Patent Application
20170368585
The present disclosure relates to a method of manufacturing a tube and a machine for use therein.
A conventional tube used for housing an axle shaft of a vehicle have a wall defining a hollow interior. The wall thickness of the conventional tube varies depending on the application, e.g. heavy duty, light duty, etc. However, a yield strength of the conventional tubes must be sufficient to avoid failure during use of the vehicle. Typically, the yield strength of the conventional tube is about 600 MPa.
The conventional tubes are made in two separate components, such as a tube portion and a spindle end. Once the separate tube portion and the spindle end are manufactured, the spindle end is coupled to the tube portion, typically by friction welding. The required step of welding two components together to form the conventional tube also adds additional manufacturing time and expense.
With a desire in the automotive industry to increase fuel efficiency, there is a desire to reduce the overall weight of vehicles. To this end, there is a desire to reduce the weight of the conventional tube while maintaining or even increasing the yield strength. Furthermore, there is a need to eliminate the need for welding steps while maintaining or even increasing the yield strength.
One embodiment is directed toward a method of manufacturing a drawn tube. The drawn tube has a hollow interior for housing an axle shaft that transmits rotational motion from a prime mover to a wheel of a vehicle. The drawn tube has a wall that has a thickness of from about 3 to about 18 millimeters. The drawn tube has a yield strength of at least 750 MPa. The method includes the steps of placing a billet into a cavity of a first die assembly, pressing the billet into the cavity of the first die to form a bore at one end of the billet thereby producing a pre-formed billet, moving the pre-formed billet from the cavity of the first die assembly to a cavity of a second die assembly, pressing the pre-formed billet into the cavity of the second die assembly to elongate the pre-formed billet and form a hollow interior therein thereby producing an extruded tube, moving the extruded tube from the cavity of the second die assembly to a cavity of a third die assembly, and pressing the extruded tube into the cavity of the third die assembly to further elongate the extruded tube and decrease the thickness of the wall of the extruded tube to of from about 3 to about 18 millimeters thereby producing the drawn tube having the yield strength of at least 750 MPa. Therefore, the drawn tube produced by the method has a reduced wall thickness as compared to conventional drawn tubes thereby decreasing the weight of the drawn tube while maintaining a relatively high yield strength.
Other advantages of the disclosed subject matter will be readily appreciated, as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
The present disclosure is related to manufacturing an article from a starting component. For example, the article may be a tube for housing an axle shaft of a vehicle. The axle shaft transmits rotational motion from a prime mover, such as an engine or electric motor, to a wheel of a vehicle. Other possible examples of the article include drive shafts, gas cylinders, and CV joints.
It is to be appreciated that, depending on the steps used to manufacture the tube, the tube may be referred to as an extruded tube 30 or a drawn tube 32. For example, when the tube is formed by extrusion, the tube is referred to as the extruded tube 30. When the tube is additionally formed by drawing, the tube is referred to as the drawn tube 32.
Additionally, the tube may be further defined as a full-float axle tube 76, generally shown in
Referring to the Figures, wherein like numerals indicate like or corresponding parts throughout the several views, a billet 34 is generally shown in cross-section in
With reference to
With reference to
As shown in
When the extruded tube 30 is the full-float axle tube 76, the hollow interior 42 of the extruded tube 30 extends from the open end 44 into the extruded necked portion 50 towards the wheel end 46 and the wheel end 46 is closed. When the extruded tube 30 is the semi-float tube 78, the hollow interior 42 extends from the open end 44 to the wheel end 46 with the wheel end 46 closed. During subsequent machining, the wheel end 46 of both the full-float axle tube 76 and the semi-float axle tube 78 is opened such that the hollow interior 42 extends from the open end 44 to the wheel end 46.
An interior surface 54 of the extruded tube 30 defines the hollow interior 42. The extruded tube 30 also has an exterior surface 56 opposite the interior surface 54 of the extruded tube 30. An extruded wall 58 of the extruded tube 30 is defined between the interior surface 54 and the exterior surface 56 of the extruded tube 30. The extruded wall 58 has a thickness. Generally, the thickness of the extruded wall 58 is substantially consistent in the extruded body portion 48. Typically, the thickness of the extruded wall 58 in the extruded body portion 48 is of from about 5 to about 16 millimeters, more typically of from about 5 to about 12 millimeters. In the full-float axle tube 76, the thickness of the extruded wall 58 in the extruded necked portion 50 varies and tends to be thicker than the thickness of the extruded wall 58 in the extruded body portion 48. In the semi-float axle tube 78, the thickness of the extruded wall 58 may be thicker at the wheel end 46 relative to the extruded body portion 48.
In one embodiment described in greater detail below, a preliminarily extruded tube 126 is formed prior to the formation of the extruded tube 30. Said different, extruded tube 30 formed upon the completion of at least two extrusions.
With reference to
Generally, when the drawn tube 32 is the full-float axle tube 76, the wheel end 62 of the drawn tube 32 is referred to as a spindle end 64 of the drawn tube 32. When present, the spindle end 64 of the drawn tube 32 is integral with the drawn body portion 66 such that the spindle end 64 cannot be separated from the drawn body portion 66. The drawn tube 32 has a drawn body portion 66 having a substantially consistent diameter. The drawn body portion 66 extends from the open end 60 of the drawn tube 32. When the drawn tube 32 is the full-float axle tube 76, the drawn tube 32 has a drawn necked portion 68 adjacent the drawn body portion 66. The drawn necked portion 68 has a diameter that is smaller than the diameter of the drawn body portion 66. The drawn necked portion 68 also has a plurality of shoulders 70 where the diameter of the drawn necked portion 68 is reduced. The spindle end 64 of the drawn tube 32 is adjacent the drawn necked portion 68. The spindle end 64 has a solid cross-section.
A hollow interior 72 of the drawn tube 32 extends from the open end 60 towards the wheel end 62. In the full-float axle tube 76, the hollow interior 72 extends into the drawn necked portion 68 and extends through the drawn tube 32 such that the wheel end 62 is open. Typically, the wheel end 62 is machined to create the opening at the wheel end 62 such that the hollow interior 72 extends through the drawn tube 32. In the semi-float axle tube 78, the hollow interior 72 does not extend through the drawn tube 32 such that the wheel end 62 is closed. However, the wheel end 62 is machined to create the opening at the wheel end 62 such that the hollow interior 72 extends through the drawn tube 32.
The drawn tube 32 has a drawn wall 74 having a thickness. Generally, the thickness of the drawn wall 74 is substantially consistent in the drawn body portion 66. However, as a result of elongating the extruded tube 30 to form the drawn tube 32, the thickness of the drawn wall 74 is reduced relative to the thickness of the extruded wall 58.
Typically, the thickness of the drawn wall 74 is of from about 3 to about 18 millimeters, more typically of from about 3 to about 10 millimeters, and even more typically of from about 3 to about 8 millimeters. It is to be appreciated that the thickness of the drawn wall 74 in the drawn body portion 66 may vary depending on the application and the type of tube produced. For example, when the tube is the full-float axle tube 76 the thickness of the drawn wall 74 in the drawn body portion 66 is typically of from about 4 to about 10 millimeters, more typically or from about 4 to about 8 millimeters, and even more typically of from about 4 to about 7 millimeters for medium duty applications. Additionally, when the tube is the full-float axle tube 76 the thickness of the drawn wall 74 in the drawn body portion 66 is typically of from about 6 to about 18 millimeters, more typically or from about 6 to about 14 millimeters, even more typically of from about 6 to about 10 millimeters, and yet even more typically less than 8 millimeters for heavy duty applications. When the tube is the semi-float axle tube 78 the thickness of the drawn wall 74 in the drawn body portion 66 is typically of from about 3 to about 10 millimeters, more typically of from about 3 to about 8 millimeters, even more typically of from about 3 to about 6 millimeters, and yet even more typically less than 4.5 millimeters for light duty applications. It is to be appreciated that the term light duty generally refers to pick-up trucks and SUVs, the term medium duty generally refers to vehicles having a single wheel at each axle end, such as the Ford F-250, F-350, and F-450 or the Chevrolet (“Chevy”) Silverado 2500, 3500, and 4500, and the term heavy duty generally refers to vehicles having multiple wheels at each axle end.
