Method for annealing stamped components

Information

  • Patent Grant
  • 6217677
  • Patent Number
    6,217,677
  • Date Filed
    Monday, June 28, 1999
    25 years ago
  • Date Issued
    Tuesday, April 17, 2001
    24 years ago
Abstract
A process for forming a precision formed cup-shaped member includes stamping a blank into a cup-shaped member. The cup-shaped member is positioned onto a magnetic heating machine. A magnetic core is positioned adjacent a radius of the cup-shaped part on both a top side and a bottom side of the cup-shaped part. The part is heated with the magnetic heating machine so as to anneal the cup-shape part at the radius.
Description




FIELD OF THE INVENTION




The present invention relates to a method for annealing stamped components, and more particularly to a method for locally annealing sharp radii in precision formed housings, the housings being formed by a stamping process and made from a carbon or HSLA steel.




DESCRIPTION OF THE PRIOR ART




In an automatic transmission, several components are formed from carbon steel or HSLA steel. Torque transmission members include a number of drums which are stamped and splines are rolled into the cup-shaped outer periphery. Normally, the stamping displaces the grain structure of the steel thereby work hardening the part. This work hardening causes high stresses at the radius and slivering may occur within such drums. Typically, such parts are annealed in a furnace, wherein the entire part is heated to the appropriate temperature and the entire part is annealed, although only the stress areas require such annealing. This process requires a long cycle time to heat the entire part and anneals portions of the part for which it is not desired to be annealed and therefore softened.




The work hardening creates further problems in that the hardened portion creates areas of high stress that may contribute the fatigue and/or failure such as cracking, splintering or slivering of the material. Methods to control these problems include additional die stations to control and minimize the amount of displacement in a particular stamping operation. Alternatively, a steel having a lower carbon content may be used. Or, alternatively, a nonselected stress relief process may be used to anneal the entire component in a furnace or oven. Each of the above may require additional cost or produce undesirable characteristics in the part.




One such component is a hub for a reverse and low gear, one-way clutch in the Ford CD4E automatic transmission. It would therefore be desirable to produce a precision stamped component and anneal the areas of high stress in the stamped component.




SUMMARY OF THE INVENTION




According to the present invention, a stamped component is locally annealed using a magnetic heating process. By doing so, stresses in the part are reduced so as to avoid splintering, slivering, or other defects during subsequent operations.




A process for forming a precision formed cup-shaped member is provided, including stamping a blank into a cup-shaped member. The cup-shaped member is positioned onto a magnetic heating machine. A magnetic core is positioned adjacent a radius of the cup-shaped part on both a top side and a bottom side of the cup-shaped part. The part is heated with the magnetic heating machine so as to anneal the cup-shape part at the radius.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a partial sectional side view of a precision stamped component according to the present invention.





FIG. 2

is a partial sectional side view of the component of

FIG. 1

having a further process step formed thereon to form splines in an outer surface thereof.





FIG. 2A

is a partial end view of the component of FIG.


2


.





FIG. 3

is a partial sectional side view of the component of

FIG. 1

having yet further operations formed thereon.





FIG. 4

is a schematic representation of a machine for use with the method according to the present invention.





FIG. 5

is a schematic representation of a part in a machine for use with the method according to the present invention.











DETAILED DESCRIPTION OF PREFERRED EMBODIMENT(S)




As shown in

FIG. 1

, a precision stamped member


10


in a preferred embodiment has a cup-shaped form. The member


10


is formed from flat blank of sheet metal. The flat blank has a radius


12


formed therein to cause the cup-shaped part


10


to acquire its shape. During the formation of the radius


12


, a high stress region results thereat. Further, a second radius


14


is formed in the cup-shaped member


10


, also causing a residual stress in the part


10


.




As shown in

FIG. 2

, the cup-shaped part


10


has a later process step formed thereon to form a plurality of splines


16


, as better illustrated in the view shown in

FIG. 2



a


. As shown in

FIG. 3

, a plurality of apertures


20


,


22


are formed in the member. Similarly, a plurality of oil vanes


24


may be formed therein. Each of the subsequent operations illustrated in

FIGS. 2-3

, if performed on the part


10


in a high stress area (i.e. after forming to the shape shown in

FIG. 1

without heat treating), would result in frequent defects in the form of fracturing or slivering in this region of the part.




