Piston of internal combustion engine

• US 6,240,828 B1
• Filed: 04/09/1999
• Issued: 06/05/2001
• Est. Priority Date: 04/21/1998
• Status: Expired due to Fees

• Current Assignee: Nissan Motor Co., Ltd.
• Original Assignee: Nissan Motor Co., Ltd.
• Inventors: Fujimoto, Hiroya
• Primary Examiner(s): Ryznic, John E.
• Application Number:
  US09/288,715
• Time in Patent Office: 788 Days
• Field of Search: 922/08, 922/14, 922/32, 922/22, 922/25, 922/26, 922/27, 922/28, 922/29, 922/30
• US Class Current: 92/214
• CPC Class Codes: F02F 3/02 having means for accommodating or controlling heat expansion
• CPC Class Codes: F02F 3/08 the inserts being ring-shaped
• CPC Class Codes: F05C 2251/042 Expansivity

Abstract

A piston of an internal combustion engine, comprises a skirt portion in sliding-contact with a cylinder wall, an inner crown-plus-boss portion having a crown portion and piston-pin boss portions, and a stay portion interconnecting the skirt portion and the inner crown-plus-boss portion at a lower portion of the piston. Also provided is an annular partition groove through which a rim of the skirt portion and the inner crown-plus-boss portion are partitioned all around the circumference of the upper portion of the piston. A thermal-expansion absorption ring is tightly fitted into the annular partition groove in a gas tight-fashion. The top face of the inner crown-plus-boss portion, the flat face of the rim of the skirt portion, and the top wall of the thermal-expansion absorption ring serve as a piston crown.

Claims

1. A piston of an internal combustion engine comprising:

a skirt portion adapted to be in sliding-contact with a cylinder wall;

an inner crown-plus-boss portion having a crown portion and piston-pin boss portions;

a stay portion interconnecting said skirt portion and said inner crown-plus-boss portion at a lower portion of the piston; and

a partition groove that separates said skirt portion and said inner crown-plus-boss portion and which comprises an annular separation slot which extends completely around a circumference of an upper surface of an upper portion of the piston.

2. The piston as claimed in claim 1, wherein said skirt portion (12) has an upper skirt portion (12a) located in the upper portion (20) of the piston and annularly formed all around the circumference of the upper portion (20) of the piston, and a lower skirt portion (12b) located in the lower portion (22) of the piston and partly cut away under the piston-pin boss portions (12b, 12b) in a piston-pin direction.

3. The piston as claimed in claim 1, wherein an outer peripheral wall surface of said skirt portion is formed on a substantially same circumference of a circle throughout an entire axial length of said skirt portion.

4. The piston as claimed in claim 1, which further comprises a single ring groove (24) formed in an outer peripheral wall surface of an upper skirt portion (12a) located in the upper portion (20) of the piston, and a piston ring (23) fitted to the single ring groove.

5. The piston as claimed in claim 1, which further comprises a thermal-deflection absorption ring (30) fitted into said partition groove (D) and deformable in a radial direction of the piston for absorbing variations of a radial width of said partition groove.

6. The piston as claimed in claim 5, wherein said thermal-deflection absorption ring has a corrugated wall portion (36) deflectable in the radial direction of the piston.

7. The piston as claimed in claim 5, wherein said thermal-deflection absorption ring has a top wall portion (48;

62) being in sliding-contact with a top face of the I piston, so that the top wall portion is slidable in the radial direction of the piston in presence of the variations of the radial width of said partition groove.

8. The piston as claimed in claim 5, wherein said thermal-deflection absorption ring has a side wall portion (42, 44;

52, 54) facing one of an inner peripheral wall surface of said skirt portion (12) and a cylindrical side wall surface of the crown portion (14a) of said inner crown-plus-boss portion (14) and inclined in the radial direction so that one end of the side wall portion of said thermal-deflection absorption ring is in contact with said one of the inner peripheral wall surface of said skirt portion (12) and the cylindrical side wall surface of the crown portion (14a), and which further comprises a thermal-deflection absorption clearance (50, 50;

58, 58) defined between another end of the side wall portion of said thermal-deflection absorption ring and said one of the inner peripheral wall surface of said skirt portion (12) and the cylindrical side wall surface of the crown portion (14a) for absorbing the variations of the radial width of said partition groove.