It is also to be appreciated that the thickness of the drawn wall 74 may be consistent about the circumference of the drawn tube 32 within the drawn body portion 66. However, as shown in
With reference to
With reference to
With reference to
A second die assembly 88 is used to transform the pre-formed billet 36 into the extruded tube 30. More specifically, a second mandrel 90 is used to press the pre-formed billet 36 into a cavity 92 of the second die assembly 88 which results in the elongation of the pre-formed billet 36 and the extension of the bore 40 into the pre-formed billet 36 to form the hollow interior 42 thereby producing the extruded tube 30.
A third die assembly 94 is used to transform the extruded tube 30 into the drawn tube 32. More specifically, a third mandrel 96 is used to press the extruded tube 30 into a cavity 98 of the third die assembly 94 which results in a further elongation of the extruded tube 30 and a thinning of the thickness of the extruded wall 58 thereby producing the drawn tube 32. The third mandrel 96 is used to press the extruded tube 30 through the third die assembly 94 with the cavity 98 of the third die assembly 94 progressively narrowing to further elongate the extruded tube 30 and reducing the thickness of the extruded wall 58 thereby producing the drawn tube 32.
As generally understood in the art, the cavities 86, 92, 98 of the die assemblies 82, 88, 94 and a working end 100 of the mandrels 84, 90, 96 are configured to cooperate with each other to transform the part within each of the die assemblies 82, 88, 94. For example, when the third mandrel 96 is inserted into the cavity 98 of the third die assembly 94, a space having a distance is defined between the third die assembly 94 and the third mandrel 96. The distance of the space results in the thickness of the drawn wall 74 of the drawn tube 32 once the third mandrel 96 presses the extruded tube 30 into the third die assembly 94.
With reference to
The method of manufacturing the drawn tube 32 with the yield strength of at least 750 MPa includes the steps of placing the billet 34 into the cavity 86 of the first die assembly 82, pressing the billet 34 into the cavity 86 of the first die assembly 82 to form the bore 40 at one end 38A of the billet 34 thereby producing the pre-formed billet 36, and moving the pre-formed billet 36 from the cavity 86 of the first die assembly 82 to the cavity 92 of the second die assembly 88. The method also includes the steps of pressing the pre-formed billet 36 into the cavity 92 of the second die assembly 88 to elongate the pre-formed billet 36 and form the hollow interior 42 therein thereby producing the extruded tube 30, moving the extruded tube 30 from the cavity 92 of the second die assembly 88 to the cavity 98 of the third die assembly 94, and pressing the extruded tube 30 into the cavity 98 of the third die assembly 94 to further elongate the extruded tube 30 and decrease the thickness of the extruded wall 58 of the extruded tube 30 to be of from about 3 to about 18 millimeters thereby producing the drawn tube 32 having the yield strength of at least 750 MPa.
Although the yield strength of the drawn tube 32 is described as being at least 750 MPa above, the yield strength may also be at least 900 MPa or even at least 1,000 MPa. In this method, the billet 34 comprises a material selected from the group of low carbon alloy steels, plain carbon steels, and combinations thereof.
It is to be appreciated that the step of pressing the pre-formed billet 36 into the cavity 92 of the second die assembly 88 may be further defined as forward and backward extruding the pre-formed billet 36 to elongate the pre-formed billet 36 and form the hollow interior 42 therein thereby producing the extruded tube 30. Additionally, the step of pressing the extruded tube 30 into the cavity 98 of the third die assembly 94 may be further defined as drawing the extruded tube 30 to further elongate the extruded tube 30 and decrease the thickness of the extruded wall 58 of the extruded tube 30 to of from about 3 to about 18 millimeters thereby producing the drawn tube 32.
As shown in
A total drawn tube manufacturing time to complete the steps of placing a billet 34, pressing the billet 34 to produce the pre-formed billet 36; moving the pre-formed billet 36, pressing the pre-formed billet 36 to produce the extruded tube 30, moving the extruded tube 30, and pressing the extruded tube 30 to produce the drawn tube 32 is typically of from about 20 to about 240 seconds, more typically of from about 20 to about 120 seconds, even more typically of from about 20 to about 60 seconds, and yet even more typically of from about 20 to about 40 seconds.
The method may further comprise the step of heating the billet 34 to a temperature between 1,500 and 2,300 degrees Fahrenheit prior to the step of pressing the billet 34 into the cavity 86 of the first die assembly 82. The billet 34 may be heated in a furnace, through the use of heating methods including gas-fire and induction heating. It is to be appreciated that the billet 34 may be heated to the desired temperature by any suitable device and in any suitable manner.
The method may further comprise the step of pressing the pre-formed billet 36 into the cavity 92 of the second die assembly 88 is conducted at a temperature at least equal to 1,500 degrees Fahrenheit. As such, each of the steps prior to the step of pressing the pre-formed billet 36 into the cavity 92 of the second die assembly 88, including the step of pressing the billet 34 into the cavity 86 of the first die assembly 82 to form the bore 40 at one end 38A of the billet 34 thereby producing the pre-formed billet 36 may be performed before the pre-formed billet 34 reaches a temperature of 1,500 degrees Fahrenheit. Said differently, the billet 34 may decrease from the initial temperature of between 1,500 and 2,300 degrees Fahrenheit to at least equal to 1,500 degrees Fahrenheit as the billet 34 is formed into the extruded tube 30. As such, the pressing of the billet 34 in the first die assembly 82 and the pressing of the pre-formed billet 36 into the second die assembly 88 are commonly referred to by those skilled in the art of metal working and forming as a hot forging. Hot forging allows for increased ductility in the worked metallic material to facilitate the formation of various designs and configurations.
As described above, the second die assembly 88 may be further defined as the initial and later stage second die assemblies 128, 130 which progressively press the pre-formed billet 36 and the preliminarily extruded tube 126, respectively, to produce a work product: the extruded tube 30. It is to be appreciated that step of pressing the pre-formed billet 36 into the cavity 92 of the second die assembly 88 is conducted at a temperature at least equal to 1,500 degrees Fahrenheit may refer to both pressing the pre-formed billet 36 in the initial stage second die assembly 128 and the preliminarily extruded tube 126 in the later stage second die assembly 130 at a temperature at least equal to 1,500 degrees Fahrenheit. Alternatively, only one of the steps of pressing the pre-formed billet 36 in the initial stage second die assembly 128 and the preliminarily extruded tube 126 in the later stage second die assembly 130 may be performed at a temperature at least equal to 1,500 degrees Fahrenheit.
The step of pressing the extruded tube 30 into the cavity 98 of the third die assembly 94 may be conducted at a temperature between 800 and 900 degrees Fahrenheit. Said differently, the billet 34 may decrease from the initial temperature of between 1,500 and 2,300 degrees Fahrenheit to between 800 and 900 degrees Fahrenheit as the billet 34 is formed into the drawn tube 32. The 800-900 degree Fahrenheit range falls between the hot forging described above and cold forging, which those skilled in the art will appreciate is performed at approximately room temperature. While hot forging allows for high ductility of the worked material, the worked material generally has lower resultant yield strength than a product formed by cold forging. Alternatively, a product formed by cold forging is typically stronger than a product formed hot forging, but the worked material is typically not as ductile as the worked material in a hot forging process, which results in greater wear and tear on the cold forging machinery. Conducting the step of pressing the extruded tube 30 into the cavity 98 of the third die assembly 94 at a temperature between 800 and 900 degrees Fahrenheit balances the resultant yield strength and the ductility of the drawn tube 32 such that drawn tube 32 has a yield strength of at least 750 MPa while the incurring reduced wear and tear to the third die assembly 94 than if the drawn tube 32 was formed through a cold forging process. However, one skilled in the art will appreciate that the step of pressing the extruded tube 30 into the cavity 98 of the third die assembly 94 may be performed at any suitable temperature.