As shown in

FIG. 4

, a magnetic heating machine


40


according to the present invention is illustrated schematically. As described in “Patented Heat Treating System Uses Magnetic Fuel Technology for Through-Heating of Metal Parts”, by D. Keith Patrick, in


Industrial Heating,


March 1998, pp. 61-68, a magnetic heating process is described, the article incorporated herein by reference. A machine


40


according to this article is further described in U.S. Pat. No. 5,025,124, and


The Principles of Uniform Magnetic Heating


(


UMH


), by Mitsubishi and Core-Flux, both of which are incorporated herein by reference.




As described in the '124 patent, and as illustrated schematically in

FIG. 4

, a machine


40


includes a C-frame


42


which is used to magnetically heat the parts. The C-frame


42


includes a first, or upper, core


46


positioned adjacent the workpiece


10


opposite a second core


44


positioned the workpiece


10


on the opposite side thereof. The cores


46


,


44


are strategically positioned so as to magnetically heat the part


10


at a localized area thereof


12


, previously indicated to be a high stress area due to the forming operation formed thereon. By so locally applying this magnetic field, the part


10


may be annealed at this local radius


12


, or locally at any other portion, in order to soften the material to prevent damage during further forming operations performed on the part


10


and/or use of the part


10


in a vehicle. In a preferred embodiment, the part


10


is made of a soft steel, such as SAE 1020, and has a hardness of about 85 Rb at the radius


12


after cold forming. The process anneals the part


10


at the radius


12


to a hardness of about 60 Rb, approximately equivalent to the hardness of the remainder of the part


10


.




As shown in

FIG. 5

, the cores


44


,


46


are placed near the radius


12


. Thus, the lines of flux


47


,


48


which travel through the part


10


are concentrated at the radius


12


, thereby heating the part at the radius


12


to approximately a minimum temperature of 400° F. This enables the part


10


to be annealed locally as would be appreciated by one skilled in the art upon reading this disclosure. As described in the Mitsubishi publication, the UMH system operates on the basis of a hysteresis loss system. Preferably, the frequency of the power supply is adjusted to optimize the efficiency of the heating process, so as to heat the part at about the resonance of the part


10


. In a preferred embodiment, a part


10


of about 173 MM diameter having a height of about 60 mm and weighing about 0.45 kg. is best heated with a power supply frequency of about 140 Hz. The current flow is adjusted in a similar manner to optimize the process to achieve the desired temperature.




The machine


40


includes a number of details to heat, locate and support the part


10


as described below. The upper and lower cores comprise a laminated material, such as a grain oriented silicon directional steel, known to one skilled in the art. Attached to the upper core


46


is a plate


41


. The plate


41


is provided to support a hoop


43


. The plate


41


and hoop


43


in a preferred embodiment comprise a low carbon steel material. The hoop


43


is provided to direct the flux


47


at the local area, such as the radius


12


, to be heated. The hoop


43


circumferentially surrounds the radius


12


and is provided in light contact therewith.




The lower core


44


includes an insulator


45


provided on a top surface thereof. The insulator


45


provides a horizontal surface to support the part


10


vertically. The insulator


45


may also provide features to locate the part horizontally, such as a vertical projection


45


′ to protrude through an opening provided on the part


10


and provide an interference fit or small clearance to locate the part


10


. A second insulator


49


is provided about the outer portion of the lower core


44


. The second insulator is used to insulate the inner circumference of the part


10


from the lower core


44


.




Subsequent to the annealing step above, the process steps of forming the splines


16


on the outer surface of the part


10


, as indicated in

FIG. 2

at


16


, is performed using the GROB process as is also known to one skilled in the art. One skilled in the art appreciates the GROB process is one preferred cold working rolling process for cold forming the splines, and alternative methods exist to form these splines. The subsequent operations of forming the holes and oil dams


20


,


22


,


24


, as indicated in

FIG. 3

, are performed using typically pressing, punching, piercing, and forming operations known to one skilled in the art. The annealing process permits one to locally anneal the part


10


and thereby prevent damage of the part, such as slivering, during the subsequent forming operations.




