Pistons for internal combustion engines

• US 4,140,096 A
• Filed: 03/30/1977
• Issued: 02/20/1979
• Est. Priority Date: 03/31/1976
• Status: Expired due to Term

• Current Assignee: Perkins Engines Ltd (Caterpillar Incorporated)
• Original Assignee: Perkins Engines Ltd (Caterpillar Incorporated)
• Inventors: Dunn, Stephen J., Youdan, Glyn H.
• Primary Examiner(s): Lazarus, Ronald H.
• Application Number:
  US05/782,695
• Time in Patent Office: 692 Days
• Field of Search: 123/193 P, 123/193 CP, 123/191 SP, 123/191 A, 123/32 C, 123/32 AA
• US Class Current: 123/193.6
• CPC Class Codes: F02B 2023/0612 the material having a high temperature and pressure resistance, e.g. ceramic
• CPC Class Codes: F02B 23/0636 the combustion space having a substantially flat and horizontal bottom
• CPC Class Codes: F02B 23/0654 Thermal treatments, e.g. with heating elements or local cooling
• CPC Class Codes: F02B 3/06 with compression ignition compression ignition engines using air or gas for blowing fuel into compressed air in cylinder F02B13/02
• CPC Class Codes: F02F 2200/04 Forging of engine parts
• CPC Class Codes: F02F 3/02 having means for accommodating or controlling heat expansion
• CPC Class Codes: F05C 2201/021 Aluminium
• CPC Class Codes: F05C 2201/0448 Steel
• CPC Class Codes: F05C 2251/042 Expansivity
• CPC Class Codes: F16J 1/005 obtained by assembling several pieces
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A piston for an internal combustion engine, having a combustion chamber with an overhanging lip formed by resistant metal insert anchored in the piston by means of members extending from the insert and embedded in the piston material. A portion of the free end of each member is located in a cool portion of the piston and mechanically keyed therein and is preferably also metallurgically bonded to the piston material in order to prevent the insert being loosened during service.

Claims

1. A piston for an internal combustion engine comprising a piston body of a first metal, a crown in said piston body, a combustion chamber in said crown, a lip portion overhanging said combustion chamber, said lip portion being constituted by an annular insert of a second metal more resistant to operating conditions in said chamber than said first metal, limbs of a third metal secured at one end to the annular insert comprising at least one member embedded in said body and extending from said insert into a portion of said body having a temperature of about 150 degrees centigrade at maximum operating temperature of said piston.

2. A piston according to claim 1 wherein, said annular insert metal is capable of forming a metallurgical bond with the first metal when coated with a bonding metal or agent.

3. A piston according to claim 1 wherein the said annular insert is made from a copper base alloy selected from a group consisting of 0.5% beryllium, 2.5% cobalt, remainder copper, 8% aluminium remainder copper, and 2% nickel remainder copper.

4. A piston according to claim 1 wherein the said limb is made from a ferrous material selected from the group consisting of a cast iron containing 3% carbon, 14% nickel, 7% copper, 3% cobalt remainder iron, and an austenitic steel.

5. A piston according to claim 1 wherein the said insert is made from a ferrous material selected from the group consisting of a cast iron containing 3% carbon, 14% nickel, 7% copper, 3% cobalt remainder iron, and an austenitic steel.

6. A piston according to claim 1 wherein the limbs are made integrally with the annular insert.

7. A piston according to claim 1 wherein said anchoring means consists of a ferrous material selected from the group consisting of a cast iron containing 3% carbon, 14% nickel, 7% copper, 3% cobalt remainder iron and an austenitic steel, and said anchoring means is coated with a bonding metal selected from the group consisting of aluminium silicon alloy, zinc and nickel.

8. A piston according to claim 1 wherein said anchoring means consists of a copper alloy selected from a group consisting of 0.5% beryllium, 2.5% cobalt remainder copper, 8% aluminium remainder copper, and 2% nickel remainder copper, and said anchoring means is coated with a bonding metal selected from the group consisting of zinc and nickel.