The method may further comprise the step of cooling the extruded tube 30 prior to the step of pressing the extruded tube 30 into the cavity 98 of the third die assembly 94. More specifically, the extruded tube 30 may be cooled from approximately 1,500 degrees Fahrenheit to between 800 and 900 degrees Fahrenheit. The cooling of a material between pressings is commonly referred to in the art as dwelling. In one embodiment, the first and second die assemblies 82, 88 are coupled to a first machine 132 and the third die assembly 94 is coupled to a second machine 134. The extruded tube 30 may be removed from the second die assembly 88 in the first machine 132 and may move to the third die assembly 94 in the second machine 134. The amount of time that is required to move the extruded tube 30 from the first machine 132 to the second machine 134 while exposed to room temperature air may cool the extruded tube 30 to the desired 800 and 900 degrees Fahrenheit. Alternatively, the extruded tube 30 may be exposed to forced air between the second and third die assemblies 88, 94 which may accelerate the cooling of the extruded tube 30. As another alternative, the extruded tube 30 may be quenched in a liquid (such as oil, water, etc.) between the second and third die assemblies 88, 94 which may accelerate the cooling of the extruded tube 30. It is to be appreciated that the extruded tube 30 may be cooled in any suitable manner.
The method may include the step of machining the spindle end 64 of the drawn tube 32 to produce a full-float hollow axle tube 76 having the hollow interior 72 that spans the length of the full-float hollow axle tube 76.
It is to be appreciated that the method described above is not specifically tied to the use of a single machine 120. Said differently, the method described above may use multiple machines to complete the steps described above to manufacture the drawn tube 32. For example, as described above and in greater detail below, and shown in
An alternative method of manufacturing the drawn tube 32 having a yield strength of at least 750 MPa is described below. With reference to
It is to be appreciated that the step of extruding the first pre-formed billet 36A may be further defined as forward and backward extrusion of the first pre-formed billet 36A within the cavity 92 of the second die assembly 88 to produce the extruded tube 30 having the hollow interior 42. It is also to be appreciated that the billet 34 may be further defined as a first billet 34A and the extruded tube 30 may be further defined as a first extruded tube 30A. With reference to
As describe above and shown in
It is to be appreciated that the alternative method described above is not specifically tied to the use of a single machine 120. Said differently, the alternative method described above may use multiple machines to complete the steps described above to manufacture the drawn tube 32. For example, as described above and in greater detail below, and shown in
In each of the manufacturing methods described above, the resultant yield strength of the tube, whether the extruded tube 30 or the drawn tube 32, is influenced by several factors, including the material chemistry of the billet 34, the reduction in the cross-sectional area of the billet 34, the temperature of the billet 34, pre-formed billet 36, extruded tube 30 and drawn tube 32, and/or any rapid cooling after any of the forging steps.
The material chemistry of the billet 34 is selected to maximize the yield strength of the tube while limiting a total alloy content of the material of the billet 34 so that the material of the billet 34 maintains weldability.
A common measure of weldability is the Carbon Equivalency (CE) value. Standard practice is to maintain the CE value below 0.50. CE equals the percent carbon plus percent manganese divided by 6 plus the percents of chromium, molybdenum, and vanadium divided by 5 plus the percent copper and nickel divided by 15.
As the percent reduction in area (RA) of the billet 34 increases, the resultant yield strength of the tube will increase. The RA is found by subtracting the cross-sectional thickness of the drawn wall 74 of the tube from that of the cross-sectional area of the billet 34, dividing that by the cross-sectional area of the billet 34, and multiplying by 100. It can be seen then that for a given cross-sectional area of the billet 34, manufacturing the tube with a thinner wall thickness will increase the yield strength of the tube. For example, it has been found that manufacturing the tube with the drawn wall 74 having a thickness of 4.0 millimeters from a starting billet having a diameter of 100 millimeters can generate yield strength in the resultant drawn tube 32 of about 1000 MPa, given the appropriate material chemistry and forging temperature. However, if the thickness of the drawn wall 74 were to be 6.0 millimeters from the billet 34 having the diameter of 100 millimeters at the given forging temperature may only generate a resultant drawn tube 32 with the yield strength of about 750 MPa, and would require special in-process or post-process cooling practices (described below) to attain the yield strength of 1000 MPa.
The forging temperature of the extruded tube 30 prior to forming the drawn tube 32 is selected to balance several competing factors. The resultant yield strength of the drawn tube 32 will increase for a given forging process sequence as the forging temperature is decreased. However, the forces required to change from the billet 34 to the drawn tube 32 will increase as the forging temperature is decreased. If the forging temperature is too low, the energy required to change the billet 34 into the drawn tube 32 may exceed the capacity of the selected forging machine.
As generally discussed above, special cooling practices within the method may also be used to attain the desired yield strength of the drawn tube 32. It is known that conducting the final draw operation at lower temperatures will increase the resultant yield strength. However, conducting the prior extruding step at that same lower temperature may exceed the available energy of the extruding equipment. One approach to solve this problem is to pass the extruded tube 30 through water cooling rings just prior to the final draw operation to lower the temperature of the extruded tube 30 and allow the drawn tube 32 to attain the desired yield strength. An alternative for in-process cooling would be to delay the extruded tube 30 transportation from the second die assembly 88 to the third die assembly 94 to allow the extruded tube 30 to cool. For example, the extruded tube 30 can be placed into a cooling conveyor until the desired temperature of the extruded tube 30 is reached. Then the extruded tube 30 can be inserted into the third die assembly 94 for the final draw operation. Additionally, a separate machine could also be used for housing the third die assembly 94 for completing the final draw operation if desired.
Finally, post-forging process rapid cooling can be used to boost the yield strength of a drawn tube 32. With this technique the temperature of the billet 34 is selected to be high enough so that the temperature of the drawn tube 32 is still above a critical temperature (typically about 720 degrees Celsius (1330 degrees Fahrenheit)) after the drawn tube 32 exits the final draw operation. The drawn tube 32 is then immediately and rapidly cooled with water or forced air to attain the desired yield strength. However, the temperature of the billet 34 may be too high, which can negatively affect the mandrels 84, 90, 96 and die assemblies 82, 88, 94 if the cooling methods used for the mandrels 84, 90, 96 and die assemblies 82, 88, 94 do not have the capacity to remove enough heat to prevent excessive softening of the mandrels 84, 90, 96 and die assemblies 82, 88, 94, especially with high production rates. Also, care must be taken so that the rapid cooling method does not induce excessive runout in the drawn tube 32 that will cause problems in subsequent machining operations.
In each of the manufacturing methods described above, when the third die assembly 94 is present, the method may include a skip stroke process to produce the drawn tube 32. For example, the billet 34 may be disposed within the first die assembly 82 and the extruded tube 30 may be disposed within the third die assembly 94 with the second die assembly 88 remaining empty. The skip stroke method includes the steps of forming the billet 34 within the cavity 86 of the first die assembly 82 to produce the second pre-formed billet 36B and forming the extruded tube 30 within the third die assembly 94 to produce the drawn tube 32.
