Corrective tempering apparatus for rolling elements

Information

  • Patent Grant
  • 6248287
  • Patent Number
    6,248,287
  • Date Filed
    Tuesday, November 30, 1999
    26 years ago
  • Date Issued
    Tuesday, June 19, 2001
    24 years ago
Abstract
In a corrective tempering method and apparatus for a rolling element in which the thermal deformation of the rolling element is corrected within an extremely short time by utilizing plasticity exhibited during a metallic structure transforming process brought about by low-temperature tempering of the rolling element made of steel, the hardened rolling element is heated and pressured to a maximum temperature within a range of from 250 to 500° C. by a heating device while set in correcting molds to correct the deformation of the rolling element at a degree of working within a range not exceeding an elastic deformation range of the rolling element at a room temperature. The rolling element can be heated also by an induction heating device in addition to a conduction heating device. A product whose inner/outer diameter correcting degree of deformation is 60% or more, dimension standardizing rate is 30% or more, surface roughness is less than Ra 0.2 μm, and surface hardness is HRC 56 or more can be obtained for a correction time within 6 minutes and an induction heating time within 30 seconds.
Description




BACKGROUND OF THE INVENTION




The present invention relates to an improvement of a corrective tempering method and apparatus for correcting the hardening deformation of rolling elements.




In the process of manufacturing rolling elements such as the inner and outer races, cages, and other parts of, e.g., rolling bearings, the deformation of the rolling elements induced by such a heat treatment as hardening has heretofore been corrected by tempering. Conventional tempering methods include so-called “bracing tempering” and press tempering. The former method is characterized as correcting the deformation of a rolling element by subjecting the rolling element to such a normally tempering treatment as keeping the rolling element in the tempering furnace at a required temperature for 60 to 120 minutes with the rolling element being given a reversely bracing deformation using an appropriate tool. On the other hand, the press tempering method is characterized as correcting the deformation of a rolling element by subjecting the rolling element to the aforementioned normally tempering treatment with the rolling element pressured by molds or the like before the tempering treatment.




However, the conventional tempering methods address several problems. One problem is that the treatment time required for correcting the deformation of a rolling element is very long, not only because these methods involve the step of preparing and setting tools, molds, and the like in consideration of the size and amount of deformation of the rolling element to be corrected and pressuring the rolling element with these tools and molds, but also because the rolling element is thereafter subjected to the normally tempering treatment for 60 to 120 minutes in the furnace. More specifically, the following problems have been encountered.




(1) A number of tools and molds must be involved to treat a number of rolling elements on a mass production basis. Therefore, the conventional arts that are of low productivity cannot respond to the needs for mass production.




(2) Further, the tempering furnace, being heated with hot blast, takes 20 minutes or more for heating a rolling element, and there is a limit in shortening the treatment time imposed by this slow heating of the rolling element.




(3) Still further, if atmosphere temperature is increased to shorten the treatment time, the hardness of the rolling element is reduced.




(4) Still further, the heat-treated rolling element still holds inconsistencies caused in turning before the heat treatment, which in turn requires that grinding margins after the heat treatment be increased. As a result, grinding cost reduction is restricted.




SUMMARY OF THE INVENTION




The present invention has been made to overcome conventional problems. Therefore, the object of the invention is to provide a corrective tempering method and apparatus for rolling elements that can correct the heat-treatment deformation of the rolling elements within an extremely short time by utilizing plasticity exhibited during the metallic structure transforming process brought about by low-temperature tempering of the rolling elements that are made of steel.




To achieve the above object, a method according to the invention is achieved by a method of correctively tempering a rolling element of one of a hardened cylindrical element and a hardened annular element, the method including the steps of: inserting the rolling element into a mold to work at least one surface of an inner diameter surface and an outer diameter surface of the rolling element; and heating the rolling element for a heating time within six minutes to a maximum rolling element temperature within 250 to 500° C. to correct a hardening deformation of the rolling element.




Further, an apparatus according to the invention is achieved by an apparatus for correctively tempering a rolling element, which provides: an induction heater heating the rolling element to a desired temperature and including a heating coil; a mold constraining at least one of an inner surface, an outer surface of the rolling element and both of the inner and outer surfaces, the rolling element being at least one of a hardened cylindrical element and a hardened annular element; and a mold temperature adjusting device arranged relative to the heating coil for adjusting a temperature of the mold, the mold temperature adjusting device being positioned outside the heating coil in at least one direction of a radial direction and an axial direction of the heating coil.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a sectional view of a first embodiment illustrative of a mode of heating and pressuring method of the invention;





FIG. 2

is a diagram illustrating a relationship among product temperature, correcting degree of deformation and pressuring and heating time in a corrective tempering method, which is the first embodiment of the invention;





FIG. 3

is a graph illustrating a relationship among product temperature, rolling element hardness, and pressuring and heating time in the first embodiment of the invention;





FIG. 4

is a sectional view of a second embodiment illustrative of a mode of heating and pressuring method of the invention;





FIG. 5

is a sectional view of a third embodiment illustrative of a mode of heating and pressuring method of the invention;





FIG. 6

is a sectional view of a fourth embodiment illustrative of a mode of heating and pressuring method of the invention;





FIG. 7

is a sectional view of a fifth embodiment illustrative of a mode of heating and pressuring method of the invention;





FIGS. 8A and 8B

are diagrams illustrative of a method of measuring the amount of warpage of rolling elements;

FIG. 8A

is a sectional view in the case of a doughnutlike rolling element; and

FIG. 8B

is a sectional view in the case of an annular rolling element;





FIG. 9

is a sectional view of a first embodiment of a corrective tempering apparatus according to the invention;





FIG. 10

is a sectional view showing a main portion in a second embodiment of the corrective tempering apparatus according to the invention;





FIG. 11

is a sectional view showing a main portion in a third embodiment of the corrective tempering apparatus;





FIG. 12

is a sectional view showing a main portion in a fourth embodiment of the corrective tempering apparatus;





FIGS. 13A and 13B

each is a sectional view showing a main portion in a fifth embodiment of the corrective tempering apparatus;

FIG. 13A

shows the main portion before heating;

FIG. 13B

shows the main portion after heating;





FIG. 14

is a sectional view showing a main portion in a sixth embodiment of the corrective tempering apparatus;





FIGS. 15A and 15B

each is a sectional view showing a main portion in a seventh embodiment of the corrective tempering apparatus;

FIG. 15A

shows the main portion before heating;

FIG. 15B

shows the main portion after heating;





FIG. 16

is a sectional view showing a main portion in an eighth embodiment of the corrective tempering apparatus;





FIG. 17

is a diagram showing a relationship among maximum workpiece temperatures, correcting degrees of deformation, and workpiece surface hardnesses obtained by a corrective tempering test;





FIG. 18

is a diagram showing a relationship between maximum workpiece temperatures and dimension standardizing rates obtained by the corrective tempering test;





FIG. 19

is a diagram showing a relationship between degrees of working and surface roughnesses Ra (μm) of surfaces (the outer diameter surface in this case) obtained by the corrective tempering test, the surface being corrected by a correcting mold;





FIG. 20

is a diagram showing a relationship between degrees of working and correcting degrees of deformation obtained by the corrective tempering test;





FIG. 21

is a diagram showing an appropriate range (shaded portion) of corrective tempering conditions of the invention obtained from the relationship between maximum workpiece temperatures and degrees of working, the appropriate range being obtained by the corrective tempering test;





FIG. 22

is a diagram showing effects of the shape of a workpiece exerted on the corrective tempering conditions, the effects being obtained by a corrective tempering test;





FIG. 23A

is a plan view of a correcting mold used in another deformation correcting test with outer races of ball bearings used as workpieces;

FIG. 23B

is a sectional view taken along an arrow XXIII—XXIII shown in

FIG. 23A

; and





FIG. 24

is a diagram showing a relationship between correcting energy and product temperature with a S/V ratio as a parameter, the relationship being obtained by the deformation correcting test carried out using the mold shown in FIGS.


