Method of heat treating high carbon alloy steel parts to develop surface compressive residual stresses

Claim 3

The method as in claim 1, in which the carburizing atmosphere of step (b) is constituted to be endothermic gas containing 3-10% methane.

Claim 4

The method as in claim 1, in which said article is constituted by having 7% alloying ingredients with about 5% Cr, so that when said heat treatment is carried out, at about 1650° F., a retained austenite gradient is established.

Claim 5

The method as in claim 1, in which said article is constituted with about 17.5% alloying ingredients, with about 4% Cr, so that when heat treatment at about 1650° F. is carried out, a hardness gradient is established.

Claim 6

The method as in claim 1, in which step (c) is comprised of quenching to room temperature, and then additionally quenching in liquid nitrogen.

Claim 7

The method as in claim 4, in which the hardness gradient provides a differential between the hardness of said core and the surface region of at least 2 R c .

Claim 8

The method as in claim 3, in which the retained austenite gradient provides a differential between the core and surface region austenite of at least 10%.

Claim 9

The method as in claim 1, in which said heating is carried out at a temperature level of 815° C. for a period of about 1 hour, and the carbon potential of said carburizing atmosphere is regulated to be sufficiently high to saturate a 0.0025" thick iron foil in 30 minutes.

Claim 10

The method as in claim 1, in which the resulting article possesses a resistance to bending fatigue due to compressive residual surface stresses induced by a gradient in dissolved carbon of at least 10,000 psi in the surface region thereof and tensile stresses in the core thereof.

Claim 11

The method as in claim 1, in which the resulting article is characterized by resistance to rolling contact fatigue having a B10 fatigue life of at least 4.5 million stress cycles at a maximum hertzian contact stress of 729,000 psi.

Claim 12

The method as in claim 1, in which said steel is constituted to contain 1%C, 1.05% Cr, 0.35% Mn, 0.25 Si and the remainder Fe.

Claim 13

The method as in claim 1, in which said alloying ingredients, other than chromium, are present in an amount of at least 0.50%.

Claim 14

The method as in claim 1, in which said heated and quenched article is subjected to a tempering treatment at 100°-300° C. for 1-2 hours.

Claim 15

A high carbon steel alloy article having gradients of compressive residual stress, and at least one of a carbon gradient and hardness gradient proceeding from the surface region of said article to its core, said article being characterized by a microstructure consisting essentially of tempered martensite, retained austenite and a carbide phase, said article having a chemical content consisting essentially of 0.8-1.6% carbon, 0.75-25% alloying ingredients including 0.2-5% chromium, the remainder being essentially iron, said article having a compressive residual stress level at its surface region of at least 10,000 psi, and tensile stresses at the article core, said article having a hardness differential between its surface and core of at least 2.0 R c , and a volume fraction of primary carbides at its surface region of at least 0.18.

Claim 16

A high carbon steel alloy article having gradients of compressive residual stress, and at least one of a carbon gradient and hardness gradient proceeding from the surface region of said article to its core, said article being characterized by a microstructure consisting essentially of tempered martensite, retained austenite and a carbide phase, said article having a chemical content consisting essentially of 0.8-1.6% carbon, 0.75-25% alloying ingredients including 0.2-5% chromium, the remainder being essentially iron, said article having a compressive residual stress level at its surface region of at least 10,000 psi, and tensile stresses at the article core, said article having a hardness differential between its surface and core of at least 2.0 R c , and a volume fraction of primary carbides at its surface region of at least 0.18.

Claim 17

The steel alloy article as in claim 14, which is further characterized by a B10 rolling contact fatigue life of at least 4.5 million stress cycles, and a B50 life of at least 8.0 million stress cycles with a hertzian contact stress of 729,000 psi.

Claim 18

The steel alloy article as in claim 14, in which the volume fraction of retained austenite is about 25% at the surface.

Claim 19

The steel alloy article as in claim 14, in which the region of said article extending from the surface to 0.004 mm contains oxides in the grain boundaries, the region from 0.004 mm-0.008 mm is carbide depleted, and the region from 0.008-0.1 mmm contains 0.18 volume fraction of carbides.

Claim 20

The steel alloy article as in claim 14, which is further characterized by resistance to subsurface crack initiation at hard inclusions and the resistance to surface initiated cracking as a result of the high compressive stress distribution in its surface region.

Claim 23

The method as in claim 19, in which step (c) is further followed by an additional quenching operation employing liquid nitrogen.

Claim 24

The method as in claim 19, in which the resultant bearing body is characterized by an average B10 contact fatigue life of at least 4.5 million stress cycles, and an average B50 life of at least 8.0 million stress cycles at a maximum hertzian contact stress of 729,000 psi.

Claim 25

In a method for preparing bearing components wherein a hot-formed shape of low alloy steel containing carbon in the range of 0.8-1.5% and containing alloying ingredients in an amount to achieve a hardening response from heat treatment throughout said shape, said alloying ingredients being selected from a group consisting of Cr, Mn, Ni, Cu and Mo, said shape being subjected sequentially to a spheroidizing-anneal treatment, a rough forming treatment, and a hardening austenitizing treatment, the improvement comprising: (a) carrying out said hardening-austenitizing treatment in a carburizing atmosphere having a carbon potential sufficiently high to saturate a 0.0025" thick iron foil in 30 minutes and at a temperature level of between 800°-900° C. for a period of time between 1-2.5 hours to establish both carbon additions and an increase in the primary carbide and retained austenite phases of said steel in the surface layers of the steel; (b) establishing a compressive residual stress gradient in said steel by quenching said steel at a rate such that the core experiences a cooling rate of at least 300° F. per second when it is passing through the temperature zone of 1300°-700° F., said resultant article having a compressive stresses in the surface region which range between 5-40 KSI and tensile stresses in its core.

Claim 26

In a method for preparing bearing components wherein a hot-formed shape of low alloy steel containing carbon in the range of 0.8-1.5% and containing alloying ingredients in an amount to achieve a hardening response from heat treatment throughout said shape, said alloying ingredients being selected from a group consisting of Cr, Mn, Ni, Cu and Mo, said shape being subjected sequentially to a spheroidizing-anneal treatment, a rough forming treatment, and a hardening austenitizing treatment, the improvement comprising: (a) carrying out said hardening-austenitizing treatment in a carburizing atmosphere having a carbon potential sufficiently high to saturate a 0.0025" thick iron foil in 30 minutes and at a temperature level of between 800°-900° C. for a period of time between 1-2.5 hours to establish both carbon additions and an increase in the primary carbide and retained austenite phases of said steel in the surface layers of the steel; (b) establishing a compressive residual stress gradient in said steel by quenching said steel at a rate such that the core experiences a cooling rate of at least 300° F. per second when it is passing through the temperature zone of 1300°-700° F., said resultant article having a compressive stresses in the surface region which range between 5-40 KSI and tensile stresses in its core.