Friction loss-reduced piston for an internal combustion engine

Patent metadata

Field	Value
Publication number	US-12209551-B2
Application number	US-202017627990-A
Country	US
Kind code	B2
Filing date	Jul 20, 2020
Priority date	Jul 19, 2019
Publication date	Jan 28, 2025
Grant date	Jan 28, 2025

Abstract

A piston for an internal combustion engine, said piston having an upper piston portion ( 1 ) in which a ring zone ( 2 ) is located, and a piston lower part ( 3 ) having two opposing, load-carrying skirt wall sections ( 4,5 ) on the pressure- and counter-pressure sides of the piston adjoins the upper piston portion ( 1 ), and the two load-carrying skirt wall sections ( 4,5 ) are interconnected via connecting walls ( 6,7 ) that are recessed relative to the outer diameter of the piston. Each connecting wall ( 6, 7 ) includes a pin bore having a pin bore axis ( 18 ) for receiving a pin. The two opposing, load-carrying wall sections ( 4, 5 ) have different wall thicknesses and different transition regions at the transition of their lateral skirt connections ( 8,9 and 16,17 ) to the recessed connection walls ( 6,7 ).

First claim

What is claimed is:

1. A piston of an internal combustion engine, comprising an upper piston portion ( 1 ) in which a ring zone ( 2 ) is located, wherein, starting at the upper piston portion ( 1 ), a piston bottom part ( 3 ) with two opposing skirt wall sections ( 4 , 5 ) is respectively provided on a pressure and a counter pressure side of the piston, and the two opposing skirt wall sections ( 4 , 5 ) are interconnected via connecting walls ( 6 , 7 ) that are set back relative to an outer diameter of the piston, wherein in each connecting wall ( 6 and 7 ) a pin bore having a pin bore axis for receiving a pin is provided, wherein the two opposing skirt wall sections ( 4 and 5 ) comprise different transition areas at a transition of their lateral skirt connections ( 8 , 9 and 16 , 17 ) to the connecting walls ( 6 , 7 ), wherein the skirt wall section ( 5 ) of the counter pressure side comprises a central skirt region ( 15 ) extending all the way to a ring zone bulge ( 12 ), wherein the central skirt region ( 15 ) tapers in a direction toward the upper piston portion ( 1 ), wherein the lateral skirt connections ( 8 , 9 ) on the counter pressure side are configured to coordinate with the taper of the central skirt region ( 15 ), and wherein the central skirt region ( 15 ) comprises a constant wall thickness ( 30 ), the skirt wall section ( 4 ) of the pressure side further comprises:
two central skirt regions including an upper central skirt region ( 13 ) adjacent to the ring zone bulge ( 12 ) and a lower central skirt region ( 14 ) positioned distant from the ring zone bulge ( 12 ), to which the lateral skirt connections ( 16 , 17 ) on the pressure side are laterally adjoined, wherein the upper central skirt region ( 13 ) extends from the ring zone bulge ( 12 ) past a center of the pin bore axis ( 18 ) toward the lower central skirt region ( 14 ) and has a wall thickness ( 34 ) that is constant along an entire height ( 38 ) of the upper central skirt region ( 13 ) and the lower central skirt region ( 14 ) has a constant wall thickness ( 32 ) along an entire height ( 28 ) of the lower central skirt region ( 14 ), wherein the constant wall thickness ( 34 ) of the upper central skirt region ( 13 ) is different than the constant wall thickness ( 32 ) of the lower central skirt region ( 14 ).

2. The piston according to claim 1 , wherein the two opposing skirt wall sections ( 4 and 5 ) wall thicknesses are different from each other.

3. The piston according to claim 2 , further defining undercuts ( 10 , 11 ) projecting into the upper piston portion ( 1 ) are incorporated on an outside of the connecting walls ( 6 , 7 ) and comprise arcuate cross sections.

4. The piston according to claim 2 , wherein the ring zone bulge ( 12 ) defines a cavity, the ring zone bulge extending into the upper piston portion ( 1 ) and is provided within the skirt wall sections ( 4 and 5 ) and the connecting walls ( 6 , 7 ).

5. The piston according to claim 2 , wherein a portion of the upper central skirt region ( 13 ) is arranged at the level of the pin bore above the pin bore axis ( 18 ) thereof and is designed as a strip.

6. The piston according to claim 1 , wherein the ring zone bulge ( 12 ) defines a cavity, the ring zone bulge extending into the upper piston portion ( 1 ) and is provided within the skirt wall sections ( 4 and 5 ) and the connecting walls ( 6 , 7 ).

7. The piston according to claim 1 , wherein a portion of the upper central skirt region ( 13 ) is arranged at the level of the pin bore above the pin bore axis ( 18 ) thereof and is designed as a strip.

8. The piston according to claim 7 , wherein the lower central skirt region ( 14 ) extends from a lower edge of the pin bore to a lower edge ( 36 A) of the skirt wall section ( 4 ) on the pressure side.

9. The piston according to claim 1 , wherein the lower central skirt region ( 14 ) extends from a lower edge of the pin bore to a lower edge ( 36 A) of the skirt wall section ( 4 ) on the pressure side.

10. The piston of claim 1 , wherein the constant wall thickness ( 34 ) of the upper central skirt region is 2.5% to 6% of a nominal diameter of the piston, and the constant wall thickness ( 32 ) of the lower central skirt region is 1% to 3% of the nominal diameter of the piston.

11. The piston of claim 10 , wherein the transition areas of the lateral skirt connections ( 8 , 9 ) of the counter pressure side further comprises:
an area ( 24 ) of the counter pressure side having a height of 9%-15% of an outer diameter of the piston extends axially upward from a lower edge ( 36 ) of the skirt wall section ( 5 ) to an upper end, wherein a connection radius of the area ( 24 ) between the central skirt region ( 15 ) and the respective connecting wall ( 6 , 7 ) is a value of 5%-8% of the outer diameter of the piston, the connection radius of the area ( 24 ) remaining constant along the height of the area ( 24 ); and
an area ( 22 ) of the counter pressure side having a height of 14%-20% of the outer diameter of the piston extends axially upward from the upper end of the area ( 24 ) to a connection radius ( 37 ) of the ring zone bulge ( 12 ), wherein a connection radius of the area ( 22 ) between the central skirt region ( 15 ) and the respective connecting wall ( 6 , 7 ) increases along the height of the area ( 22 ) from a value of 5%-8% of the outer diameter of the piston from the upper end of the area ( 24 ) to a value of 15%-20% of the outer diameter of the piston to the connection radius ( 37 ) of the ring zone bulge ( 12 ).

12. The piston of claim 11 , wherein the transition areas of the lateral skirt connections ( 16 , 17 ) to the connecting walls ( 6 , 7 ) of the pressure side comprise a connection radius having a value of 9%-17% of the outer diameter of the piston and remains constant.

Assignees

• Ks Kolbenschmidt Gmbh

Inventors

• Suyama Satoru
• Takashima Yasuo
• Nonaka Yoshie
• Yamamoto Takumi

Classifications

• F02F3/00 Primary

  Pistons · CPC title

• F16J1/16

  with gudgeon-pin; Gudgeon-pins · CPC title

• F02F3/02 Primary

  having means for accommodating or controlling heat expansion · CPC title