In a preferred embodiment, the annealing process is performed in a nitrogen atmosphere to eliminate oxidation and scaling during this operation within a chamber. Alternatively, this operation could be performed without the use of a cover gas, but the resultant oxidation would be produced.




Although the preferred embodiments of the present invention have been described, it will be apparent to a person skilled in the art that variations may be made to the process that is described herein without departing from the scope of the invention as defined by the following claims.



Claims
  • 1. A process for forming a precision formed cup-shaped member, comprising the steps of:forming a blank; stamping the blank into a cup-shaped member; positioning the cup-shaped member on a magnetic heating machine; positioning a magnetic core adjacent a radius of the cup-shaped part on both a top side and a bottom side of the cup-shaped part; and heating the cup-shaped part with the magnetic heating machine so as to anneal the cup-shape part locally at the radius.
  • 2. The process according to claim 1, further comprising the step of cold forming a plurality of splines about the outer circumference of the cup-shaped member after the part is magnetically heated.
  • 3. A process according to claim 2, further comprising the step of piercing oil holes through one of the splines formed therein.
  • 4. A process according to claim 1, further comprising the step of introducing an oxygen-starved atmosphere prior to heating the part.
  • 5. A process for forming a precision formed cup-shaped member, comprising the steps of:forming a blank; forming the blank into a cup-shaped member having a sharp radius; positioning the cup-shaped member on a magnetic heating machine; positioning a first magnetic core adjacent an outside portion of the sharp radius of the cup-shaped part; positioning a second magnetic core adjacent an inside portion of the sharp radius of the cup-shaped part; and applying a magnetic field to heat the cup-shaped part so as to anneal the cup-shape part substantially only at the radius.
  • 6. The process according to claim 5, wherein the magnetic field heats the cup-shaped member using a hysteresis loss principle.
  • 7. The process according to claim 6, further comprising the step of forming a plurality of splines about an outer circumference of the cup-shaped member.
  • 8. The process of claim 7, wherein the splines are formed using a cold forming process.
  • 9. A process according to claim 8, further comprising the step of piercing oil holes through one of the splines formed therein.
  • 10. A process for forming a clutch hub for an automatic transmission, comprising the steps of:forming a blank; forming the blank into a cup-shaped hub having a radius; positioning the hub on a magnetic heating machine; positioning a first magnetic core adjacent an outside portion of the radius of the hub; positioning a second magnetic core adjacent an inside portion of the radius of the hub; and applying a magnetic field to heat the hub using a hysteresis loss so as to anneal the hub substantially only at the radius.
  • 11. The process according to claim 10, further comprising the step of forming a plurality of splines about an outer circumference of the hub after the step of applying the magnetic field to the hub.
  • 12. The process of claim 11, wherein the splines are formed using a cold forming process.
  • 13. A process according to claim 12, further comprising the step of piercing oil holes through one of the splines formed in the hub.
  • 14. A process according to claim 10, further comprising the step of introducing a nitrogen atmosphere before magnetically heating the hub.
US Referenced Citations (12)
Number Name Date Kind
3211364 Wentling et al. Oct 1965
4496818 Reynolds et al. Jan 1985
4864706 Jenkel Sep 1989
4868365 Farone et al. Sep 1989
5023419 Langstedt Jun 1991
5025124 Alfredeen Jun 1991
5197190 Coolidge Mar 1993
5373144 Thelander Dec 1994
5373809 Fox et al. Dec 1994
5588019 Ruffini et al. Dec 1996
5683607 Gillespie et al. Nov 1997
5705794 Gillespie et al. Jan 1998
Foreign Referenced Citations (1)
Number Date Country
1143168 Feb 1989 GB
Non-Patent Literature Citations (1)
Entry
“Patented Heat treating System Uses Magnetic Field Technology for Through-Heating of Metal Parts” by D. Keith Patrick, Industrial Heating/Mar. 1998.