9. The piston as claimed in claim 5, wherein said thermal-deflection absorption ring has a curved surface portion (68) having a substantially circular-arc shape in cross section and being curved inwards in the radial direction of the piston so that one end of the curved surface portion of said thermal-deflection absorption ring is in sliding-contact with one of an inner peripheral wall surface of said skirt portion (12) and a cylindrical side wall surface of the crown portion (14a) of said inner crown-plus-boss portion (14), and which further comprises a thermal-deflection absorption clearance (72) defined between another end of the curved surface portion of said thermal-deflection absorption ring and said one of the inner peripheral wall surface of said skirt portion (12) and the cylindrical side wall surface of the crown portion (14a) for absorbing the variations of the radial width of said partition groove.

10. The piston as claimed in claim 5, which further comprises a projected edged portion (60) formed on at least one of an upper inside edged portion of said skirt portion (12) and an upper outside edged portion of the crown portion (14a) and radially projecting towards said partition groove (D), for preventing falling of said thermal-deflection absorption ring.

11. The piston as claimed in claim 5, which further comprises a radially-protruding portion (64, 64;

74) formed in said thermal-deflection absorption ring, and a recessed portion (66, 66;

76) formed on at least one of an inner peripheral wall surface of said skirt portion (12) and a cylindrical side wall surface of the crown portion (14a) of said inner crown-plus-boss portion (14), so that the radially-protruding portion (64, 64;

74) is fitted into the recessed portion (66, 66;

76).

12. The piston as claimed in claim 5, wherein said thermal-deflection absorption ring has an oil passage (80) extending in a circumferential direction of the piston, and an oil hole (78) communicating the oil passage (80) for introducing lubricating oil into the oil passage (80) or exhausting the lubricating oil from the oil passage (80).

13. The piston as claimed in claim 12, wherein said thermal-deflection absorption ring has a pair of side wall portions (42, 44) respectively being in contact with an inner peripheral wall surface of said skirt portion (12) and a cylindrical side wall surface of the crown portion (14a) of said inner crown-plus-boss portion (14), and at least one of the pair of side wall portions (42, 44) has an auxiliary oil hole (82;

88;

96) communicating the oil passage (80).

14. The piston as claimed in claim 13, which further comprises an oil receiving portion (84;

92) formed in at least one of the inner peripheral wall surface of said skirt portion (12) and the cylindrical side wall surface of the crown portion (14a) to oppose the auxiliary oil hole (82;

88;

96).

15. The piston as claimed in claim 12, wherein said thermal-deflection absorption ring has a pair of side wall portions (42, 44) respectively being in contact with an inner peripheral wall surface of said skirt portion (12) and a cylindrical side wall surface of the crown portion (14a) of said inner crown-plus-boss portion (14), and at least one of the pair of side wall portions (42, 44) has a hole-flanged portion (86;

90) formed with an auxiliaryoil hole (82;

88) communicating the oil passage (80), and which further comprises an oil receiving portion (84;

92) formed in at least one of the inner peripheral wall surface of said skirt portion (12) and the cylindrical side wall surface of the crown portion (14a) to oppose the auxiliary oil hole (82;

88), and the hole-flanged portion is fitted into the oil receiving portion.

16. The piston as claimed in claim 12, wherein said thermal-deflection absorption ring has a pair of side wall portions (42, 44) respectively being in contact with an inner peripheral wall surface of said skirt portion (12) and a cylindrical side wall surface of the crown portion (14a) of said inner crown-plus-boss portion (14), and at least one of the pair of side wall portions (42, 44) has a plurality of slotted portions (94) each having an auxiliary oil hole (96) communicating the oil passage (80) and a pair of radially-inwardly protruding upper and lower flanges (94a, 94b), and which further comprises an oil receiving portion (84) formed in at least one of the inner peripheral wall surface of said skirt portion (12) and the cylindrical side wall surface of the crown portion (14a) to oppose the auxiliary oil hole (96), and the plurality of slotted portions (94) are fitted into the oil receiving portion (84).

17. The piston as claimed in claim 1, wherein said inner crown-plus-boss portion (14) has a rib (97) integrally formed on an underside of the crown portion (14a) and expanded radially outwards so that a vertex of the rib is formed close to either thrust side of a major thrust face and a minor thrust face of said skirt portion (12) while both ends of the rib are connected to respective root sections of the piston-pin boss portions (14b, 14b).