23


A and


23


B.











DETAILED DESCRIPTION OF THE INVENTION




Details of the present invention will hereinafter be described.




The inventors have positively made a study to overcome problems addressed by the conventional corrective tempering methods and apparatuses. As a result of the study, it was found out that corrective tempering can be implemented within an extremely short time (in the order of seconds) by (1) pressuring a rolling element to be corrected using a mold that has been heated to a predetermined temperature by a conduction heating device, and heating and pressuring the rolling element while transmitting the heat of the mold to the rolling element by conduction or by (2) heating and pressuring a rolling element to be corrected while pressuring the rolling element by a mold with the rolling element being heated to a predetermined temperature directly by an electromagnetic induction heating device. Hence, the inventors have found out that the deformation of a rolling element can be corrected within a short time with a smaller reduction in hardness compared with the corrective tempering methods using a conventional furnace.




That is, the invention is characterized in that carbon dissolved in martensite immediately after the hardening of a rolling element made of steel is precipitated and diffused as ε-carbides by heating the rolling element to 250 to 500° C. and that toughness is imparted to the rolling element by transforming the martensite from the tetragonal to the cubic. And post-treatment deformation of the rolling element such as warpage as well as pre-treatment mechanically produced dimensional inconsistencies are corrected by utilizing plasticity exhibited during this process.




Thus, in the corrective tempering method for rolling elements according to the invention, the amount of deformation such as warpage, dimensions, and the like can be controlled within a prescribed value and, at the same time, hardness is kept so as not to be reduced below HRC


56


which is required for the rolling element in order to maintain the rolling fatigue life.




Steel materials of which rolling elements of the invention are made are: carbon steels containing 0.5wt % or more of carbon, bearing steels containing about 1% of carbon, or case hardening steels containing 0.5wt % or less of carbon before case hardening and 0.6wt % or more of carbon in the case after case hardening. These steel materials are used either singly or in combination.




The reasons why the deformation correcting temperatures are set to values between 250 and 500° C. are as follows.




In the case of using bearing steels and case hardening steels in particular, deformation correction within a short time (within 6 minutes when mass production of the rolling elements is considered) is hard if the mold temperature is less than 250° C. On the other hand, at a mold temperature exceeding 500° C. in the case of conduction heating, not only hardness is reduced from HRC


56


that is required for bearings although the amount of deformation corrected remains unchanged, but also the durability of the mold is impaired. Therefore, mold temperatures ranging from 250 to 500° C. are desirable from the viewpoint of the control of product heating temperature. However, even if the mold temperature exceeds 500° C. (e.g., also 700° C.), such mold temperature is allowed as long as a rolling element is tempered at a maximum rolling element temperature within a range of from 250 to 500° C. for a time not exceeding 6 minutes.




Further, a corrective tempering time not exceeding 6 minutes is desired because the heating time must match the hardening speed of a rolling element during the manufacturing process.




The corrective tempering methods are characterized in that: after a cylindrical or annular rolling element has been subjected to hardening, the thus hardened rolling element is inserted into a mold whose temperature has already been adjusted; and the rolling element is then subjected to tempering by heating using a heating device to a high temperature within a range of from 250 to 500° C. for a short time with at least one of the outer surfaces (the outer diameter surface, the inner diameter surface, both end faces) of the rolling element bound by the mold. Conduction heating or induction heating is employed as the heating device.




In the case of induction heating, the heating time is within 30 seconds, which is thus advantageous in quickening the tempering treatment. In this case, the mold is preferred to be made of a material less affected by high frequencies. A material whose magnetic permeability is 1.5 or less is desirable; e.g., ceramic is desirable. The reason therefor is that corrective tempering can be implemented precisely, quickly, as well as reliably because such a material can prevent the mold temperature from increasing due to lines of magnetic force produced by the induction heating coil, so that the mold temperature can be controlled independently of the induction heating source.




Further, the mold must have a required strength. Materials other than ceramic capable of meeting these requirements are: nonmagnetic steels, aluminum, brass, and copper.




The expansion coefficient of a ceramic mold is about {fraction (1/5+L )} that of a steel mold. Therefore, a rolling element within the induction-heated mold is thermally expanded to be compressed and corrected strongly by the ceramic mold. At the same time, the rolling element precipitates and diffuses ε-carbides from the martensite at the time of hardening due to the effect of tempering, so that tempering is completed with the structural transformation.




According to the corrective tempering methods for rolling elements according to the invention, the deformation of a rolling element induced by hardening can be corrected by utilizing plasticity exhibited during the process of tempering the hard steel structure produced in the hardened rolling element. That is, the deformation can be corrected within an extremely short time. In addition, a minimum hardness of HRC


56


required to maintain the rolling fatigue life of a rolling element can be ensured, and the amount of warpage or deformation in the outer or inner diameter required to guarantee product accuracies can be controlled under a prescribed value. Moreover, a number of rolling elements can be manufactured on a mass production basis with a small number of tools and molds.




Still further, the corrective tempering methods of the invention can standardize the dimensions of rolling elements, which in turn contributes to improving roundness and inclination. Still further, the surface roughness of a rolling element can be improved by increasing the margin of fit between the rolling element and the mold. More specifically, such requirements as a correcting degree of deformation of 60% or more, a surface hardness of HRC


56


or more, a corrected surface roughness of Ra 0.2 μm or less, and a dimension standardizing rate of 30% or more can be achieved by the invention.




The corrective tempering apparatus of the invention is characterized in that: the induction heater is employed as a source for heating a rolling element, and that the mold temperature adjusting device is arranged outside the heating coil of the induction heater, so that the mold temperature can be controlled independently of the induction heating source, which in turn achieves precise, quick, and reliable corrective tempering of the rolling element.




The temperature adjuster, which is the mold temperature adjusting device of the corrective tempering apparatus of the invention, is constructed of a temperature control panel with a temperature sensor and a temperature adjusting source embedded therein. The temperature adjusting source is formed by either one of an electric heater or a heat medium solution circulation path alone or in combination with a cooling device such as a cooling water circulation path. The temperature adjusting panel is made, e.g., of a steel plate. The temperature adjusting panel may also be made of a metal that exhibits good heat conductivity including ceramic such as SiC, copper, and aluminum. This temperature control panel is arranged so as to be in intimate contact with the correcting mold, and the temperature of the mold is adjusted to a required temperature by the temperature sensor and the temperature adjusting source. If the correcting mold is made of ceramic, such mold is not heated by high frequencies from the induction heating source because the magnetic permeability of the mold is 1.5 or less. Therefore, the mold can be kept precisely at a required temperature only by adjusting the mold temperature adjusting device to a predetermined temperature.




Precise, quick, and reliable corrective tempering of a rolling element can be implemented by the corrective tempering apparatus of the invention while utilizing this function of the mold temperature adjusting device. That is,




(1) If the mold temperature adjusting device is set to a temperature that will adjust the mold temperature in such a manner a rolling element, which is a workpiece heated by the induction heater, is not thermally expanded to be in intimate contact with the mold, the workpiece can be set in the mold quickly under low forcing pressure.




Further, the induction-heated workpiece is cooled through conduction of the heat thereof to the ceramic mold whose temperature has been adjusted by the mold temperature adjusting device, which in turn allows the workpiece to be dropped naturally from the mold due to thermal shrinkage. As a result, the workpiece is no longer required to be forcibly extracted out of the mold with an extracting press. Hence, the temperature of the ceramic mold is controlled independently by the mold temperature adjusting device, which in turn allows the operation of setting the workpiece in and taking the workpiece out of the mold to be completed within an extremely short time. This is a remarkable advantage for a continuous process.




