 |
DE60220925T2 (en) | 2008-02-28 |
ES2289129T3 (en) | 2008-02-01 |
KR20040041583A (en) | 2004-05-17 |
MXPA04001580A (en) | 2004-07-08 |
WO2003019049A1 (en) | 2003-03-06 |
EP1419328A4 (en) | 2005-10-19 |
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