WO2013119909A1 - Piston with enhanced cooling gallery - Google Patents
Piston with enhanced cooling gallery Download PDFInfo
- Publication number
- WO2013119909A1 WO2013119909A1 PCT/US2013/025283 US2013025283W WO2013119909A1 WO 2013119909 A1 WO2013119909 A1 WO 2013119909A1 US 2013025283 W US2013025283 W US 2013025283W WO 2013119909 A1 WO2013119909 A1 WO 2013119909A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- piston
- ring groove
- uppermost
- ring
- cooling gallery
- Prior art date
Links
Classifications
-
- 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
- F02F3/16—Pistons having cooling means
- F02F3/20—Pistons having cooling means the means being a fluid flowing through or along piston
- F02F3/22—Pistons having cooling means the means being a fluid flowing through or along piston the fluid being liquid
-
- 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
- F16J1/09—Pistons; Trunk pistons; Plungers with means for guiding fluids
-
- 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
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/02—L-section rings
-
- 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
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/12—Details
- F16J9/22—Rings for preventing wear of grooves or like seatings
Definitions
- This invention relates generally to internal combustion engines, and more particularly to pistons therefor.
- a piston constructed in accordance with this invention is able to better withstand the excessive heat generated in modern high performance engines, as will become apparent to those skilled in the art upon reading the disclosure and viewing the drawings herein.
- a piston for an internal combustion engine includes a body having a cylindrical outer surface with an annular uppermost ring groove and a lower ring groove extending into the outer surface.
- a top land extends from the uppermost ring groove to an upper combustion surface.
- the body has a pair of pin bosses with pin bores aligned with one another along a pin bore axis.
- a first piston ring is disposed in the uppermost ring groove and a second piston ring is disposed in the lower ring groove.
- the body has an annular sealed cooling gallery with a cooling medium contained therein.
- the sealed cooling gallery is configured in substantial radial alignment between the first and second piston rings.
- the sealed cooling chamber is configured to optimize the cooling effect of the coolant medium contained therein on the upper combustion surface and the ring belt region. Accordingly, the piston is able to attain an enhanced useful life.
- Figure 1 is a cross-sectional view taken generally transverse to a pin bore axis of a piston constructed in accordance with one aspect of the invention
- Figure 2 is a cross-section view of the piston of Figure 1 taken generally along the pin bore axis;
- Figure 3 is a cross-sectional view taken generally transverse to a pin bore axis of a piston constructed in accordance with another aspect of the invention.
- Figures 1 and 2 illustrate a cross- sectional view of a piston 10 constructed in accordance with one presently preferred aspect of the invention for reciprocating movement in a cylinder bore of an internal combustion engine, such as a modern, compact, high performance vehicle engine, for example.
- the piston 10 has a body 12, such as a single, monolithic piece of cast material or formed from either forged or billet materials, by way of example and without limitation, extending along a central longitudinal axis 13 along which the piston 10 reciprocates in the cylinder bore.
- the body 12 has an upper combustion wall 14 having on one side an upper combustion surface 16 configured for direct exposure to combustion gases within a cylinder bore and on an opposite side an undercrown surface 18 located axially beneath a portion of the upper combustion surface 16.
- the piston body 12 also includes a generally cylindrical outer wall 20 having a cylindrical outer surface 21 depending from the upper combustion surface 16 over a ring belt region 22 immediately adjacent the upper combustion surface 16.
- the ring belt region 22 includes an uppermost ring groove 23 and a lower ring groove, shown as a lowermost ring groove 24.
- Each of the ring grooves 23, 24 are configured for receipt of first and second piston rings 26, 27 therein, respectively.
- the piston body 12 is formed having a closed cooling gallery 28 with a cooling medium 30 disposed and contained therein.
- the cooling gallery 28 is configured radially inwardly and in substantial radial alignment with the ring belt region 22.
