The present invention relates to metal forming dies and the like, and in particular to a pilot assembly and associated method.
Metal forming dies, such as stamping dies and the like, are well known in the art. Progressive metal forming dies are unique, very sophisticated mechanisms which have multiple stations or progressions that are aligned longitudinally, and are designed to perform a specified operation at each station in a predetermined sequence to create a finished metal part. Progressive stamping dies are capable of forming complex metal parts at very high speeds, so as to minimize manufacturing costs.
Heretofore, the dies used in metal forming processes have typically been individually designed, one of a kind assemblies for a particular part, with each of the various components being handcrafted and custom mounted or fitted in an associated die set, which is in turn positioned in a stamping press. Not only are the punches and the other forming tools in the die set individually designed and constructed, but the other parts of the die set, such as stock lifters, guides, end caps and keepers, cam returns, pilots, etc. are also custom designed, and installed in the die set. Current die making processes require carefully machined, precision holes and recesses in the die set for mounting the individual components, such that the same are quite labor intensive, and require substantial lead time to make, test, and set up in a stamping press. Consequently, such metal forming dies are very expensive to design, manufacture, and repair or modify.
The metal part can be accurately located in an individual working station by means of a previously formed hole on the part being placed over a pilot, which registers the part before the work is performed. The pilot is mounted in one of the die members and the part is presented to the pilot. The pilot usually has a shaped end that makes it easier to enter the formed hole on the part. Much of engagement into locating the hole in the part is dependent upon the work being performed in the tool. The part may need to be lifted prior to or after work is performed. The part is usually located on the pilot in the working position and potentially the lifted position as well. These pilots can be purchased as standard components or home-made by a shop.
The shaped end of the pilot that enters the formed hole in the metal part comes in many shapes, such as a short taper, long taper, acute-angle, bullet nose, parabolic point, spherical, and chamfered.
While such prior pilot assemblies have been successful, they are rather expensive and time-consuming to construct and install in an associated die set, such that further improvements and enhancements to the same, as well as metal forming dies generally, would be clearly advantageous and are disclosed herein.
One aspect of the present invention is a multi-station metal forming die having at least two mutually converging and diverging die members between which an elongate stock is shifted longitudinally to form parts from the stock incorporating a pilot assembly. The pilot assembly includes a pilot operably supported on one of the die members. The pilot has an outer end oriented toward the stock, an oppositely disposed inner end away from the stock, and a medial portion disposed axially between the outer and inner ends. The pilot has a generally cylindrical shaped shoulder portion disposed at the medial portion, having a first diameter. The pilot also has a generally cylindrically shaped body portion disposed at the inner end of the pilot that has a second diameter which is less than the first diameter of the shoulder portion. The difference in diameters forms a first annularly shaped, radially oriented shoulder therebetween. The pilot also has a generally tapered transition portion disposed at the outer end. The generally tapered transition portion includes a generally cylindrical innermost portion disposed adjacent to the generally cylindrically shaped shoulder portion of the pilot. The generally cylindrical innermost portion has a third diameter that is less than the first diameter of the shoulder portion to define a second annularly shaped, radially oriented shoulder therebetween for securing said pilot in an associated pilot mounting aperture in the die member. The generally tapered transition portion of the pilot also has an outermost portion extending from a generally cylindrical portion, having a fourth diameter which is smaller than the third diameter. The generally tapered transition portion of the pilot also includes a shaped portion that tapers from the third diameter to the fourth diameter. The pilot assembly also includes at least one fastener relief formed in a portion of the generally cylindrically shaped shoulder portion of the pilot. The pilot assembly also includes at least one mounting fastener having an enlarged head portion that is at least partially received in the fastener relief, and a shank portion anchored in the die member to secure the pilot to the die member.