With reference to
Returning to
Returning to
One of the first and second platform mandrels 112, 114 is aligned with the die assembly 82, 88, 94. For example, when the first platform mandrel 112 is aligned with the die assembly 82, 88, 94, the second platform mandrel 114 is not aligned with the die assembly 82, 88, 94. Rotation of the rotatable platform 110 selectively aligns either the first platform mandrel 112 or the second platform mandrel 114 with the cavity 86, 92, 98 of the die assembly 82, 88, 94. For example, when the first platform mandrel 112 is aligned with the cavity 86, 92, 98 of the die assembly 82, 88, 94, rotation of the rotatable platform 110 results in the alignment of the second platform mandrel 114 with the cavity 86, 92, 98 of the die assembly 82, 88, 94 and results in the non-alignment of the first platform mandrel 112 and the die assembly 82, 88, 94.
The apparatus 102 may include a container 116 coupled to the fixed base 104 adjacent the die assembly 82, 88, 94 with the container 116 including a cooling fluid, a lubricating fluid, and/or a combination thereof therein and configured to receive the second platform mandrel 114 as the first platform mandrel 112 enters the cavity 86, 92, 98 of the die assembly 82, 88, 94 for cooling the second platform mandrel 114.
Additionally, the apparatus 102 may include a third platform mandrel 118 coupled to and extending from the rotatable platform 110 toward the fixed base 104. As such rotation of the rotatable platform 110 aligns one of the first platform mandrel 112, the second platform mandrel 114, and the third platform mandrel 118 with the cavity 86, 92, 98 of the die assembly 82, 88, 94.
In one embodiment, the container 116 is further defined as a first container 116A and the apparatus 102 includes a second container 116B coupled to the fixed base 104 adjacent the die assembly 82, 88, 94 and the first container 116A. The second container 116B includes the lubricating fluid therein and is configured to receive the third platform mandrel 118 as the first platform mandrel 112 enters the cavity 86, 92, 98 of the die assembly 82, 88, 94 and the second platform mandrel 114 enters the first container 116A. However, it is to be appreciated that the second container 116B may include the cooling fluid, the lubricating fluid or a combination thereof.
In another embodiment, the mandrel assembly 108 is further defined as a first mandrel assembly 108A and the apparatus 102 includes a second mandrel assembly 108B and another die assembly 82, 88, 94. Typically, the die assembly 82, 88, 94 is the second die assembly 88 described above and the another die assembly 82, 88, 94 is the third die assembly 94 described above. When the another die assembly 82, 88, 94 is the third die assembly 94, the third die assembly 94 is coupled to the fixed base 104 and defines the cavity 98 therein configured to receive the extruded tube 30.
The second mandrel assembly 108B is coupled to the single press structure 106. Similar to the first mandrel assembly 108A, the second mandrel assembly 108B comprises a rotatable platform 110 coupled to the single press structure 106 with the rotatable platform 110 rotatable relative to the single press structure 106. The second mandrel assembly 108B includes a first platform mandrel 112 coupled to and extending from said rotatable platform 110 toward the fixed base 104 with the first platform mandrel 112 of the second mandrel assembly 108B configured to enter the cavity 86, 92, 98 of the another die assembly 82, 88, 94. A second platform mandrel 114 is coupled to and extending from the rotatable platform 110 toward the fixed base 104 with the second platform mandrel 114 of the second mandrel assembly 108B configured to enter the cavity 92 of the second die assembly 88. Rotation of the rotatable platform 110 of the second mandrel assembly 108B aligns either the first platform mandrel 112 of the second mandrel assembly 108B or the second platform mandrel 114 of the second mandrel assembly 108B with the cavity 86, 92, 98 of the another die assembly 82, 88, 94.
It is to be appreciated that the platform mandrels 112, 114, 118 be fixed, or may shuttle along a linear slide.
A method of manufacturing the article using the apparatus 102 is described below. The apparatus 102 has the fixed base 104 and the single press structure 106 movable toward the fixed base 104. The apparatus 102 includes the die assembly 82, 88, 94 coupled to the fixed base 104. It is to be appreciated that the die assembly 82, 88, 94 of the apparatus 102 may be any one of the first, second, and third die assemblies 82, 88, 94 described above. Furthermore, the second die assembly 88 may be further defined as the initial and final stage second die assemblies 128, 130 as described above. The apparatus 102 includes the container 116 coupled to the fixed base 104 spaced from the die assembly 82, 88, 94 and the mandrel assembly 108. The mandrel assembly 108 includes the rotatable platform 110 coupled to the single press structure 106, the first platform mandrel 112 coupled to and extending from the rotatable platform 110 toward the fixed base 104, and the second platform mandrel 114 coupled to and extending from the rotatable platform 110 toward the fixed base 104.
The method of using the apparatus 102 comprises the steps of placing the starting component into the cavity 86, 92, 98 of the die assembly 82, 88, 94 and pressing the starting component into the cavity 86, 92, 98 of the die assembly 82, 88, 94 with the first platform mandrel 112 to form the first starting component into the article. The method of using the apparatus 102 also includes the steps of moving the second platform mandrel 114 into the container 116 simultaneously with the step of pressing the starting component with the first platform mandrel 112, removing the article from the die assembly 82, 88, 94 and placing the second starting component into the cavity 86, 92, 98 of the die assembly 82, 88, 94. The method of using the apparatus 102 further includes the steps of rotating the rotatable platform 110 to align the second platform mandrel 114 with the die assembly 82, 88, 94 and to align the first platform mandrel 112 with the container 116, pressing the second starting component into the cavity 86, 92, 98 of the die assembly 82, 88, 94 with the second platform mandrel 114 to form the second starting component into another article, and moving the first platform mandrel 112 into the container 116 simultaneously with the step of pressing the second starting component with the second platform mandrel 114.
It is to be appreciated that when the container 116 contains the cooling fluid and/or lubricating fluid, the step of moving the second platform mandrel 114 into the container 116 may be further defined as cooling the second platform mandrel 114 simultaneously with the step of pressing the first starting component with the first platform mandrel 112. It is also to be appreciated that the container 116 may be further defined as a first container 116A and the apparatus 102 includes the second container 116B spaced from the die assembly 82, 88, 94 and the first container 116A. In such an embodiment, the mandrel assembly 108 includes the third platform mandrel 118 coupled to and extending from the rotatable platform 110. As such, the method of using the apparatus 102 further comprises the step of moving the third platform mandrel 118 into the second container 116B simultaneously with the step of pressing the first starting component with the first platform mandrel 112. Furthermore, when the apparatus 102 includes the first and second containers 116A, 116B, the first container 116A contains the cooling fluid and the second container 116B contains the lubricating fluid. In such an embodiment, the step of moving the second platform mandrel 114 into the first container 116A is further defined as cooling the second platform mandrel 114 with the cooling fluid simultaneously with the step of pressing the first starting component with the first platform mandrel 112, and lubricating the third platform mandrel 118 with the lubricating fluid simultaneously with the step of pressing the first starting component with the first platform mandrel 112.
When the mandrel assembly 108 includes the third platform mandrel 118, the step of rotating the rotatable platform 110 to align the second platform mandrel 114 with the die assembly 82, 88, 94 is further defined as rotating the rotatable platform 110 to align the third platform mandrel 118 with the die assembly 82, 88, 94, to align the first platform mandrel 112 with the first container 116A, and to align the second mandrel 90 with the second container 116B.
It is to be appreciated that the apparatus 102 could be the single machine 120 described in detail below.