(2) In the corrective tempering apparatus of the invention, a ratio of volume between a workpiece to be treated and a ceramic mold is set to 1 to 100 or so from the viewpoint of strength. However, when heat treatment is performed only by induction heating without employing the mold temperature adjusting device, induction heating efficiency is reduced because the heat conduction from the induction-heated workpiece to the non-induction-heated ceramic mold is large. Further, an inconsistent temperature distribution between a workpiece portion that is in contact with the mold and a workpiece portion remote from the mold brings about a problem of inconsistent product quality. If, on the other hand, the temperature of the ceramic mold is controlled independently by the mold temperature adjusting device, efficient and uniform induction heating can be implemented. Thick-walled annular bodies, in particular, are more susceptible to tempering quality inconsistency with larger difference between the mold temperature and the workpiece temperature at the time of heating. In such a case, tempering quality inconsistency can be suppressed as small as possible by heating the rolling element mainly through conduction heating from the mold with the mold temperature being kept at a high temperature by the mold temperature adjusting device. That is, by adjusting the ratio of induction heating to conduction heating, heat treatment conditions optimal to the shape of the workpiece and the treatment tact can be selected.




Next, preferred embodiments of the invention will be described.




In a first embodiment of the invention shown in

FIG. 1

, a rolling element


1


A has a flat doughnutlike shape with an outer diameter of 40 mm, an inner diameter of 18 mm, and a thickness of 1.2 mm, and is made of a high carbon bearing steel (SUJ2 according to Japanese Industrial Standard) containing 0.95 to 1.10% of carbon. The hardness of the rolling element


1


A after hardening is HRC


66


. The rolling element


1


A that has been hardened was subjected to a warpage correcting treatment to correct the warpage produced during the hardening. The warpage correcting treatment was carried out by interposing the rolling element


1


A between heated upper and lower molds


2


,


3


and holding the element


1


A for a predetermined time with a pressure P equal to 1 ton applied from both top and bottom.





FIG. 2

shows deformation correcting temperature, i.e., maximum temperature reached by the rolling element


1


A (hereinafter referred to as the “product temperature”) in function of the amount of warpage of the rolling element


1


A with heating and pressuring time as a parameter. That is,

FIG. 2

shows the results of measurements made when the rolling element


1


A made of a bearing steel was subjected to a corrective tempering treatment by pressure. The initial amount of warpage of the rolling element


1


A before the treatment was 0.43±0.09 mm. As is apparent from

FIG. 2

, a satisfactory deformation correction was made by heating the product to 250° C. or more. That is, by heating the product to 250° C. or more, a warpage requirement of the product of 0.2 mm or less (the maximum allowable warpage) was met for a heating and pressuring time not exceeding 6 minutes.





FIG. 3

shows product temperature in function of rolling element


1


A hardness with the heating and pressuring time as a parameter in the aforementioned case. As is apparent from

FIG. 3

, the higher the mold temperature and the longer the heating and pressuring time, the lower the hardness. Therefore, a satisfactory deformation correction can be made within a range A defined in FIG.


3


. The range A ensures for the rolling element a hardness of HRC


56


or more with pressure being applied for such a short time as not exceeding 6 minutes.





FIG. 4

shows a second embodiment of the invention. An annular rolling element


1


B (e.g., the outer race of a rolling bearing) is heated and pressured by applying a pressure P from sideways (orthogonal to the axis of the rolling element) using a correcting split mold


5


that has already been heated to a predetermined temperature. In this case, the deformation of the outer diameter is corrected by binding the outer diameter surface of the rolling element


1


B. It may be noted that deformation correction using the split mold can be applied also to the doughnutlike rolling element


1


A, which is the first embodiment.





FIG. 5

shows a third embodiment of the invention. The annular rolling element


1


B is forced into a hole


7


of a die


6


to correct deformation. The die


6


has predetermined dimensions and serves as a correcting mold. The rolling element


1


B has the deformation of the outer diameter thereof corrected with a pressure applied from sideways while passing though the tapered portion


8


of the already heated hole


7


.





FIG. 6

shows a fourth embodiment of the invention. The outer race (or the inner race) of a ball bearing


1


C, which is a rolling element, has the deformation thereof produced by hardening corrected. In this case, the deformation is corrected by not only applying a pressure P to both end faces of the outer race of the ball bearing


1


C with already heated cylindrical pressing molds


10


,


10


, but also pushing an already heated mold


11


, which is a tapered shaft or a straight shaft, into the center bore of the outer race of the ball bearing


1


C. As a result of this operation, the warpage on the end faces of the outer race of the ball bearing


1


C as well as the deformation of the inner diameter thereof can be corrected simultaneously.




Further, if the warpage on the end faces is not so serious, only one mold


10


may be used in order to push the outer race of the ball bearing


1


C so as to allow the already heated mold


11


to be inserted into the outer race, instead of causing both sides of the outer race to be pressured by the already heated pressing molds


10


,


10


. In this case, the other pressing mold


10


is abutted against one end face of the outer race of the ball bearing


1


C through, e.g., a spring and is used only for heating the outer race of the ball bearing


1


C. Thus, the other pressing mold


10


may not necessarily be required to be used.





FIG. 7

shows a fifth embodiment of the invention. The deformation of the outer diameter of the rolling element


1


B is corrected by inserting the rolling element


1


B into a pressuring mold


16


made of ceramic (e.g., alumina, SiC, Si


3


N


4


, or diamond), thereafter heating the rolling element


1


B using an inductor coil


19


arranged outside the pressuring mold


16


, so that the deformation of the outer diameter can be corrected by the fitting force as well as the pressuring force produced between the rolling element


1


B and the pressuring mold


16


by the thermal expansion of the rolling element


1


B.




In either one of the aforementioned embodiments, not only the amount of deformation such as warpage can be controlled within a prescribed value corresponding to the size of a rolling element, but also hardness can be maintained at HRC


56


or more by a quick treatment.




It may be noted that an exemplary method of measuring the amount of warpage is shown in

FIGS. 8A and 8B

.





FIG. 8A

shows a case where the amount of deformation of the doughnutlike rolling element


1


A is measured. The amount of vertical movement of one end of the rolling element


1


A is measured with a dial gauge


14


by placing the rolling element


1


A on a surface plate


12


and biasing the opposite end of the rolling element


1


A intermittently with a finger tip with the outer diameter surface of the rolling element


1


A held by a locating ring


13


to prevent horizontal displacement.





FIG. 8B

shows a case where the amount of deformation of the annular rolling element


1


B is measured. The amount of deformation of the outer diameter is measured with the dial gauge


14


by rotating the rolling element


1


B in such a manner as shown in

FIG. 8B

while placing the rolling element


1


B on the surface plate


12


, bringing one end of the outer diameter surface of the rolling element


1


B into contact with a V block


15


fixed on the surface plate


12


at two points, and bringing the outer diameter surface on the other end into contact with the dial gauge


14


at one point.




It may be noted that the method of heating the heating and pressuring mold in each of the aforementioned embodiments is not particularly limited. A method in which a mold whose heat capacity is large is heated in a furnace in advance, a method in which a mold incorporating a heating source therein is heated by the heating source, an induction heating method, or a like method may be selected arbitrarily.




Still further, it is required that a mold already heated to a predetermined temperature be kept heated for a predetermined time (within 6 minutes). Therefore, the heated mold is placed in a heated atmosphere so that correction by pressure may be effected in such heated atmosphere.




Still further, correction by pressure may also be effected by using a pressuring mold made of ceramic and heating the rolling element through induction heating from outside such pressuring mold.