In another aspect of the present invention is a pilot assembly for a metal forming die in which a stock is formed into at least one part. The pilot assembly includes a pilot operably supported on a die. The pilot has an outer end oriented toward the stock, an operably disposed inner end oriented away from the stock and a generally cylindrically shaped shoulder therebetween having a first diameter. The pilot also includes a generally cylindrical shaped body portion disposed at the inner end having a second diameter that is less than the first diameter of the shoulder portion to define a first annularly shaped shoulder therebetween. The pilot also has a generally tapered transition portion disposed at the outer end. The generally tapered transition portion includes a generally cylindrical innermost portion having a third diameter disposed adjacent to the generally cylindrically shaped shoulder portion. The third diameter is less than the first diameter of the shoulder portion, defining a second shoulder for securing the pilot in a pilot mounting aperture in the die member. The generally tapered transition portion also includes an outermost portion extending from a generally cylindrical portion that has a fourth diameter that is smaller than the third diameter. The generally tapered transition portion also includes a shaped portion extending from the generally cylindrical portion having a fourth diameter which is smaller than the third diameter. The pilot assembly also has at least one shaped fastener relief formed into a portion of the generally cylindrically shaped body portion of the pilot. The pilot assembly also includes at least one mounting fastener having an enlarged head portion, and a shank portion anchored in the die member to securely mount the pilot to the die member. The pilot assembly also includes at least one shaped washer that is recessed on the at least one mounting fastener to engage at least a portion of the shaped fastener relief.
Yet another aspect of the present invention is a pilot assembly for engaging a hole in a stock. The pilot assembly includes a pilot having an outer end oriented toward the stock, an oppositely disposed inner end oriented away from the stock, and a medial portion disposed axially between the outer and the inner ends. The pilot includes a generally cylindrically shaped shoulder portion disposed at the medial portion, having a first diameter. The pilot includes a generally cylindrically shaped body portion disposed at the inner end having a second diameter that is less than the first diameter of the shoulder portion to define a first annularly shaped, radially oriented shoulder therebetween. The pilot also includes a generally tapered transition portion disposed at the outer end. The generally tapered transition portion includes a generally cylindrical innermost portion disposed adjacent to the generally cylindrically shaped shoulder portion of the pilot, with a third diameter that is less than the first diameter of the shoulder portion, to define a second annularly shaped, radially oriented shoulder therebetween. The generally tapered transition portion also includes an outermost portion extending from a generally cylindrical portion having a fourth diameter, which is smaller than the third diameter. The generally tapered portion also includes a tapered portion that extends from the third diameter to the fourth diameter. The pilot also includes at least one fastener relief, having a tapered portion, formed into a portion of the generally cylindrically shaped shoulder portion of the pilot. The pilot assembly includes at least one mounting fastener with a shaped washer that engages the shaped portion of the at least one fastener relief.
These and other advantages of the invention will be further understood and appreciated by those skilled in the art by reference to the following written specification, claims, and appended drawings.
For purposes of description herein, the terms “upper,” “lower,” “right,” “left,” “rear,” “front,” “vertical,” “horizontal” and derivatives thereof shall relate to the invention as oriented in
The reference numeral 2 (
The pilot assembly 2 includes an outer end 16 that will be oriented toward the stock 6, an oppositely disposed inner end 14 that will be oriented away from the stock 6, and a medial portion 12 disposed axially between the outer end 16 and the inner end 14, as illustrated in
The outer end 16 of the pilot assembly 2 has a generally cylindrical innermost portion 26 that is disposed adjacent to the medial portion 12 of the pilot assembly 2. The generally cylindrical innermost portion 26 has a third diameter 46 that is less than the first diameter 42 thereby forming a second annularly shaped, radially oriented shoulder 28 therebetween. The outer end 16 of the pilot assembly 2 also includes a generally cylindrical portion 20 at the outermost portion of the outer end 16, having a fourth diameter 44 that is less than the third diameter 46. The outer end 16 of the pilot assembly 2 also includes a generally conically shaped outermost portion 24 that extends from the generally cylindrically shaped portion 20 having a fourth diameter 44. A curved radial portion 22 can be located between the generally conically shaped outermost portion 24 and the generally cylindrical portion 20 that has the fourth diameter 44.
As illustrated in
At least one fastener relief 32 is formed into the pilot assembly 2.