A method of manufacturing either the extruded tube 30 or the drawn tube 32 using the apparatus 102 is described below. As described above, the apparatus 102 includes the fixed base 104 and the single press structure 106 movable toward the fixed base 104. The apparatus 102 also includes the die assembly 82, 88, 94 coupled to the fixed base 104, the container 116 coupled to the fixed base 104 and spaced from the die assembly 82, 88, 94, and the mandrel assembly 108. The mandrel assembly 108 comprises the rotatable platform 110 coupled to the single press structure 106, the first platform mandrel 112 coupled to and extending from the rotatable platform 110 toward the fixed base 104, and the second platform mandrel 114 coupled to and extending from the rotatable platform 110 toward the fixed base 104.
The method of using the apparatus 102 to manufacture the tube comprises the steps of placing a first pre-formed billet 36A into the cavity 92 of the die assembly 88, pressing the first pre-formed billet 36A into the cavity 92 of the die assembly 88 with the first platform mandrel 112 to elongate the first pre-formed billet 36A to produce an extruded tube 30, and moving the second platform mandrel 114 into the container 116 simultaneously with the step of pressing the first pre-formed billet 36A with the first platform mandrel 112. The method of using the apparatus 102 to manufacture the tube also includes the steps of removing the extruded tube 30 from the die assembly 88, placing a second pre-formed billet 36B into the cavity 92 of the die assembly 88, and rotating the rotatable platform 110 to align the second platform mandrel 114 with the die assembly 88 and to align the first platform mandrel 112 with the container 116. The method of using the apparatus 102 to manufacture the tube further includes the steps of pressing the second pre-formed billet 36B into the cavity 92 of the die assembly 88 with the second platform mandrel 114 to elongate the second pre-formed billet 36B to produce another extruded tube 30, and moving the first platform mandrel 112 into the container 116 simultaneously with the step of pressing the second billet 34B with the second platform mandrel 114.
It is to be appreciated that the step of pressing the first pre-formed billet 36A into the cavity 92 may be further defined as extruding the pre-formed billet 36 to produce the extruded tube 30. It is also to be appreciated that the method of using the apparatus 102 to manufacture the tube could be used to produce a drawn tube 32 in addition to the extruded tube 30 as described above. For example, rather than placing a first pre-formed billet 36A into the die assembly 88, a first extruded tube 30A could be inserted into the die assembly 94. The subsequent step of pressing the extruded tube 30 into the cavity 98 would produce the drawn tube 32.
In an effort to further minimize the total extruded tube manufacturing time, the second mandrel 90 of the apparatus 102 may be further defined as the mandrel assembly 108. As described above, the mandrel assembly 108 includes the rotatable platform 110 coupled to the single press structure 106 with the rotatable platform 110 rotatable relative to the single press structure 106. A first platform mandrel 112 is coupled to and extends from the rotatable platform 110 toward the fixed base 104. Similarly, the second platform mandrel 114 is coupled to and extends from the rotatable platform 110 toward the fixed base 104. The rotatable platform 110 is rotatable relative to the single press structure 106 for selectively aligning either the first platform mandrel 112 or the second platform mandrel 114 with the cavity 92 of the second die assembly 88. As such, the apparatus 102 can switch between the first platform mandrel 112 or the second platform mandrel 114 for pressing the pre-formed billet 36 into the second die assembly 88. By switching between the first and second platform mandrels 112, 114, only one of the first and second platform mandrels 112, 114 is actually doing work to transform the pre-formed billet 36 into the extruded tube 30 while the other one of the first and second platform mandrels 112, 114 is allowed to cool. This type of cooling is referred to as offline cooling because one of the first and second platform mandrel 112, 114 is allowed to cool without delaying or stopping the apparatus 102 from continuing to work using the other one of the first and second platform mandrels 112, 114.
When the container 116 contains the cooling fluid, the step of moving the second platform mandrel 114 into the container 116 is further defined as cooling the second platform mandrel 114 simultaneously with the step of pressing the first pre-formed billet 36A with the first platform mandrel 112. It is to be appreciated that the container 116 may be further defined as the first container 116A and the apparatus 102 includes the second container 116B spaced from the die assembly 82, 88, 94 and the first container 116A. In such an embodiment, the mandrel assembly 108 includes the third platform mandrel 118 coupled to and extending from the rotatable platform 110 and the method further comprises the step of moving the third platform mandrel 118 into the second container 116B simultaneously with the step of pressing the first pre-formed billet 36A with the first platform mandrel 112. Additionally, when the first container 116A contains the cooling fluid and the second container 116B contains the lubricating fluid, the step of moving the second platform mandrel 114 into the first container 116A is further defined as, cooling the second platform mandrel 114 with the cooling fluid simultaneously with the step of pressing the first pre-formed billet 36A with the first platform mandrel 112, and lubricating the third platform mandrel 118 with the lubricating fluid simultaneously with the step of pressing the first pre-formed billet 36A with the first platform mandrel 112.
When the third platform mandrel 118 is present, the step of rotating the rotatable platform 110 to align the second platform mandrel 114 with the die assembly 88 is further defined as rotating the rotatable platform 110 to align the third platform mandrel 118 with the die assembly 88 to align the first platform mandrel 112 with the first container 116A, and to align the second mandrel 90 with the second container 116B.
In each of the manufacturing methods described above, when the third die assembly 94 is present, the method may include a skip stroke process to produce the drawn tube 32. For example, the billet 34 may be disposed within the first die assembly 82 and the extruded tube 30 may be disposed within the third die assembly 94 with the second die assembly 88 remaining empty. The skip stroke method includes the steps of forming the billet 34 within the cavity 86 of the first die assembly 82 to produce the second pre-formed billet 36B and forming the extruded tube 30 within the third die assembly 94 to produce the drawn tube 32.
It is to be appreciated that the apparatus 102 could be the single machine 120 described in detail below.
Generally, at least one machine is used to manufacture the extruded tube 30 or the drawn tube 32. In one embodiment, the extruded tube 30 is manufactured from the billet 34 using a single machine 120. As shown in
The single machine 120 includes the second die assembly 88 coupled to the fixed base 104 and spaced from the first die assembly 82. The second die assembly 88 defines the cavity 92 therein and is configured to receive the pre-formed billet 36. During operation of the single machine 120, the second die assembly 88 is configured to hold the pre-formed billet 36 and to assist with extruding the pre-formed billet 36 into the extruded tube 30.
As described above, the second die assembly 88 may be further defined as the initial stage second die assembly 128 and the later stage second die assembly 130, which is generally shown in
Returning to
It is to be appreciated that the single press structure 106 may include a single press plate 124 coupled to the moveable component 122. Alternatively. The single press structure 106 may include multiple press plates 124A, 124B, as shown in
The single press structure 106 comprises the first mandrel 84 aligned with the cavity 86 of the first die assembly 82. The single press structure 106 also comprises the second mandrel 90 aligned with the cavity 92 of the second die assembly 88. For example, the first and second mandrels 84, 90 may be coupled to the single press plate 124. Alternatively, the first and second mandrels 84, 90 may be coupled to a respective one of the multiple press plates 124A, 124B. Because the first and second mandrels 84, 90 are coupled to the single press plate 124 or a respective one of the multiple press plates 124A, 124B and the multiple press plates 124A, 124B are coupled to the same moveable component 122, the first and second mandrels 84, 90 move simultaneously with each other as the single press structure 106 moves towards and then away from the fixed base 104. When the single press structure 106 moves toward the fixed base 104 from the starting position to the pressed position, the first mandrel 84 enters the cavity 86 of the first die assembly 82 and the second mandrel 90 enters the cavity 92 of the second die assembly 88 as the single press structure 106 moves towards the fixed base 104.
The term single machine 120 as used herein is meant to convey that the use of moveable component 122 even though multiple die assemblies 82, 88, 94 may be used. For example, even though the single machine 120 has the first and second die assemblies 82, 88 and the first and second mandrels 84, 90, it is still considered a single machine 120 because it only has a single press structure 106 moveable by the single moveable component 122 common to both the first and second die assemblies 82, 88, 94.
