1. Technical Field
This invention relates generally to internal combustion engines, and more particularly to pistons therefor.
2. Related Art
Engine manufacturers are encountering increasing demands to improve engine efficiencies and performance, including, but not limited to, improving fuel economy, improving fuel combustion, reducing oil consumption, increasing the exhaust temperature for subsequent use of the heat within the vehicle, increasing compression loads within the cylinder bores, decreasing weight and making engines more compact. Accordingly, it is desirable to increase the temperature and compression loads within the combustion chamber of the engine. However, by increasing the temperature and compression loads within the combustion chamber, the wear and physical demands on the piston are increased, thereby reducing its potential useful life. A particular area of concern is with the excessive heat buildup and associated wear within the piston ring region of the piston.
A piston constructed in accordance with this invention is able to 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 is provided. The piston has a body that extends along a longitudinal central axis. The body includes an upper combustion wall having an upper combustion surface, a cylindrical outer wall with a ring belt region adjacent the upper combustion surface, a pair of pin bosses having pin bores aligned along a pin bore axis beneath the upper combustion wall, and a closed annular cooling gallery located in radial alignment with the ring belt region. A coolant medium is contained in the cooling gallery. The cooling gallery has an inner surface including a radially outermost portion that extends along the ring belt region. The outermost portion converges from the upper combustion wall toward the longitudinal central axis. Accordingly, during a downward stroke of the piston, the cooling medium is caused to flow into contact with the upper combustion wall, thereby allowing heat to be transferred from the upper combustion wall to the cooling medium.
A piston for an internal combustion engine constructed in accordance with another aspect of the invention includes a body extending along a longitudinal central axis. The body includes an upper combustion wall having an upper combustion surface, a cylindrical outer wall with a ring belt region adjacent the upper combustion surface, a pair of pin bosses beneath the upper combustion wall, a closed annular cooling gallery located radially inwardly from the ring belt region, and a cooling medium contained in the cooling gallery. The cooling gallery has an inner surface bounding the cooling gallery. The inner surface includes a web that diverges conically from the upper combustion wall away from the longitudinal central axis to a lowermost valley of the cooling gallery. Accordingly, during a downward stroke of the piston, the cooling medium is caused to flow into contact with the upper combustion wall, thereby allowing heat to be transferred from the upper combustion wall to the cooling medium.
These and other aspects, features and advantages of the invention will become more readily appreciated when considered in connection with the following detailed description of presently preferred embodiments and best mode, appended claims and accompanying drawings, in which:
Referring in more detail to the drawings,
The cooling medium 28 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 properties desired. Further, the cooling medium 28 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 change the specific heat of the cooling medium 28. Further yet, heat transfer liquids, such as those typically used for industrial heat exchanging, can be used.
As best shown in
The upper combustion surface 16 is represented as having a combustion bowl 42 recessed therein to provide the desired gas flow within the cylinder bore. As a result of the combustion bowl 42 being recessed within the upper combustion surface 16, the combustion wall 16 has a relatively thin thickness (t) across its entirety, as viewed in axial cross-section. In particular, the combustion wall 16 includes a first region 44, second region 46 and a third region 48, wherein the second and third regions 46, 48 are thinned due to the recessed combustion bowl 42.
The cooling gallery 26 is configured to optimize the cooling effect of the cooling medium 28. In particular, the cooling gallery 26 can be viewed as being bounded by four different portions of the inner surface 30, including an uppermost first portion 50 of the inner surface 30 that extends beneath the first region 44 of the combustion wall 16, an inner second portion 52 of the inner surface 30 that extends along the second region 46 of the combustion wall 16, an inner third portion 54 of the inner surface 30 that extends along a web 55 that diverges from the combustion wall 16 away from the longitudinal central axis 14 to a lowermost valley 57 of the cooling gallery 26 and generally to the outer wall 21, and an outer fourth portion 56 that extends generally along the ring belt region 22 of the outer wall 21. The second, third and fourth portions 52, 54, 56 are inclined having an angular relation in accordance with the invention, relative to the longitudinal axis 14 and pin bore axis 36, to provide the desired fluid flow of the cooling medium 28 within the cooling gallery 26 during reciprocating upward and downward strokes of the piston 10 within the cylinder bore.