- the cooling gallery 28 is configured in accordance with the invention to enhance the transfer of heat from the upper combustion surface 16 and ring belt region 22 to the cylinder liner and engine block. Accordingly, heat generated within the upper combustion wall 14 and ring belt region 22 is ultimately transferred to the cylinder liner and engine block, thereby facilitating reduction of the operating temperature of the piston 10, and thus, enhancing the useful life of the piston 10.
- the cooling medium 30 can be provided entirely as a metallic coolant, which is liquid at operating temperature of the piston 10. Any suitable lightweight metallic material could be used, taking into account the heat transfer coefficient desired. Further, the cooling medium 30 can be provided as a liquid metal mixed with powdered metal, such as copper or aluminum. The addition of metallic powder can be used particularly when it is desired to raise the heat transfer properties of the cooling medium 30. Further yet, heat transfer liquids, such as those typically used for industrial heat exchanging, can be used.
- the piston body 12 has a pair of pin bosses 32 depending from the undercrown surface 18 to provide laterally spaced pin bores 34 coaxially aligned along a pin bore axis 36 that extends generally transverse to the central longitudinal axis 13.
- the pin bosses 32 are joined to laterally spaced skirt portions 38 that are diametrically spaced from one another across opposite sides the pin bore axis 36 and have convex outer surfaces 40 contoured for sliding movement within the cylinder bore to facilitate maintaining the piston 10 in its desired orientation as it reciprocates within the cylinder bore.
- the upper combustion surface 16 is represented as having a recessed combustion bowl 42 depending from a planar uppermost portion of the upper combustion surface 16 to a lowermost annular valley 43 extending about a raised central peak 45 to provide a desired gas flow within the cylinder bore. At least in part due to the combustion bowl 42, relatively thin regions of piston body material are formed between the combustion bowl 42, the cooling gallery 28 and the undercrown surface 18.
- the outer wall 20 is shown as extending downwardly from the upper combustion surface 16 having a diameter Dl that is reduced from a maximum diameter D2 of the ring belt region 22, which depends from an upper land region 44.
- an annular gap or space 46 is provided for receipt of a first portion 48 of the generally L-shaped first piston ring 26 between the outer surface 21 and the cylinder liner.
- the diameter Dl is sized so that the first portion 48 of the piston ring 26 is free to float between the upper land region 44 and the cylinder liner, thereby being able to automatically find its desired sliding orientation.
- the annular ring groove 23 extends radially inwardly into the reduced diameter outer wall 20 of the upper land region 44, wherein the ring groove 23 is sized for receipt of a laterally extending second portion 50 of the generally L-shaped first piston ring 26.
- the ring groove 23 is sized so that the second portion 50 of the first piston ring 26 is free to float therein, thereby further allowing the piston ring 26 to automatically find its desired sliding orientation during reciprocating movement of the piston 10.
- the first portion 48 provides the upstanding or vertically extending leg of the L-shaped configuration and the second portion 50 provides the laterally or horizontally extending leg of the L-shaped configuration. As discussed above, the first portion 48 is received in the annular space 46 and the second portion 50 is received in the ring groove 23.
- the second piston ring 27 is spaced axially downwardly from the first piston ring 26, and is represented as a wiper ring to facilitate wiping oil from the liner back to the crankcase.
- the outer surface 21 extending between the first and second piston rings 26, 27 is continuous and uninterrupted, thus, being free of any ring grooves between the uppermost ring groove 23 and lower ring groove, shown as being a lowermost ring groove 24. Accordingly, the piston 10 has only the two ring grooves 23, 24 and correspondingly piston rings 26, 27. It is to be understood that the concept discussed herein also covers the traditional 3 ring piston package, 2 rings being the preferred embodiment.
- the cooling gallery 28 extends between the ring grooves 23, 24, thereby facilitating cooling of the entire ring belt region 22 as well as the portion valley region 43 of the combustion bowl 42 and the uppermost planar region of the upper combustion surface 16.
- the cooling gallery 28 extends upwardly to an uppermost peak or surface 52 and downwardly to a lowermost valley or surface 54.
