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    • 3. 发明专利
    • SE318297B
    • 1969-12-08
    • SE143766
    • 1966-02-04
    • NASA
    • ZARETSKY EPARKER RANDERSON W
    • C21D9/32C21D9/36F16C33/30F16C33/62F16C33/64C21D9/40
    • 1,117,841. Bearings; gearing. NATIONAL AERONAUTICS & SPACE ADMINISTRATION. 4 Feb., 1966 [8 Feb., 1965], No. 5050/66. Headings F2A and F2Q. [Also in Division B3] A method of making a rolling-element system having elements in rolling and sliding contact wherein one or more elements in contact receive a greater number of stress cycles on each point of the surface during the operation of the system than the other elements, comprises heat treating the elements receiving the lesser number of stress cycles per point to a predetermined hardness and heat treating the elements receiving the greater number of stress cycles per point to one to two points Rockwell C hardness less than the elements in contact therewith having the lesser number of stress cycles. When making rolling-element bearings blanks of highchromium steel are fabricated into rings and heat treated to a Rockwell C hardness not exceeding 60. The rings are then ground to form inner and outer races. Bearing balls are made from high carbon chromium steel and heat treated to a hardness approximately equal to that of the races. Subsequently the inner and outer races are tempered to a Rockwell C hardness one to two points less than the rolling elements. The rolling elements and races are then ground to their final dimensions and finish and finally assembled. Alternatively the races can be brought to their lower degree of hardness subsequent to being ground and finished. In a modification the race blanks are heat treated to at least Rockwell C58 hardness and the rolling element blanks to one or two points greater hardness prior to grinding and finishing. The method is also applicable to gear trains, in which case the gears having the greater number of teeth of meshing pairs are heat treated to a Rockwell C hardness one to two points more than the smaller gears.