The second portion 52 of the inner surface 30 is an upper radially inner portion that extends along a valley portion of the combustion bowl 42 generally along an axis 58 that converges conically from the first portion 50 of the upper combustion wall 16 toward the longitudinal central axis 14. The angle of convergence relative to the longitudinal axis 14 can be selected as desired, such as between 15-75 degrees, and preferably between 30-60 degrees. This angular slope of the second portion 52 causes the cooling medium 28 to be directed radially outwardly toward the outer wall 21 as the piston 10 is moving downwardly during a downward stroke within the cylinder bore, thereby carrying heat away from the upper combustion wall 16 to the outer wall 21, whereupon the heat can be readily transferred to the cylinder liner and engine block.
The third portion 54 of the inner surface 30 is a lower radially inner portion that extends along an axis 60 that diverges conically from the upper combustion wall 16 away from the longitudinal central axis 14 toward the outer wall 21. Then angle of divergence relative to the longitudinal axis 14 can be selected as desired, such as between 15-75 degrees, and preferably between 30-60 degrees. This angular slope of the third portion 54 causes the cooling medium 28 to be directed radially outwardly toward the outer wall 21 as the piston 10 is moving downwardly during a downward stroke within the cylinder bore, thereby carrying heat away from the upper combustion wall 16 to the outer wall 21, whereupon the heat can be readily transferred to the cylinder liner and engine block.
The fourth portion 56 of the inner surface 30 is a radially outermost portion that extends generally along an axis 62 that converges conically from the upper combustion wall 16 toward the longitudinal central axis 14. Then angle of convergence of the axis 62 relative to the longitudinal axis 14 can be selected as desired, such as between 1-30 degrees, and preferably between 10-20 degrees. This angular slope of the fourth portion 56 causes the cooling medium 28 to be directed radially inwardly and thereby efficiently transferring absorbed heat from the combustion wall 16 and the fourth portion 52 to the ring belt region 22 as the piston 10 is moving upwardly during an upward stroke within the cylinder bore. Accordingly, the heat transfer cycle is complete, which allows the efficient transfer of heat from the combustion wall 16 downwardly and outwardly and ultimately to the cylinder liner and engine block.
Obviously, given the detailed description of presently preferred embodiments discusses above, many modifications and variations 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.
Number | Name | Date | Kind |
---|---|---|---|
1678957 | Phillip | Jan 1926 | A |
1878566 | Woolson | Feb 1929 | A |
1820628 | Niven | Aug 1931 | A |
1876917 | Gosslau | Sep 1932 | A |
1905582 | Gazda | Apr 1933 | A |
1953109 | Heron | Apr 1934 | A |
2126306 | Bernard | Aug 1938 | A |
2153501 | Harper, Jr. | Apr 1939 | A |
2155383 | Carr | Apr 1939 | A |
3385375 | Pratt | May 1968 | A |
3545341 | Fischer | Dec 1970 | A |
3616729 | Fischer | Nov 1971 | A |
3703126 | Haug | Nov 1972 | A |
4356800 | Moebus | Nov 1982 | A |
4493292 | Showalter | Jan 1985 | A |
4587932 | Moebus | May 1986 | A |
5339775 | Clarke et al. | Aug 1994 | A |
6026777 | Kemnitz et al. | Feb 2000 | A |
6957638 | Scharp | Oct 2005 | B2 |
7628135 | Messmer | Dec 2009 | B2 |
8074617 | Grahle et al. | Dec 2011 | B2 |
20070137605 | Scharp | Jun 2007 | A1 |
20100275861 | Schneider | Nov 2010 | A1 |
20110226211 | Messmer | Sep 2011 | A1 |
20130146017 | Muscas et al. | Jun 2013 | A1 |
Number | Date | Country |
---|---|---|
19915782 | Nov 2000 | DE |
S53154907 | Dec 1978 | JP |
56017335 | Feb 1981 | JP |
57156053 | Sep 1982 | JP |
S5924853 | Jul 1984 | JP |
H02131055 | Oct 1990 | JP |
Entry |
---|
International search report mailed Apr. 19, 2013 (PCT/US2013/025256). |
Number | Date | Country | |
---|---|---|---|
20130206094 A1 | Aug 2013 | US |