Next, corrective tempering apparatuses according to the invention will be described.





FIG. 9

is a first embodiment of the corrective tempering apparatus according to the invention. A cylindrical ceramic mold


22


whose magnetic permeability is 1.5 or less is set in a main body


21


of a corrective tempering apparatus


20


. A workpiece W, which is an annular rolling element, is inserted into the inner diameter surface of the mold


22


with the outer diameter surface thereof bound. Induction heating coils


23


serving as workpiece heating device are arranged on both upper and lower end faces of the mold


22


in proximity. In this case, the mold


22


is made as thin as possible so that the induction heating coils


23


can be arranged as close to the workpiece W to be heated as possible. In addition, each coil has two turns so that the workpiece W can be heated uniformly from both ends thereof by induction heating. The inner diameter of each coil


23


is made slightly larger than the inner diameter of the mold


22


.




A mold temperature adjuster


24


serving as a mold temperature adjusting device for adjusting the temperature of the mold


22


is arranged outside one of the heating coils


23


, which is the induction heating source, in the radial direction of the coil


23


so as to be in intimate contact with the upper end face of the ceramic mold


22


. The mold temperature adjuster


24


of this embodiment is formed into a flat doughnutlike shape. The mold temperature adjuster


24


includes a steel (SC) panel


25


, a temperature adjusting source


26


, and a not shown temperature sensor


27


. The steel panel


25


is used as a conducting member for conducting heat satisfactorily. The temperature adjusting source


26


such as an electric heater or a heat medium solution and the temperature sensor


27


such as a thermocouple are incorporated in the mold temperature adjuster. The upper surface of the mold temperature adjuster is covered with an insulating material


28


. The flat surface of the steel panel


25


is arranged so as to be in intimate contact with the flat surface of the mold


22


.




Up to a mold temperature of about 300° C., the mold temperature adjuster


24


is of such type that a heat medium oil is circulated in a coil-like groove formed inside the mold temperature adjuster


24


or that an electric heater is embedded inside the mold temperature adjuster


24


. If the mold temperature exceeds 300° C., it is preferred that the mold temperature adjuster


24


be of the latter type (electric heater type), because the heat medium oil type addresses a problem of heat deterioration. If cooling is required to keep mold temperature constant, water or oil is circulated in the coil-like groove formed in the mold temperature adjuster


24


. Temperature control is effected by making a changeover between the heating source and the cooling source based on a detection signal from the temperature sensor


27


embedded in the mold temperature adjuster


24


.




Although close to the induction heating coils


23


, the mold


22


is made of ceramic whose magnetic permeability is 1.5 or less and the mold


22


will not therefore be further heated by the lines of magnetic force produced by the induction heating coils


23


. Hence, the mold


22


temperature can be adjusted by the mold temperature adjuster


24


alone.




Not only a workpiece forcing tool


30


and a main cylinder


31


for vertically moving the workpiece forcing tool


30


are arranged at the upper end, but also a workpiece supporting tool


32


and a sub-cylinder


33


for vertically moving the workpiece supporting tool


30


are arranged at the lower end along the center shaft of the apparatus main body


21


.




Further, a workpiece W insertion port


36


and an insertion chute


37


are arranged on an upper side surface of the apparatus main body


21


, whereas a workpiece discharge cylinder


38


, a treated workpiece discharge port


39


, and a treated workpiece discharge chute


40


are arranged on a lower side surface of the apparatus main body


21


.




An operation of the corrective tempering apparatus


20


will be described next.




The workpiece forcing tool


30


and the workpiece supporting tool


32


are first set in the upper and lower evacuated positions, respectively.




The workpiece supporting tool


32


is elevated to the workpiece insertion port


36


on the upper side of the apparatus by operating the sub-cylinder


33


on the lower side of the apparatus. Then, a workpiece W is charged onto the workpiece supporting tool


32


from the insertion chute


37


via the workpiece insertion port


36


. It is so designed that the charged workpiece W is automatically aligned with the mold


22


.




Once the workpiece W has been charged onto the workpiece supporting tool


32


, the workpiece forcing tool


30


is lowered by operating the main cylinder


31


so that the workpiece W is clamped between both tools


30


,


32


. The tools


30


,


32


are lowered with the workpiece W horizontally clamped therebetween, pass through the upper induction heating coil


23


, and are forced into the middle portion of the mold


22


from the upper tapered portion of the inner diameter surface of the ceramic mold


22


. After being forced, the workpiece forcing tool


30


is elevated, whereas the workpiece supporting tool


32


is lowered to move away from the workpiece W. The workpiece W is subjected to induction heating by operating the induction heating coils


23


under this condition. It is preferred that the maximum workpiece W temperature range from 250 to 500° C. and that the induction heating time for keeping the workpiece at such maximum temperature not exceed 30 seconds. Even if the workpiece W is heated for more than 30 seconds, the effect of tempering and deformation correcting capability will not be improved. That is, heating for a time exceeding 30 seconds will be wasted.




Upon end of the heating, the workpiece forcing tool 30 is lowered to a large extent to push the workpiece W out toward the lower portion of the mold


22


by operating the main cylinder


31


, and the workpiece W is received by the elevated workpiece supporting tool


32


. Then, the workpiece supporting tool


32


is lowered so that the workpiece W is located at the workpiece discharge port


39


. The workpiece W on the workpiece supporting tool


32


is thereafter thrown out onto the workpiece discharge port


39


and sent to the discharge chute


40


by operating the workpiece discharge cylinder


38


. As a result of these steps, one cycle of the operation is completed.




If induction heating efficiency is improved, or if a small-capacity high frequency power source is used for the workpiece, it is suggested that induction heating be effected by interposing highly permeable members between the workpiece forcing tool


30


and a corresponding contact surface of the workpiece W and between the workpiece supporting tool


32


and the corresponding other contact surface of the workpiece W with the workpiece interposed between both tools. By first induction-heating the highly permeable members to a high temperature and then by utilizing the heat conduction effect of the induction heating, the workpiece W is heated with high efficiency.




Further, according to the corrective tempering apparatus


20


, the workpiece W can also be subjected to an ironing process inside the ceramic mold


22


during the heating in order to improve the surface roughness of the outer diameter surface of the workpiece W.





FIGS. 10

to


16


show various embodiments of the invention, which are modifications of the apparatus, and modes of arrangement of the correcting mold


22


, the induction heating coil


23


, and the mold temperature adjuster


24


, in particular. It may be noted that the same or like parts and components are denoted as the same reference numerals.





FIG. 10

shows a second embodiment of the corrective tempering apparatus. The outer diameter of the workpiece W is corrected by induction heating based on an inner diameter heating method. The mold


22


is arranged outside the induction heating coil


23


in the radial direction of the coil. The mold temperature adjuster


24


is arranged so as to be in intimate contact with the outer diameter surface of the mold


22


.





FIG. 11

shows a third embodiment of the corrective tempering apparatus. The outer diameter of the workpiece W is corrected by induction heating based on an outer diameter heating method. The induction heating coil


23


is arranged outside the mold


22


in the radial direction of the mold, the mold


22


having the workpiece W forced thereinto. The mold temperature adjusters


24


are arranged so as to be in intimate contact with the mold


22


and so as to be distant from the coil


23


in the axial direction of the coil so that the mold temperature adjusters


24


are less affected by high frequencies.





FIG. 12

shows a fourth embodiment of the corrective tempering apparatus. The inner diameter of the workpiece W is corrected. A collet type correcting mold


22


is employed. The inner diameter of the workpiece W is corrected by expansion while inserting the mold


22


into the inner diameter surface of the workpiece W and forcing a collet into the mold


22


. The induction heating coil


23


is arranged outside the workpiece W. The mold temperature adjusters


24


are arranged outside the mold


22


in the axial direction of the coil.