- the uppermost surface 52 is shown as being radially aligned with a planar lowermost surface 55 of the uppermost ring groove 23 and the lowermost surface 54 is shown as being radially aliged with an uppermost planar surface 56 of the lower ring groove 24.
- FIG. 3 illustrates a cross-sectional view of a piston 1 10 constructed in accordance with one presently preferred aspect of the invention, wherein the same reference numerals as above, offset by a factor of 100, are used to identify like features discussed above.
- the piston 1 10 has a body 1 12, an upper combustion wall 1 14 having an upper combustion surface 1 16 and an undercrown surface 1 18, as discussed above.
- the piston body 1 12 also includes a generally cylindrical outer wall 120 having a cylindrical outer surface 121 depending from the upper combustion surface 1 16 over a ring belt region 122.
- the ring belt region 122 includes an uppermost ring groove 123 and a lower ring groove, shown as a lowermost ring groove 124.
- Each of the ring grooves 123, 124 are configured for receipt of first and second piston rings 126, 127 therein, respectively.
- the piston body 12 has a closed cooling gallery 128 with a cooling medium 130 disposed and contained therein.
- the cooling gallery 128 is configured radially inwardly and in substantial radial alignment with the ring belt region 122.
- the upper most ring groove 123 is configured as discussed above, however, the lowermost ring groove 123 is moved axially upwardly, such that a relatively thin annular flange 60 of piston body material having a thickness approximately the thickness of the second piston ring 127 is formed between the ring grooves 123, 124. Accordingly, the ring belt region 122 has a reduced axial length in comparison with the ring belt region 22.
- the combustion bowl 142 has a full concave surface, and thus, does not have a central peak.
- the cooling gallery 128, as with the first embodiment extends upwardly to an uppermost peak or surface 152 and downwardly to a lowermost surface 154, wherein the uppermost surface 152 is shown as being radially aligned with a planar lowermost surface 1 5 of the uppermost ring groove 123.
- the lowermost surface 154 is shown as extending below a lowermost planar surface 62 of the lower ring groove 124. Accordingly, the cooling gallery 128 extends across the full axial width of the lowermost piston ring groove 124.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BR112014019774A BR112014019774A8 (en) | 2012-02-10 | 2013-02-08 | PISTON WITH IMPROVED COOLING GALLERY |
JP2014556707A JP2015511290A (en) | 2012-02-10 | 2013-02-08 | Piston with improved cooling cavity |
CN201380018416.XA CN104204487B (en) | 2012-02-10 | 2013-02-08 | Piston with enhancing cooling duct |
EP13705889.7A EP2812553B1 (en) | 2012-02-10 | 2013-02-08 | Piston with enhanced cooling gallery |
KR1020147023873A KR102080359B1 (en) | 2012-02-10 | 2013-02-08 | Piston with enhanced cooling gallery |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/370,645 US10753310B2 (en) | 2012-02-10 | 2012-02-10 | Piston with enhanced cooling gallery |
US13/370,645 | 2012-02-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2013119909A1 true WO2013119909A1 (en) | 2013-08-15 |
Family
ID=47748784
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2013/025283 WO2013119909A1 (en) | 2012-02-10 | 2013-02-08 | Piston with enhanced cooling gallery |
Country Status (7)
Country | Link |
---|---|
US (1) | US10753310B2 (en) |
EP (1) | EP2812553B1 (en) |
JP (2) | JP2015511290A (en) |
KR (1) | KR102080359B1 (en) |
CN (1) | CN104204487B (en) |
BR (1) | BR112014019774A8 (en) |