A method of manufacturing the tube, when the tube is the extruded tube 30, with the single machine 120 comprises the steps of placing the billet 34 into the cavity 86 of the first die assembly 82 and pressing the billet 34 into the cavity 86 of the first die assembly 82 with the first mandrel 84 that is coupled to the single press structure 106. The pressing of the first mandrel 84 into the billet 34 forms a bore 40 at one end of the billet 34 thereby producing the pre-formed billet 36.
It is to be appreciated that the step of pressing the first mandrel 84 into the billet 34 may be further defined as extruding the pre-formed billet 36 by cycling the single press structure 106 towards and then away from the fixed base 104 to elongate the pre-formed billet 36 and form the hollow interior 42 therein thereby producing the extruded tube 30. Said differently, the billet 34 may be transformed into the pre-formed billet 36 by forward and/or backward extrusion that is accomplished within the first die assembly 82.
The method further includes the steps of moving the pre-formed billet 36 from the cavity 86 of the first die assembly 82 to the cavity 92 of the second die assembly 88. Then the pre-formed billet 36 is pressed into the cavity 92 of the second die assembly 88 with the second mandrel 90 that is coupled to the single press structure 106 to elongate the pre-formed billet 36 and form the hollow interior 42 therein to produce the extruded tube 30.
The method has a total extruded tube manufacturing time to produce the extruded tube 30. Because the first and second die assemblies 82, 88 are within the single machine 120 and the because the first and second mandrels 84, 90 are coupled to the single press structure 106, the total extruded tube manufacturing time is minimized relative to conventional tube manufacturing practices. More specifically, because the use of the single machine 120 eliminates the use of multiple machines to produce the extruded tube 30, any additional steps of heating or lubricating parts and the time to move parts between multiple machines is eliminated, which reduces the total extruded tube manufacturing time.
Typically, the total extruded tube manufacturing time to complete the steps of placing a billet 34, pressing the billet 34 to produce the pre-formed billet 36; moving the pre-formed billet 36, and pressing the pre-formed billet 36 to produce the extruded tube 30 is of from about 15 to about 120 seconds, more typically of from about 15 to about 60 seconds, and even more typically of from about 15 to about 30 seconds.
In an effort to further minimize the total extruded tube manufacturing time, the second mandrel 90 of the single machine 120 may be further defined as the mandrel assembly 108. As described above, the mandrel assembly 108 includes the rotatable platform 110 coupled to the single press structure 106 with the rotatable platform 110 rotatable relative to the single press structure 106. A first platform mandrel 112 is coupled to and extends from the rotatable platform 110 toward the fixed base 104. Similarly, the second platform mandrel 114 is coupled to and extends from the rotatable platform 110 toward the fixed base 104. The rotatable platform 110 is rotatable relative to the single press structure 106 for selectively aligning either the first platform mandrel 112 or the second platform mandrel 114 with the cavity 92 of the second die assembly 88. As such, the single machine 120 can switch between the first platform mandrel 112 or the second platform mandrel 114 for pressing the pre-formed billet 36 into the second die assembly 88. By switching between the first and second platform mandrels 112, 114 only one of the first and second platform mandrels 112, 114 is actually doing work to transform the pre-formed billet 36 into the extruded tube 30 while the other one of the first and second platform mandrels 112, 114 is allowed to cool. This type of cooling is referred to as offline cooling because one of the first and second platform mandrel 112, 114 is allowed to cool without delaying or stopping the single machine 120 from continuing to work using the other one of the first and second platform mandrels 112, 114.
The single machine 120 may include the container 116 coupled to the fixed base 104 adjacent the second die assembly 88. The container 116 includes the cooling fluid therein and is configured to receive the second platform mandrel 114 as the first platform mandrel 112 enters the cavity 92 of the second die assembly 88 for cooling the second platform mandrel 114.
Additionally, the mandrel assembly 108 of the single machine 120 may include the third platform mandrel 118 coupled to and extending from the rotatable platform 110 toward the fixed base 104. Rotation of the rotatable platform 110 aligns one of the first platform mandrel 112, the second platform mandrel 114, and the third platform mandrel 118 with the cavity 92 of the second die assembly 88.
When the mandrel assembly 108 of the single machine 120 includes the third platform mandrel 118, the container 116 of the single machine 120 is further defined as the first container 116A and the single machine 120 further comprises the second container 116B. The second container 116B is coupled to the fixed base 104 adjacent the second die assembly 88 and the first container 116A. The second container 116B includes the lubricating fluid therein and is configured to receive the third platform mandrel 118 as the first platform mandrel 112 enters the cavity 92 of the second die assembly 88 and the second platform mandrel 114 enters the first container 116A.
As described above and generally shown in
When the tube is to be the drawn tube 32, the single machine 120 further includes the third die assembly 94 coupled to the fixed base 104 and spaced from the first and second die assemblies 82, 88. The third die assembly 94 defines the cavity 98 configured to receive the extruded tube 30. When the single machine 120 includes the third die assembly 94, the single machine 120 includes the third mandrel 96 coupled to the single press structure 106 and aligned with the cavity 98 of the third die assembly 94. During operation of the single machine 120, the third die assembly 94 is configured to assist with drawing the extruded tube 30 to further elongate the extruded tube 30 to produce the drawn tube 32.
When the third mandrel 96 is present, the first, second, and third mandrels 84, 90, 96 move simultaneously with each other as the single press structure 106 moves towards and away from the fixed base 104 such that the first mandrel 84 enters the cavity 86 of the first die assembly 82, the second mandrel 90 enters the cavity 92 of the second die assembly 88, and the third mandrel 96 enters the cavity 98 of the third die assembly 94 as the single press structure 106 moves towards the fixed base 104.
Typically, the second mandrel 90 has a length of at least 600 millimeters and the third mandrel 96 has a length of at least 1,000 millimeters. Due to the length of the second and third mandrels 90, 96, the single press structure 106 must have a large enough stroke length to accommodate the second and third mandrels 90, 96 while allowing parts to be inserted into and removed from the second and third die assemblies 88, 94.
When the single machine 120 is to produce the drawn tube 32, the method described above further includes the steps of moving the extruded tube 30 from the cavity 92 of the second die assembly 88 to the cavity 98 of the third die assembly 94 and pressing the extruded tube 30 into the cavity 98 of the third die assembly 94 with the third mandrel 96 coupled to the single press structure 106 to elongate the extruded tube 30 and decrease the thickness of the extruded wall 58 of the extruded tube 30 thereby producing the drawn tube 32. It is to be appreciated that the step of pressing the extruded tube 30 may be further defined as drawing the extruded tube 30 by cycling the single press structure 106 towards and then away from the fixed base 104 to elongate the extruded tube 30 and decrease the thickness of the extruded wall 58 of the extruded tube 30 thereby producing the drawn tube 32.
The method has a total drawn tube manufacturing time to produce the drawn tube 32. Because the first, second, and third die assemblies 82, 88, 94 are within the single machine 120 and the because the first, second, and third mandrels 84, 90, 96 are coupled to the single press structure 106, the total drawn tube manufacturing time is minimized relative to conventional tube manufacturing practices. Typically, the total drawn tube manufacturing time to complete the steps of placing a billet 34, pressing the billet 34 to produce the pre-formed billet 36; moving the pre-formed billet 36, and pressing the pre-formed billet 36 to produce the extruded tube 30, moving the extruded tube 30, and pressing the extruded tube 30 to produce the drawn tube 32 is of from about 20 to about 240 seconds, more typically of from about 20 to about 120 seconds, and even more typically of from about 20 to about 40 seconds.