FIGS. 13A and 13B

show a fifth embodiment of the corrective tempering apparatus. The inner diameters of the workpieces W are corrected.

FIG. 13A

shows the molds


22


which is made of a material whose linear expansion coefficient is larger than those of the workpieces W.

FIG. 13B

shows the mold


22


which is heated by the induction heating coil


23


arranged outside the outer diameter surface of each workpiece W is thermally expanded to come in intimate contact with the inner diameter of the workpiece, so that the inner diameter of each workpiece is heated and pressured.





FIG. 14

shows a sixth embodiment of the corrective tempering apparatus. Both the inner and outer diameter surfaces of the workpiece W are corrected. This is an example in which the inner and outer diameter surfaces are corrected simultaneously using a collet mold


22


A for the inner diameter surface and a cylindrical mold


22


B for the outer diameter surface. The induction heating coils


23


are arranged on both upper and lower end faces of both molds. The mold temperature adjuster


24


is arranged outside the coils


23


in the radial direction of the coils


23


.





FIGS. 15A and 15B

each shows a seventh embodiment of the corrective tempering apparatus. The deformation of the workpiece W is corrected taperingly. This is an example in which not only the deformation is corrected by tapering, but also the outer and inner races of conical bearings are fabricated. The inner diameter surface of the mold


22


is tapered. A pressing tool


41


is employed, the tool


41


pressuring the workpiece W inserted into the mold


22


in the axial direction. The induction heating coils


23


are arranged on both upper and lower end faces of the tapered mold


22


. The mold temperature adjuster


24


is arranged outside the coils


23


in the radial direction of the coils.





FIG. 16

shows an eighth embodiment of the corrective tempering apparatus. A plurality of workpieces W are processed at once using only one mold. The mold


22


is a vertically elongated cylindrical body. The workpieces W are inserted inside the mold


22


while placed one upon another in the axial direction of the mold. The outer diameter surfaces of the thus inserted workpieces are subjected to a continuous corrective tempering treatment. The outer diameter surfaces of the workpieces are bound by heating to be corrected by tempering and are thereafter separated from the mold by utilizing the shrinkage of the workpieces W brought about by cooling. The induction heating coils


23


are arranged in a plurality of rows so as to enclose the outer diameter surface of the cylindrical mold


22


. The mold temperature adjusters


24


are arranged outside these coils


23


in the axial direction of the coils.




While the mold temperature adjusters are arranged so as to neighbor the correcting mold in the aforementioned apparatus and their modifications, the mold temperature adjusters may also be arranged inside the mold.




A comparative corrective tempering test carried out using the aforementioned corrective tempering apparatuses


20


will be described.




Thin-walled annular rolling elements made of steel were used as workpieces W. The steel grades selected were SUJ2, SCR420, SUS440C. These workpieces W were heated to 840° C. and kept at such temperature for 30 minutes. Then, the workpieces W were subjected to hardening using a hardening oil at 60° C. and were hardened to obtain specimens.




A total of five corrective tempering ceramic molds


22


were used. Their inner diameters were: 47.000 mm, 50.150 mm, 65.150 mm, 61.700 mm, and 62.200 mm.




A total of four mold temperatures were set by the mold temperature adjusters


24


. The four mold temperatures were: 55° C., 200° C., 400° C., and 500° C.




A total of six maximum workpiece W temperatures were set by the induction heating coil


23


. The six maximum workpiece W temperatures were: 200° C., 250° C., 300° C., 400° C., 500° C., and 600° C.




Table 1 shows evaluation items, evaluation criteria, and judgment symbols per evaluation item for the comparative test.

















TABLE 1














Tempering








Standard-





Rapid




Consistency








izing





Treatment




(ΔH


v


)







Degree of




rate of




Surface




Time (sec)




(surface






Evalu-




Correction




dimensions




Roughness




(including




hardness






ation




(%)




(%)




(Ra)




set time)




dispersion)











A




80≦




80≦




<0.1




 0-35




 0-16






B




60-80




50-80




0.1-0.2




35-60




16-31









(inclusive)






C









30-50









 60-360











D




<60




<30




not




360≦




31≦









changed











(Note) Evaluation is ranked with the following degrees:










A: very superior










B: superior










C: usable










D: not-usable.













The correcting degree of deformation (degree of correction) in the inner/outer diameter of a workpiece W was calculated in accordance with the following equation.












Degree





of





correction

=







Pre


-


correction





roundness



-




Post


-


correction





roundness





Pre


-


correction





roundness


×
100











Further, the dimension standardizing rate was calculated in accordance with the following equation.














Dimension




standardizing




rate



=







Pre


-


tempering





dimensional




dispersion



-





P

ost



-


tempering





dimensional




dispersion





Pre


-


tempering





dimensional





dispersion


×
100











The object of the corrective tempering according to the invention is that the treated workpieces W satisfy the following conditions.




The correcting degree of deformation of the inner/outer diameter is 60% or more.




The rate of standardizing the dimension of the inner/outer diameter is 30% or more.




The surface roughness of the corrected surface is less than Ra 0.2 μm.




The rapid treatment time is within 360 seconds (6 minutes).




The surface hardness is HRC


56


or more.




Tables


2


A to


2


D show the test conditions and the test results.




The column for the degree of working (%) in Table


2


A shows a degree of working δ, which is calculated in accordance with the following equation.






δ={


D/d


(1+


α•T


)−1}×100  (1)






where D: Outer diameter of a workpiece before corrective tempering (mm)




d: Inner diameter of a correcting mold (mm)




a: Linear expansion coefficient of a steel grade (e.g., 0.000012 for SUJ2)




T: Maximum workpiece temperature (°C.)


















TABLE 2A
















Degree of








Steel





Dimensions




Working






















Species




No.




Inner




Outer




Height




250° C.




500° C.




