Piston for internal combustion engines

• US 5,894,824 A
• Filed: 02/28/1997
• Issued: 04/20/1999
• Est. Priority Date: 02/29/1996
• Status: Expired due to Fees

• Current Assignee: Unisia Jecs Corporation (Hitachi, Ltd.)
• Original Assignee: Unisia Jecs Corporation (Hitachi, Ltd.)
• Inventors: Shirane, Kazuhiko, Watanabe, Hiroaki, Miyasaka, Hideyuki, Motoda, Shingo
• Primary Examiner(s): MCMAHON, MARGUERITE J
• Application Number:
  US08/808,749
• Time in Patent Office: 781 Days
• Field of Search: 123/193.6, 92/187
• US Class Current: 123/193.6
• CPC Class Codes: F02F 3/022 the pistons having an oval circumference or non-cylindrical shaped skirts, e.g. oval F02F3/025, F02F3/027 take precedence
• CPC Class Codes: F05C 2251/042 Expansivity

Abstract

A piston for an internal combustion engine includes a ring land formed with a piston-ring groove, and a skirt connected to the ring land so that the piston-ring groove is adjacent thereto, the skirt being formed with a piston-pin hole with an axis, and having a plane including the axis of the piston-pin hole. A taper is formed on the skirt in a first portion thereof nearer to the ring land than the plane to converge on the ring land.

Claims

1. A piston for an internal combustion engine, comprising:

a ring land formed with a piston-ring groove;

a skirt connected to said ring land so that said piston-ring groove is adjacent to said skirt, said skirt being formed with a piston-pin hole with a first axis substantially perpendicular to a central longitudinal axis of said piston; and

a taper formed on an external surface of said skirt, said taper extending from a side surface of said piston-ring groove toward a plane including said first axis of said piston-pin hole, said taper converging on said ring land, said taper extending to at least a reference point located at half a distance between said first axis of said piston-pin hole and said side surface of said piston-ring groove.

2. A piston as claimed in claim 1, wherein said piston-pin hole has a second axis substantially perpendicular to said first axis, and wherein said second axis of said piston-pin hole is offset toward a counterthrust side of said piston with respect to said central longitudinal axis of said piston.

3. A piston as claimed in claim 1, wherein said taper is arranged on a thrust side of the piston.

4. A piston as claimed in claim 3, wherein said piston has an imaginary axis parallel to said central longitudinal axis and intersecting said reference point, and said taper has a taper amount defined as a distance along said first axis from said imaginary axis to an outermost point of said skirt on said thrust side, said taper amount having a value given by multiplying a diameter (μ

m) of said piston by 0.00015 to 0.0006.

5. A piston as claimed in claim 1, wherein said skirt is, on a thrust side of the piston, gradually circumferentially increased in thickness from positions along a plane that is substantially perpendicular to said first axis of said piston-pin hole and that divides the thrust side of the piston and a counterthrust side of the piston.

6. A piston as claimed in claim 1, wherein said piston-ring groove is formed, on a thrust side of the piston, with a slit for fluid communication between inside and outside of the piston.

7. A piston as claimed in claim 6, wherein said slit is formed with a recess hole at either circumferential end thereof.

8. A piston as claimed in claim 1, wherein said skirt has a surface roughness which, at least on a thrust side of the piston, is greater in a first portion nearer said ring land relative to said plane than in a second portion farther from said ring land relative to said plane.

9. A piston as claimed in claim 1, wherein said piston-ring groove is formed with a hole on the thrust side of the piston, said hole partly extending to said skirt over said side surface of said piston-ring groove, said hole being deeper than said piston-ring groove, said hole failing to be in communication with an inner periphery of the piston.

10. A piston as claimed in claim 9, wherein said ring land is formed with a through hole located to be substantially symmetrical with said hole of said piston-ring groove with respect to said central longitudinal axis of the piston, said through hole partly extending to said skirt over said side surface of said piston-ring groove, said through hole communicating with said inner periphery of the piston.