The drawn tube 32 produced by the single machine 120 has a yield strength typically of at least 600 MPa, even more typically of at least 700 MPa, and even more typically of at least 750 MPa.
When the full-float hollow axle tube 76 is desired, the method includes the step of machining the wheel end 62 of the drawn tube 32 to produce the full-float hollow axle tube 76 having the hollow interior 72 that spans the length of the full-float hollow axle tube 76.
When the single machine 120 is to be used to produce the drawn tube 32, the mandrel assembly 108 may be further defined as the first mandrel assembly 108A and the third mandrel 96 may be further defined as a second mandrel assembly 108B. Similar to the mandrel assembly 108 described above, the second mandrel assembly 108B includes the rotatable platform 110 coupled to the single press structure 106 with the rotatable platform 110 rotatable relative to the single press structure 106. The second mandrel assembly 108B also includes the first platform mandrel 112 coupled to and extending from the rotatable platform 110 toward the fixed base 104 and the second platform mandrel 114 coupled to and extending from the rotatable platform 110 toward the fixed base 104. Rotation of the rotatable platform 110 of the second mandrel assembly 108B aligns either the first platform mandrel 112 of the second mandrel assembly 108B or the second platform mandrel 114 of the second mandrel assembly 108B with the cavity 98 of the third die assembly 94.
It is to be appreciated that the method of manufacturing the extruded tube 30 and the method of manufacturing the drawn tube 32 with the single machine 120 may include at least one of the steps of lubricating the second mandrel 90 before the step of pressing the pre-formed billet 36 into the cavity 92 of the second die assembly 88 and cooling the second mandrel 90 before the step of lubricating the second mandrel 90.
In an alternative method to produce the extruded tube 30 with the single machine 120, the method includes the steps of placing the billet 34 into the cavity 86 of the first die assembly 82 and placing the first pre-formed billet 36A having the bore 40 defined in one end 38A thereof into the cavity 92 of the second die assembly 88. The alternative method using the single machine 120 also includes the step of moving the single press structure 106 toward the fixed base 104 after the steps of placing the billet 34 into the first die assembly 82 and placing the pre-formed billet 36 into the second die assembly 88 such that the first mandrel 84 contacts the billet 34 in the first die assembly 82 and the second mandrel 90 contacts the first pre-formed billet 36A in the second die assembly 88. The step of moving the single press structure 106 completes the steps of forming the billet 34 within the cavity 86 of the first die assembly 82 to produce the second pre-formed billet 36B having the bore 40 defined in one end 38A thereof, and extruding the first pre-formed billet 36A within the cavity 92 of the second die assembly 88 to produce the extruded tube 30 having the hollow interior 42.
In the alternative method using the single machine 120 described above, the billet 34 may be further defined as the first billet 34A and the extruded tube 30 may be further defined as the first extruded tube 30A. As such, the alternative method of using the single machine 120 may include the steps of placing the second pre-formed billet 36B into the cavity 92 of the second die assembly 88, placing the second billet 34B into the cavity 86 of the first die assembly 82, and moving the single press structure 106 toward the fixed base 104 after the steps of removing the second pre-formed billet 36B, placing the second pre-formed billet 36 into the first die assembly 82, and placing the second billet 34B into the cavity 86 of the first die assembly 82. The step of moving the single press structure 106 completes the steps of forming the second billet 34B within the cavity 86 of the first die assembly 82 to produce the third pre-formed billet 36C having the bore 40 defined in one end 38A thereof, and extruding the second pre-formed billet 36B within the cavity 92 of the second die assembly 88 to produce the second extruded tube 30B having the hollow interior 42.
As described above and generally shown in
Furthermore, in the alternative method using the single machine 120 described above, the billet 34 may be further defined as the first billet 34A, the extruded tube 30 may be further defined as the first extruded tube 30A, and the single machine 120 further includes the third die assembly 94. In such an alternative method, the alternative method includes the steps of removing the second pre-formed billet 36B from the cavity 86 of the first die assembly 82, placing the second pre-formed billet 36B into the cavity 92 of the second die assembly 88, placing a second billet 34B into the cavity 86 of the first die assembly 82, removing the first extruded tube 30A from the cavity 92 of the second die assembly 88, placing the first extruded tube 30A into a cavity 98 of the third die assembly 94, and moving the single press structure 106 toward the fixed base 104 after the steps of placing the second billet 34B into the first die assembly 82, placing the second pre-formed billet 36B into the second die assembly 88, and placing the first extruded tube 30A into the third die assembly 94 such that the first mandrel 84 contacts the second billet 34B in the first die assembly 82, the second mandrel 90 contacts the second pre-formed billet 36B in the second die assembly 88, and the third mandrel 96 contacts the first extruded tube 30A in the third die assembly 94. The step of moving the single press structure 106 completes the steps of forming the second billet 34B within the cavity 86 of the first die assembly 82 to produce a third pre-formed billet 36C having a bore 40 defined in one end thereof, extruding the second pre-formed billet 36B within the cavity 92 of the second die assembly 88 to produce a second extruded tube 30B having a hollow interior 42, and drawing the first extruded tube 30A within the cavity 98 of the third die assembly 94 to produce a drawn tube 32 having a wall that has a thickness that is reduced relative to the first extruded tube 30A.
The alternative method using the single machine 120 may also include the steps of removing the second extruded tube 30B from the second die assembly 88, placing the second extruded tube 30B into the cavity 98 of the third die assembly 94, moving the single press structure 106 toward the fixed base 104 after the step of placing the second extruded tube 30B into the third die assembly 94 to complete the step of drawing the second extruded tube 30B within the cavity 98 of the third die assembly 94 to produce a second drawn tube 32 having a wall that has a thickness that is reduced relative to the second extruded tube 30B.
When the single machine 120 is to be used to produce the drawn tube 32, the mandrel assembly 108 may be further defined as the first mandrel assembly 108A and the third mandrel 96 may be further defined as a second mandrel assembly 108B. Similar to the mandrel assembly 108 described above, the second mandrel assembly 108B includes the rotatable platform 110 coupled to the single press structure 106 with the rotatable platform 110 rotatable relative to the single press structure 106. The second mandrel assembly 108B also includes the first platform mandrel 112 coupled to and extending from the rotatable platform 110 toward the fixed base 104 and the second platform mandrel 114 coupled to and extending from the rotatable platform 110 toward the fixed base 104. Rotation of the rotatable platform 110 of the second mandrel assembly 108B aligns either the first platform mandrel 112 of the second mandrel assembly 108B or the second platform mandrel 114 of the second mandrel assembly 108B with the cavity 98 of the third die assembly 94.
In each of the manufacturing methods described above, when the third die assembly 94 is present, the method may include a skip stroke process to produce the drawn tube 32. For example, the billet 34 may be disposed within the first die assembly 82 and the extruded tube 30 may be disposed within the third die assembly 94 with the second die assembly 88 remaining empty. The skip stroke method includes the steps of forming the billet 34 within the cavity 86 of the first die assembly 82 to produce the second pre-formed billet 36B and forming the extruded tube 30 within the third die assembly 94 to produce the drawn tube 32.
As generally described above and shown in
The first machine 132 comprises the initial stage second die assembly 128 coupled to the fixed base 104A spaced from the first die assembly 82 and defining the cavity 136 therein with the initial stage second die assembly 128 configured to extrude the pre-formed billet 36 into the preliminarily extruded tube 126. The first machine 132 further comprises the later stage second die assembly 130 coupled to the fixed base 104A spaced from the initial stage second die assembly 128 and defining the cavity 138 therein. The later stage second die assembly 130 is configured to extrude the preliminarily extruded tube 126 into the extruded tube 30.