18. The piston as claimed in claim 17, wherein the rib (97) is dimensioned so that a height (h1) of the vertex of the rib close to the thrust side of side skirt portion (12) is lower than a height (h2) of the rib at each of the root sections of the piston-pin boss portions (14b, 14b).

19. The piston as claimed in claim 1, wherein said inner crown-plus-boss portion (14) has a plurality of ribs (97) integrally formed on an underside of the crown portion (14a) and expanded radially outwards so that a vertex of each of the ribs is formed close to either thrust side of a major thrust face and a minor thrust face of said skirt portion (12) while both ends of each of the ribs are connected to respective root sections of the piston-pin boss portions (14b, 14b), and wherein each of the ribs (97) is dimensioned so that a height (h1) of the vertex of each of the ribs close to the thrust side of said skirt portion (12) is lower than a height (h2) of each of the ribs at each of the root sections of the piston-pin boss portions (14b, 14b).

20. The piston as claimed in claim 19, wherein a height (h) of an inside rib of two adjacent ribs, measured in a same thrust direction, is lower than a height of an outside rib of the two adjacent ribs.

21. The piston as claimed in claim 19, wherein said inner crown-plus-boss portion (14) has an intermediate rib (98) integrally formed on the underside of the crown portion (14a) so that the intermediate rib (98) interconnects vertexes of the two adjacent ribs, and wherein the intermediate rib (98) is dimensioned so that a height (h) of the intermediate rib decreases gradually towards a center of the piston.

22. The piston as claimed in claim 5, wherein said thermal-deflection absorption ring defines at least one annular hollow space within said partition groove.

23. The piston as claimed in claim 5, wherein said thermal-deflection absorption ring has an indent portion which defines at least one annular space within said partition groove.

24. A piston of an internal combustion engine comprising:

a skirt portion having an upper annular end;

an inner crown-plus-boss portion having a crown portion and piston-pin boss portions, the crown portion having a peripheral edge portion located in a contact-free relationship inboard of and juxtaposedly spaced from the upper annular end of the skirt portion, to define an annular void via which free fluid communication between a space above the crown portion and a space below the piston-pin boss portion, is permitted, said annular void extending completely and continuously about the periphery of the crown portion to completely separate the crown and boss portion from the skirt portion; and

a resilient ring member disposed in the annular void so as to interconnect the upper annular end of the skirt portion and the peripheral edge portion of the crown portion in a manner which closes the annular void and prevents the free fluid communication therethrough.

25. The piston as claimed in claim 24, further comprising a stay portion interconnecting said skirt portion and said inner crown-plus-boss portion at a lower portion of the piston and at a level which is separate and spaced from the connection provided by the ring member.

27. The piston as claimed in claim 24, wherein said ring member defines at least one annular, hollow space within the annular void into which oil can be introduced from the space below the piston-pin boss portion.

26. A piston of an internal combustion engine comprising:

a skirt portion having an upper annular end;

an inner crown-plus-boss portion having a crown portion an piston-pin boss portions, the crown portion having a peripheral edge portion located in a contact-free relationship inboard of and juxtaposedly spaced from the upper annular end of the skirt portion, to define an annular void via which free fluid communication between a space above the crown portion and a space below the piston-pin boss portion, is permitted;

a ring member disposed in the annular void so as to interconnect the upper annular end of the skirt portion and the peripheral edge portion of the crown portion in a manner which closes the annular void and prevents the free fluid communication therethrough; and

wherein said ring member has at least one wall member which flexes and absorbs thermally induced radial expansion of the crown portion toward the upper annular end of the skirt portion.

28. A piston of an internal combustion engine comprising:

a skirt portion having an upper annular end;

an inner crown-plus-boss portion having a crown portion and piston-pin boss portions, the crown portion having a peripheral edge portion located in a contact-free relationship inboard of and juxtaposedly spaced from the upper annular end of the skirt portion, to define an annular void via which free fluid communication between a space above the crown portion and a space below the piston-pin boss portion, is permitted; and

thermal-expansion absorption ring means disposed in the annular void for interconnecting the upper annular end of the skirt portion and the peripheral edge portion of the crown portion in a manner which closes the annular void, prevents the free fluid communication therethrough, and resiliently absorbs thermal expansion of said inner crown-plus-boss portion toward the upper annular end of said skirt portion.