S




V




S/V

























Inventive




SUJ2




A1




43.78




46.81




7.00









0.20




1029




1509




0.68






Examples





A2




43.78




46.95




7.00




0.20




0.50




1032




1581




0.65








A3




43.78




47.00




7.00




0.30




0.60




1033




1606




0.64








A4




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








A5




43.78




47.17




7.00




0.66




0.96




1037




1694




0.61








A6




43.78




47.20




7.00




0.73




1.03




1037




1710




0.61







SUJ2




B1




43.78




47.15




7.00




0.62




0.93




1036




1685




0.62








B2




43.78




47.20




7.00




0.73




1.03




1037




1710




0.61







SCR420




C1




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








C2




43.78




47.20




7.00




0.73




1.03




1037




1710




0.61







SUS440C




D1




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








D2




43.78




47.20




7.00




0.73




1.03




1037




1710




0.61







SUJ2




E1




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








E2




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








E3




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








E4




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62







SUJ2




F1




42.00




50.26




6.40




0.62




0.92




1010




3829




0.26








F2




42.00




50.26




6.40




0.62




0.92




1010




3829




0.26








F3




42.00




50.26




6.40




0.62




0.92




1010




3829




0.26








F4




42.00




50.26




6.40




0.62




0.92




1010




3829




0.26







SUJ2




G1




55.00




65.35




8.00




0.61




0.91




1642




7823




0.21








G2




55.00




65.35




8.00




0.61




0.91




1642




7823




0.21








G3




55.00




65.35




8.00




0.61




0.91




1642




7823




0.21








G4




55.00




65.35




8.00




0.61




0.91




1642




7823




0.21







SUJ2




H1




50.00




61.90




9.00




0.63




0.93




1749




9408




0.19








H2




50.00




61.90




9.00




0.63




0.93




1749




9408




0.19








H3




50.00




61.90




9.00




0.63




0.93




1749




9408




0.19







SUJ2




I1




41.50




62.40




7.50




0.62




0.92




1470




12785 




0.11








I2




41.50




62.40




7.50




0.62




0.92




1470




12785 




0.11






Comparative




SUJ2




J1




43.78




46.70




7.00




−1.34




−0.04




1026




1452




0.71






Examples





J2




43.78




46.72




7.00




−0.30




0.00




1027




1462




0.70








J3




43.78




47.23




7.00




0.79




1.09




1038




1725




0.60







SUJ2




K1




50.00




61.90




9.00




0.63




0.93




1749




9408




0.19







SUJ2




L1




41.50




62.40




7.50




0.62




0.92




1470




12785 




0.11








L2




41.50




62.40




7.50




0.62




0.92




1470




12785 




0.11







SUJ2




M1




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








M2




43.78




47.20




7.00




0.73




1.03




1037




1710




0.61







SUJ2




N1




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








N2




43.78




47.20




7.00




0.73




1.03




1037




1710




0.61







SUJ2




O1




43.78




47.15




7.00




0.62




0.92




1036




1684




0.62








O2




43.78




47.20




7.00




0.73




1.03




1037




1710




0.61




























TABLE 2B
















Mold











Dimensions







Steel





Pre-




(Correcting




Corrective Tempering



















Species




No.




treatment




Part)




Mold Temp.




Heating Temp.




Heating Time























Inventive




SUJ2




A1




Lathe




47.000




 55° C.




500° C.





 3 sec.







Examples





A2







250° C.





 3 sec.








A3







300° C.




×




10 sec.








A4







400° C.





30 sec.








A5







500° C.








A6










SUJ2




B1




CRF




47.000




 55° C.




400° C.




×




 3 sec.








B2







500° C.





10 sec.







SCR420




C1




Lathe




47.000




 55° C.




400° C.




×




 3 sec.








C2







500° C.




×




10 sec.







SUS440C




D1




Lathe




47.000




 55° C.




400° C.




×




 3 sec.








D2







500° C.




×




10 sec.



















SUJ2




E1




Lathe




47.000




 55° C.




Induction Heating




 3 sec.








E2






200° C.




400° C.




 3 sec.








E3






400° C.





 2 sec.








E4






500° C.




Only Conduction Heating




20° C.












400° C.







SUJ2




F1




Lathe




50.150




 55° C.




Induction Heating




10 sec.








F2






200° C.




400° C.




 7 sec.








F3






400° C.





 6 sec.








F4






500° C.




Only Conduction Heating




30 sec.












400° C.







SUJ2




G1




Lathe




65.150




 55° C.




Induction Heating




25 sec.








G2






200° C.




400° C.




15 sec.








G3






400° C.





10 sec.








G4






500° C.




Only Conduction Heating




40 sec.












400° C.







SUJ2




H1




Lathe




61.700




200° C.




Induction Heating




25 sec.








H2






400° C.




400° C.




20 sec.








H3






500° C.




Only Conduction Heating




60 sec.












400° C.







SUJ2




I1




Lathe




62.200




400° C.




Induction Heating 400° C.




27 sec.








I2






500° C.




Only Conduction Heating




80 sec.












400° C.




















Comparative




SUJ2




J1




Lathe




47.000




 55° C.




250° C.




×




 3 sec.







Examples





J2







500° C.





 7 sec.















J3





Impossible for Forcing



















SUJ2




K1




Lathe




61.700




 55° C.




Induction Heating 400° C.




30 sec.







SUJ2




L1




Lathe




62.200




 55° C.




Induction Heating 400° C.




30 sec.








L2






200° C.




Induction Heating 400° C.




30 sec.





















SUJ2




M1




Lathe




47.000




 55° C.




200° C.




×




 3 sec.









M2









30 sec.







SUJ2




N1




Lathe




47.000




 55° C.




600° C.




×




 3 sec.








N2









30 sec.
















SUJ2




O1




Lathe




Bracing Tempering








O2





200° C.    2 Hr


























TABLE 2C













Outer Diameter

















Steel





Roughness




Inner Diameter



















Species




No.




Correction




Dispersion




(Ra)




Correction




Dispersion






















Inventive




SUJ2




A1




B




A




B




B




C






Examples





A2




250° C. Heated Element




B  C




B




250° C. Heated Element




C  B








A3




300° C. Heated Element




B  B




B




300° C. Heated Element




B  B








A4




400° C. Heated Element




A  A




A




400° C. Heated Element




B  C








A5




500° C. Heated Element




A  A




A




500° C. Heated Element




B  C








A6






A
















SUJ2




B1




All A




All A








B2



















SCR420




C1




400° C. Heated Element




A  A




A




400° C. Heated Element




B  C








C2




500° C. Heated Element




A  A




A




500° C. Heated Element




B  C







SUS440C




D1




400° C. Heated Element




A  A




A




400° C. Heated Element




B  C








D2




500° C. Heated Element




A  A




A




500° C. Heated Element




B  C







SUJ2




E1




A




Impossible




A




B




Impossible








E2





due to same






due to same








E3





dimensions






dimensions








E4







SUJ2




F1




A




Impossible




A




B




Impossible








F2





due to same






due to same








F3





dimensions






dimensions








F4







SUJ2




G1




A




Impossible




A




B




Impossible








G2





due to same






due to same








G3





dimensions






dimensions








G4







B







SUJ2




H1




A




Impossible




A




B




Impossible








H2





due to same






due to same








H3





dimensions






dimensions







SUJ2




I1




A




Impossible




A




B




Impossible








I2





due to same






due to same










dimensions






dimensions






Comparative




SUJ2




J1




250° C. Heated Element




D  D









250° C. Heated Element




D  D






Examples





J2




500° C. Heated Element




D  D









500° C. Heated Element




D  D














J3




All D due to being impossible for forcing



















SUJ2




K1




A




Impossible




A




B




Impossible







SUJ2




L1




A




Impossible




A




B




Impossible








L2





due to same






due to same










dimensions






dimensions







SUJ2




M1




D




D




A




D




B








M2




D




D




A




D




B







SUJ2




N1




A




A




A




B




D








N2






A







SUJ2




O1




B




D









D




D








O2




































TABLE 2D















Rapid







Steel





Hardness




Tempering




Treatment







Species




No.




(HRC)




Consistency




Time





























Inventive




SUJ2




A1




HRC




A




A






Examples





A2




56-66








A3








A4








A5








A6







SUJ2




B1





A




A








B2







SCR420




C1





A




A








C2







SUS440C




D1





A




A








D2







SUJ2




E1





A




A








E2








E3








E4







SUJ2




F1





B




A








F2





A








F3








F4






B







SUJ2




G1





B




A








G2








G3





A








G4






B







SUJ2




H1





B




A








H2








H3





A




C







SUJ2




I1





B




C








I2





A




C






Comparative




SUJ2




J1




HRC




A











Examples





J2




56-66














J3




All D due to being








impossible for forcing

















SUJ2




K1




HRC




D




A







SUJ2




L1




56-66




D




A








L2





D




B







SUJ2




M1





A




A








M2







SUJ2




N1




HRC




A




A








N2




48-52







SUJ2




O1




HRC




A




D








O2




56-66















Incidentally, the degree of working for a workpiece to be corrected by the mold in these tests was calculated in accordance with the following equation.












Degree





of





working






(
%
)


=







Outer





diameter






of





workpiece




-




Inner





diameter






of





mold






Inner





diameter





of





mold


×
100











The lower limit of the degree of working is the minimum degree of working that permits the correction of the deformation of a workpiece. If the degree of working is calculated based on the inner diameter of a mold and is found to be less than the lower limit, then the workpiece cannot be corrected by such a mold. On the other hand, the upper limit of the degree of working is the maximum degree of working that permits the forcing of a workpiece into a mold. If the degree of working is calculated based on the inner diameter of a mold and is found to be more than the upper limit, the workpiece cannot be forced into such a mold because the outer diameter of the workpiece (at room temperature) is too large for the inner diameter of the mold.