The first machine 132 comprises the press structure 106A moveable toward and then away from the fixed base 104A. The press structure 106A comprises the first mandrel 84 aligned with the cavity 86 of the first die assembly 82. The press structure 106A further comprises the initial stage second mandrel 140 aligned with the cavity 136 of the initial stage second die assembly 128 and the later stage second mandrel 142 aligned with the cavity 138 of the later stage second die assembly 130. The first mandrel 84 and the initial and later stage second mandrels 140, 142 move simultaneously with each other as the press structure 106A moves towards and then away from the fixed base 104A such that the first mandrel 84 enters the cavity 86 of the first die assembly 82, the initial stage second mandrel 140 enters the cavity 136 of the initial stage second die assembly 128, and the later stage second mandrel 142 enters the cavity 138 of the later stage second die assembly 130 as the press structure 106A moves towards the fixed base 104A.
The manufacturing system 144 further comprises the second machine 134. The second machine 134 comprises the fixed base 104B and the third die assembly 94 coupled to the fixed base 104B and defining the cavity 98 therein. The third die assembly 94 is configured to draw the extruded tube 30 to produce the drawn tube 32. The second machine 134 further comprises the press structure 106B moveable toward and then away from the fixed base 104B. The press structure 106B comprises the third mandrel 96 coupled to the press structure 106B and aligned with the cavity 98 of the third die assembly 94. The third mandrel 96 moves with the press structure 106B as the press structure 106B moves towards and away from the fixed base 104B such that the third mandrel 96 enters the cavity 98 of the third die assembly 94 as the press structure 106B moves towards the fixed base 104B.
One having skill in the art will appreciate that the manufacturing system 144 may comprise the apparatus 102 having the die assemblies 82, 88, 94 and the mandrel assemblies 84, 90, 96 as described above. Furthermore, although the second die assembly 88 and the second mandrel 90 described herein are further defined as the initial and later stage second die assemblies 128, 130 and the initial and later stage second mandrels 140, 142, respectively, it is to be appreciated that the second die assembly 88 and the second mandrel 90 may each be single units.
As also generally described above and shown in
The is tube formed in at least the first machine 132 and the second machine 134 each having the fixed base 104A, B and the press structure 106A, B movable toward the fixed base 104A, B, with the first die assembly 82 coupled to the fixed base 104A of the first machine 132, the second die assembly 88 coupled to the fixed base 104A of the first machine 132 and further defined as the initial stage second die assembly 128 and the later stage second die assembly 130, and the first mandrel 84 coupled to the press structure 106A of the first machine 132, the second mandrel 90 coupled to the press structure 106A of the first machine 132 and spaced from the first mandrel 84 further defined the the initial stage second mandrel 140 and the later stage second mandrel 142. The third die assembly 94 is coupled to the fixed base 104B of the second machine 134 and the third mandrel 96 is coupled to the press structure 106B of the second machine 134.
The method comprises the steps of placing the billet 34 into the cavity 86 of the first die assembly 82 and pressing the billet 34 into the cavity 86 of the first die assembly 82 with the first mandrel 84 coupled to the press structure 106A of the first machine 132 to form the bore 40 at one end of the billet 34 thereby producing the pre-formed billet 36.
The method further comprises the steps of moving the pre-formed billet 36 from the cavity 86 of the first die assembly 82 to the cavity 136 of the initial stage second die assembly 128 and pressing the pre-formed billet 36 into the cavity 136 of the initial stage second die assembly 128 with the initial stage second mandrel 140 coupled to the press structure 106A of the first machine 132 to elongate the pre-formed billet 36 and form the hollow interior 42 therein thereby producing the preliminarily extruded tube 126.
The method further comprises the steps of moving the preliminarily extruded tube 126 from the cavity 136 of the initial stage second die assembly 128 to the cavity 138 of the later stage second die assembly 130 and pressing the preliminarily extruded tube 126 into the cavity 138 of the later stage second die assembly 130 with the later stage second mandrel 142 coupled to the press structure 106A of the first machine 132 to further elongate the preliminarily extruded tube 126 thereby producing the extruded tube 30.
The method further comprises the steps of moving the extruded tube 30 from the cavity 138 of the later stage second die assembly 130 to the cavity 98 of the third die assembly 94 and pressing the extruded tube 30 into the cavity 98 of the third die assembly 94 with the third mandrel 96 coupled to the press structure 106B of the second machine 134 to elongate the extruded tube 30 and decrease the thickness of the wall of the extruded tube 30 thereby producing the drawn tube 32.
It is to be appreciated that each of the steps described above referring to the method of manufacturing the tube with the single machine 120 may be applied to the method of manufacturing the tube with the first and second machines 132, 134, described herein.
The subject invention also provides for an alternative method of manufacturing the tube as shown in
The method comprises the steps of placing the first billet 34A into the cavity 86 of the first die assembly 82, placing the first pre-formed billet 36A having the bore 40 defined in one end thereof into the cavity 136 of the initial stage second die assembly 128, placing the first preliminarily extruded tube 126A having the hollow interior 42 into the cavity 138 of the later stage second die assembly 130, and placing the first extruded tube 30A into the cavity 98 of the third die assembly 94. The method further comprises the steps of moving the press structure 106A of the first machine 132 toward the fixed base 104A after the steps of placing the first billet 34A into the first die assembly 82, placing the first pre-formed billet 36A into the initial stage second die assembly 128, and placing the first preliminarily extruded tube 126A into the later stage second die assembly 130 such that the first mandrel 84 contacts the first billet 34A in the first die assembly 82, the initial stage second mandrel 140 contacts the first pre-formed billet 36A in the initial stage second die assembly 128, and the later stage second mandrel 142 contacts the first preliminarily extruded tube 126A in the later stage second die assembly 130 to complete the steps of forming the first billet 34A within the cavity 86 of the first die assembly 82 to produce the second pre-formed billet 36B having the bore 40 defined in one end thereof, extruding the first pre-formed billet 36A within the cavity 136 of the initial stage second die assembly 128 to produce the second preliminarily extruded tube 126B having the hollow interior 42, and extruding the first preliminarily extruded tube 126A within the cavity 138 of the later stage second die assembly 130 to produce the second extruded tube 30B.
The method further comprises the steps of moving the press structure 106B of the second machine 134 toward the fixed base 104B after the step of placing the first extruded tube 30A into the cavity 98 of the third die assembly 94 to complete the step of drawing the first extruded tube 30A within the cavity 98 of the third die assembly 94 to produce the drawn tube 32 having the wall that has a thickness that is reduced relative to the first extruded tube 30A.
It is to be appreciated that each of the steps described above referring to the alternative method of manufacturing the tube with the single machine 120 may be applied to the alternative method of manufacturing the tube with the first and second machines 132, 134, described herein.
As alluded to above, it is to be appreciated that the apparatus 102 described above may be the single machine 120. Said differently, the single machine 120 may be used to manufacture the article and/or the tube with the inclusion of the mandrel assembly 108 described with the apparatus 102. Additionally, it is to be appreciated that the method of manufacturing the drawn tube 32 having a yield strength of at least 750 MPa can be performed using either the apparatus 102 or the single machine 120 described herein.
While the invention has been described with reference to exemplary embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
This application claims priority to and all advantages of U.S. Provisional Patent Application Nos. 62/093,193, 62/093,197, and 62/093,202, each of which were filed on Dec. 17, 2014, the disclosures of which are specifically incorporated by reference in their entirety.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/US15/66337 | 12/17/2015 | WO | 00 |
| Number | Date | Country | |
|---|---|---|---|
| 62093197 | Dec 2014 | US | |
| 62093202 | Dec 2014 | US | |
| 62093193 | Dec 2014 | US |