WO (1) | WO2013119909A1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8544441B2 (en) * | 2011-08-04 | 2013-10-01 | Federal-Mogul Ignition Company | Piston including a pair of cooling chambers |
US20130213341A1 (en) * | 2012-02-16 | 2013-08-22 | Teoman Uzkan | Engine having piston with l-shaped timing ring |
JP6392221B2 (en) * | 2012-07-20 | 2018-09-19 | フェデラル−モーグル・リミテッド・ライアビリティ・カンパニーFederal−Mogul Llc | Piston having oil-cooled passage and method for constructing the same |
DE102013009155A1 (en) * | 2013-05-31 | 2014-12-04 | Mahle International Gmbh | Piston for an internal combustion engine |
US10202936B2 (en) | 2015-04-09 | 2019-02-12 | Tenneco Inc. | Zero oil cooled (ZOC) piston incorporating heat pipe technology |
CN106801647A (en) * | 2017-01-25 | 2017-06-06 | 日照金港活塞有限公司 | One kind closing cooling chamber piston |
US10724516B2 (en) * | 2017-06-13 | 2020-07-28 | Forum Us, Inc. | Reciprocating piston |
US10731598B2 (en) | 2018-10-18 | 2020-08-04 | Tenneco Inc. | Piston having an undercrown surface with coating and method of manufacture thereof |
GB2578803B (en) * | 2019-04-04 | 2020-12-16 | Cox Powertrain Ltd | Marine outboard motor with piston cooling gallery |
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US4346685A (en) * | 1979-01-23 | 1982-08-31 | Kawasaki Jukogyo Kabushiki Kaisha | Internal combustion engine with gas sealing device |
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FR2901577A3 (en) * | 2006-05-29 | 2007-11-30 | Renault Sas | Internal combustion engine`s piston, has transverse wall with internal cavity containing refrigerant fluid, and including annular part that extends skirt continuously on assembly of its circumference, in plan normal to translation axis |
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-
2012
- 2012-02-10 US US13/370,645 patent/US10753310B2/en active Active
-
2013
- 2013-02-08 EP EP13705889.7A patent/EP2812553B1/en active Active
- 2013-02-08 KR KR1020147023873A patent/KR102080359B1/en active IP Right Grant
- 2013-02-08 BR BR112014019774A patent/BR112014019774A8/en not_active IP Right Cessation
- 2013-02-08 JP JP2014556707A patent/JP2015511290A/en active Pending
- 2013-02-08 WO PCT/US2013/025283 patent/WO2013119909A1/en active Application Filing
- 2013-02-08 CN CN201380018416.XA patent/CN104204487B/en not_active Expired - Fee Related
-
2017
- 2017-09-26 JP JP2017184696A patent/JP6527203B2/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2000249A1 (en) * | 1970-01-05 | 1971-09-23 | Koehler Wolfgang Dipl Ing | Pistons for internal combustion engines |
US4346685A (en) * | 1979-01-23 | 1982-08-31 | Kawasaki Jukogyo Kabushiki Kaisha | Internal combustion engine with gas sealing device |
DE102004038945A1 (en) * | 2004-08-11 | 2006-02-23 | Mahle International Gmbh | Light metal piston with heat pipes |
FR2901577A3 (en) * | 2006-05-29 | 2007-11-30 | Renault Sas | Internal combustion engine`s piston, has transverse wall with internal cavity containing refrigerant fluid, and including annular part that extends skirt continuously on assembly of its circumference, in plan normal to translation axis |
Also Published As
Publication number | Publication date |
---|---|
JP6527203B2 (en) | 2019-06-05 |
US10753310B2 (en) | 2020-08-25 |
EP2812553A1 (en) | 2014-12-17 |
KR102080359B1 (en) | 2020-02-21 |
KR20140120923A (en) | 2014-10-14 |
US20130206095A1 (en) | 2013-08-15 |
JP2015511290A (en) | 2015-04-16 |
BR112014019774A8 (en) | 2017-07-11 |
EP2812553B1 (en) | 2019-10-16 |
CN104204487B (en) | 2017-11-14 |
JP2018021560A (en) | 2018-02-08 |
BR112014019774A2 (en) | 2017-06-20 |
CN104204487A (en) | 2014-12-10 |
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