The upper limit of the degree of working δ is determined in the following way.




Let it be assumed that the inner diameter d of a correcting mold is set constant and that the maximum outer diameter of a workpiece permitting the workpiece to be forced into the correcting mold before corrective tempering is D


0


. Since equation (1) expressing the degree of working δ can be converted into






δ={(


D−d


)/


d+DαT/d}×


100


=K




1




+K




2




T


  (2)






(where K


1


=100×(D−d)/d, K


2


=100Dα/d)




Therefore, a curve defined by K


1


=K


10


, K


2


=K


20


that are obtained by substituting D=D


0


into K


1


, K


2


in equation (2) expresses δ


max


(%) permitting the forcing of the workpiece into the mold. That is, the upper limit of the degree of working is defined by






δ


max




=K




10




+K




20




T


  (3)






The outer diameter of specimen A


6


was the limit that permits a specimen to be forced into the mold in this invention. The upper limit δ of the degree of working, i.e., δ


max


(%) of equation (3) at maximum workpiece temperatures of 250° C. and 500° C. can be calculated as follows from Table


2


A.




Since the linear expansion coefficient α of the steel grade SUJ2 is 0.000012,






δ


max


={47.20/47.000(1+0.000012×250)−1}×100 0.73%






at 250° C.






δ


max


={47.20/47.000(1+0.000012×500)−1}×100=1.03%






at 500° C.




Further, K


10


, K


20


are




K


10


=100×(47.20−47.0) /47.0 ≈0.43




K


20


=100×47.2×α/47.0≈100.4α




It may be noted that K


20


=1.21×10


−3


when α=0.000012 is substituted.




K


10


, K


20


were obtained on a test basis assuming that d=47.00 and the like. Even taking into account the fact that the roundnesses of hardened workpieces are not consistent and the fact that the dimensions of workpieces and correcting molds are changed, K


10


, K


20


can be defined as follows.




K


10


=0.43±0.03




K


20


=(100. 4±0.2) α




While differences between room temperatures and 0° C. and fluctuations brought about by the temperature in the inner diameter d of a correcting mold have been neglected in the aforementioned equations (1) to (3) and the like, all these values are very small in view of the elastic deformability of a workpiece and the like. Accordingly, it can be said that substantially reliable approximations can be provided by the aforementioned equations and the like.




It was verified that all the combinations of the outer diameters of the workpieces and the inner diameters of the molds of the invention were within the range between the upper limit δ (=δ


max


) and the lower limit δ (=0.20) and that some of Comparative Examples were out of that range (specimen J3 exceeding the upper limit δ, so that specimen J


3


cannot be forced into the mold, and specimens J


1


and J


2


were smaller than the lower limit δ so that specimens J


1


and J


2


cannot be corrected).





FIG. 17

is a graph showing the results of the corrective tempering test made to compare Inventive Examples A


1


to A


6


with Comparative Examples M


1


, M


2


and N


1


, N


2


. The abscissa indicates the maximum workpiece temperature, whereas the ordinate indicates the correcting degree of deformation and the workpiece surface hardness (HRC).




The correcting degree of deformation differs from every heating time and is improved as increasing maximum workpiece temperature. When the maximum workpiece temperature exceeds 500° C., the correcting degree of deformation is no longer improved. The passable lower limit is 60% in the graph. A more preferable passable lower limit is 80%.




It is understood from these results that a maximum workpiece temperature range satisfying both a passable surface hardness limit of HRC


56


within 30 seconds of the heating time and a passable degree of correction of 60% or more is between 250° C. and 500° C.





FIG. 18

is a plot illustrating a relationship between the maximum workpiece temperature and the dimension (outer diameter) standardizing rate from the test results of Inventive Examples A


1


to A


6


in Tables


2


A to


2


C. The dimension standardizing rate increases as the dimensional dispersion after tempering decreases, compared with the dimensional dispersion before tempering. Therefore, the effect of correcting for making the dimensions consistent are significant. It is understood from this graph that the effect of correcting are satisfactory within a maximum workpiece temperature range of from 250 to 500° C. and that the effect of correcting are more satisfactory within a range of from 300 to 500° C., or still more satisfactory within a range of from 380 to 500° C.





FIG. 19

is a plot illustrating a relationship between the degree of working and the surface roughness Ra (μm) of the deformed surfaces (the outer diameter surfaces in this case) corrected by the correcting mold from the test results of Inventive Examples A


1


to A


6


in Tables


2


A and


2


C.




If the worst surface roughness permitting correction is set to Ra 0.2 μm, the degree of working may be 0.2% or more. Inventive Examples A


1


to A


6


all satisfy this degree of working. Further, it is understood from

FIG. 19

that the degree of working must, more preferably, be 0.6% or more (Ra 0.1 μm or less).





FIG. 20

is a plot illustrating a relationship between the degree of working (in abscissa) and the correcting degree of deformation from the test results of Inventive Examples A


1


to A


6


and Comparative Examples J


1


and J


2


in Tables


2


A and


2


B.




It is apparent also from these results that a correcting degree of deformation of 60% or more is obtained only when the degree of working is 0.2% or more. In other words, it is apparent that the lower limit of the degree of working is 0.2%.





FIG. 21

is a plot illustrating a relationship between the maximum workpiece temperature (in abscissa) and the degree of working from the test results of Inventive Examples A


1


to A


6


and Comparative Examples J


1


to J


3


in Tables


2


A and


2


C. In

FIG. 21

, the horizontal line indicating a degree of working of 0.2% is the lower limit of the degree of working, i.e., the minimum degree of working that permits correction of a workpiece. Further, while the lines of the degrees of working plotted by each of Inventive Examples A


1


to A


6


and Comparative Examples J


1


to J


3


are presented in the graph, it was found out that the upper limit of the degree of working, i.e., the maximum degree of working permitting a workpiece W to be forced into a mold is defined by the line of the degree of working of Inventive Example A


6


in this embodiment as described above. That is, the maximum degree of working is determined by the curve obtained within the range of K


10


=0.43±0.03, and K


20


=(100.4±0.2) α in equation (3).




That is, it is possible to increase the upper limit of the degree of working δ up to the value so defined as described above from the lower limit of the degree of working, 0.20%, within the maximum workpiece temperature range of from 250 to 500° C. The shaded area in the middle of

FIG. 21

is the maximum workpiece temperature and the degree of working range permitting the workpiece W to be forced into the mold while satisfying all such effects of the invention as a surface hardness of HRC


56


or more, a correcting degree of deformation of 60% or more, a dimension standardizing rate of 30% or more, and a corrected surface roughness of less than Ra 0.2 μm.





FIG. 22

shows how the shape of a workpiece W affects corrective tempering.




Differences ΔH


v


(surface hardness dispersion) between the largest value and the smallest value in the surface hardness (H


v


) of the workpiece W and ratios of the contact surface area between the mold


22


and the workpiece W to the volume V (S/V ratio) of the workpiece W were plotted with the abscissa indicating the difference ΔH


v


and with the ordinate indicating the S/V ratio with respect to a plurality of specimens including Inventive and Comparative Examples denoted as respective reference symbols in Table


2


A. The mold temperature was set to different values from 55 to 500° C. using the mold temperature adjuster


24


. The workpieces W, which were the specimens, were heated through conduction heating from the mold


22


and through induction heating using the induction heating coil


23


either singly or in combination. It may be noted that the workpiece temperature was 400° C. and that the average surface hardness ranged from HRC


58


to


60


. The upper limit surface hardness dispersion ΔH


v


is 30 or less, or more preferably 16 or less. Further, a S/V ratio of 0.27 or more is required when induction heating is employed, and a S/V ratio of 0.1 or more is required when only conduction heating is employed.




As increasing the S/V ratio, the surface hardness dispersion ΔH


v


decreases in a heating method based mainly on induction heating and the treatment time is shortened. In this case, the mold temperature is low, so that the workpiece W can be set in the mold easily without thermal expansion. In addition, the workpiece W is cooled rapidly and is therefore naturally dropped after the treatment. This dispenses with the use of the extracting mold, which in turn contributes to increasing the life of the mold.




On the other hand, as decreasing the S/V ratio, the chances for employing a heating method based mainly on conduction increase, which provides the advantage of allowing large workpieces to be treated with less surface hardness dispersion. However, this heating method entails a long treatment time and makes the setting of a workpiece in and taking the workpiece out of a mold hard, which in turn makes it likely to reduce the life of the mold.




Another deformation correcting test will be described.




Separately from the aforementioned test, a test was carried out by subjecting workpieces W, which are the outer races of ball bearings, to a deformation correcting treatment in order to study a relationship between correcting energy and mold temperature. This another deformation correcting test will now be described.





FIGS. 23A and 23B

are a diagram showing a mold of a corrective tempering apparatus used for the test.




The workpieces W used in the test were the outer races of ball bearings, whose designations are


6808


,


6808


,


6212


, and


6312


made of SUJ2. A total of four S/V ratios, i.e., the ratio of the volume (V mm


3


) to the contact surface area (S mm


2


) were arranged. These four values are: 1, 0, 0.5, 0.25, and 0.17 for the above designations, respectively.




These outer races (workpieces W) were kept at 840° C. for 20 minutes, thereafter dipped into an oil bath for hardening, and then inserted into a split mold


50


(trisected) that had been heated to a predetermined temperature. The workpieces W were heated and pressured for a predetermined time by inserting the split mold


50


into an outer mold


51


, and then taken out of the mold


50


. Then, the roundnesses and hardnesses of these workpieces W were measured, and a comparison was then made with the roundnesses of these workpieces W after hardening and before the pressuring and heating of the corrective tempering.





FIG. 24

shows the results of these measurements.




The abscissa indicates the mold temperature measured by the mold temperature adjuster. The ordinate indicates the correcting energy. The correcting energy is calculated by the equation: Mold temperature (°C.)×Pressuring/heating time (sec)×10


−3


.

FIG. 24

shows that the workpiece W heating energy decreases as increasing S/V ratio, and also shows a S/V ratio of each workpiece W which can satisfy both a correcting degree of deformation of 60% or more and a surface hardness of HRC


56


or more. That is, the S/V ratio which allows satisfactory correcting results to be obtained is from 0.17 to 1.0.




As described in the foregoing, the corrective tempering methods for rolling elements according to the invention are characterized in that the hardening deformation of a rolling element made of steel is corrected by utilizing plasticity exhibited during the process of tempering the hard steel structure of the rolling element brought about by hardening. That is, the deformation correction is made by the method of heating (tempering) the steel rolling element having been subjected to hardening to 250 to 500° C. for a time not exceeding 6 minutes while applying pressure to the rolling element. As a result, the deformation of the rolling element can be corrected within a short period of time. In addition, not only the smallest hardness required for maintaining the rolling fatigue life of the rolling element, which is HRC


56


, can be ensured, but also the amount of warpage or deformation of the outer diameter or inner diameter of the rolling element required to ensure product accuracies can be kept within a prescribed value. The method in particular involves induction heating for heating the rolling element, and corrects the deformation of the rolling element by treating the rolling element for a time not exceeding 30 seconds at a degree of working ranging from 0.2 to the upper limit δ. Hence, according to the corrective tempering methods of the invention, corrective tempering can be completed within such an extremely short time as not exceeding 6 minutes in order to achieve a correcting degree of deformation of 60 % or more for inner and outer diameter deformations, a dimension standardizing rate of 30% or more for the inner and outer diameters, a corrected surface roughness of less than Ra 0.2 μm, and a surface hardness of HRC


56


or more. In addition, only a small number of tools and molds are required for a mass production of rolling elements, which is another advantage. Therefore, the invention is suitably applied to a highly efficient mass production of long-life and highly accurate rolling elements such as the inner and outer races as well as cages of rolling bearings. The corrective tempering apparatus for rolling elements according to the invention is characterized in that not only the induction heater is included as a heating source for heating a hardened rolling element to a desired temperature, but also the mold temperature adjusting device for adjusting the temperature of a mold that binds the rolling element is arranged. As a result of this construction, the rolling element can be treated within such an extremely short time as not exceeding 30 seconds through direct induction heating. In addition, fitting dimensions between the mold and the rolling element can be adjusted by freely controlling the mold temperature using the mold temperature adjusting device. Therefore, the rolling element can be set in and taken out of the mold easily as well as quickly. Hence, the corrective tempering apparatus of the invention can complete corrective tempering within such an extremely short time as not exceeding 30 seconds in order to achieve a correcting degree of deformation of 60 % or more for inner and outer diameter deformations, a dimension standardizing rate of 30% or more for the inner and outer diameters, a corrected surface roughness of less than Ra 0.2 μm, and a surface hardness of HRC


56


or more. In addition, only a small number of tools and molds are required for a mass production of rolling elements, which is another advantage. Therefore, the invention is suitably applied to a highly efficient mass production of long-life and highly accurate rolling elements such as the inner and outer races as well as cages of rolling bearings.



Claims
  • 1. An apparatus for correctively tempering a bearing component, comprising:an induction heater heating the bearing component to a desired temperature and including a heating coil; a mold made of ceramic material constraining at least one of an inner surface, an outer surface and both of end faces of the bearing component, the bearing component being at least one of a hardened cylindrical body, a hardened annular body and a hardened flat shaped body; and a mold temperature adjusting device arranged relative to the heating coil for adjusting a temperature of said mold by being in contact with an outer peripheral surface of said mold, said mold temperature adjusting device being positioned outside the heating coil in at least one direction of a radial direction and an axial direction of the heating coil wherein said mold temperature adjusting device is disposed apart from said heating coil.
  • 2. The apparatus according to claim 1, in which said mold temperature adjusting device is arranged outside said heating coil in the radial direction.
  • 3. The apparatus according to claim 1, wherein said mold temperature adjusting device adjusts the temperature of said mold by heating and cooling said mold.
  • 4. The apparatus according to claim 1, wherein said mold temperature adjusting device comprising:a conducting member for conducting heat, the conducting member being in contact with the outer peripheral surface of said mold; and a temperature adjusting source for heating and cooling said mold.
  • 5. The apparatus according to claim 4, wherein said conducting member is made of a steel panel.
  • 6. The apparatus according to claim 4, wherein said mold temperature adjusting device further comprising a temperature sensor incorporated therein.
Priority Claims (1)
Number Date Country Kind
6-199620 Aug 1994 JP
Parent Case Info

This is a divisional of Application No. 08/632,418 filed Apr. 24, 1996 now U.S. Pat. No. 6,093,268, the disclosure of which is incorporated herein by reference which is a 371 of PCT/JP95/01662 filed Aug. 23, 1995.

US Referenced Citations (4)
Number Name Date Kind
1894590 Ingersoll Jan 1933
4479833 Gessinger et al. Oct 1984
5410132 Gregg et al. Apr 1995
5591369 Matsen et al. Jan 1997
Foreign Referenced Citations (5)
Number Date Country
56-9217 B2 Feb 1981 JP
58-35575 B2 Aug 1983 JP
59-226118 Dec 1984 JP
62-37315 Feb 1987 JP
1252363 Aug 1986 SU