At least one fastener 50 is used to secure the pilot assembly 2 to the die member 4. The fastener 50 includes an enlarged head 52 and a shank 54. As illustrated in
A shaped washer 62 includes a tapered surface 63 that engages the tapered surface 34 of the fastener relief 32 when the fastener 50 is secured into the die member 4, as illustrated in
In order to install the pilot assembly 2 into the die member 4, a pilot mounting aperture 70 is formed in the die member 4. The pilot mounting aperture 70 includes a larger diameter portion 76 and a smaller diameter portion 74 with an integrally formed shoulder 72 therebetween, as shown in
The die member 4 further includes a fastener aperture 56. The fastener aperture 56 includes a portion 60 shaped to receive the enlarged head 52 and the shaped washer 62. The fastener aperture 56 further includes a threaded portion 58, shaped to receive the shank portion 54 of the fastener 50, as shown in
The illustrated pilot assembly 2 has a one-piece construction formed from a solid bar of rigid material, such as metal or the like. Thus, all machining operations on the solid bar of rigid material can be made during a single machine setup, so as to achieve greater accuracy and consistency of the pilot assembly 2, as well as reduced manufacturing costs. As illustrated in
As illustrated in
Another embodiment of the pilot assembly 102 is illustrated in
The pilot assembly 102 is secured to the die member 4 using a fastener 130 with an enlarged head 131 and a shank portion 132. The die member 4 has a pilot aperture 140 that closely receives the inner end 104 of the pilot assembly 102. The die member 4 also has a fastener aperture 133 that receives the fastener and the shaped washer 120. The shaped washer 120 has a shaped surface 122 that can be of any shape that abuts a corresponding shaped fastener surface 170 on the inner end 104 of the pilot assembly 102. In the illustrated example, the shaped fastener surface 170 and the shaped surface 122 of the shaped washer 120 have curved surfaces that abut each other. However, the shaped surface 122 of the shaped washer 120 and the shaped fastener surface 170 could have other shapes that engage each other to secure the pilot assembly 102 when the fastener 130 is installed in the die member 4. Alternatively, the shaped surface could be formed on the fastener 130 directly to engage the shaped fastener surface 170 when a washer is not used.
As illustrated in
In the foregoing description, it will be readily appreciated by those skilled in the art that modifications may be made to the invention without departing from the concepts disclosed herein. Such modifications are to be considered as included in the following claims, unless these claims by their language expressly state otherwise.
It will be understood by one having ordinary skill in the art that construction of the present disclosure and other components is not limited to any specific material. Other exemplary embodiments of the disclosure disclosed herein may be formed from a wide variety of materials, unless described otherwise herein.
For purposes of this disclosure, the term “coupled” or “operably coupled” (in all of its forms, couple, coupling, coupled, etc.) generally means the joining of two components (electrical or mechanical) directly or indirectly to one another. Such joining may be stationary in nature or movable in nature. Such joining may be achieved with the two components (electrical or mechanical) and any additional intermediate members being integrally formed as a single unitary body with one another or with the two components. Such joining may be permanent in nature or may be removable or releasable in nature unless otherwise stated.
For purposes of this disclosure, the term “connected” or “operably connected” (in all of its forms, connect, connecting, connected, etc.) generally means that one component functions with respect to another component, even if there are other components located between the first and second component, and the term “operable” defines a functional relationship between components.
It is also important to note that the construction and arrangement of the elements of the present disclosure as shown in the exemplary embodiments is illustrative only. Although only a few embodiments of the present innovations have been described in detail in this disclosure, those skilled in the art who review this disclosure will readily appreciate that, unless otherwise described, many modifications are possible (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters, mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter recited. For example, elements shown as integrally formed may be constructed of multiple parts or elements shown as multiple parts may be integrally formed, the operation of the interfaces may be reversed or otherwise varied, the length or width of the structures and/or members or connector or other elements of the system may be varied, the nature or number of adjustment positions provided between the elements may be varied. It should be noted that the elements and/or assemblies of the system may be constructed from any of a wide variety of materials that provide sufficient strength or durability, in any of a wide variety of colors, textures, and combinations. Accordingly, all such modifications are intended to be included within the scope of the present innovations. Other substitutions, modifications, changes, and omissions may be made in the design, operating positions, and arrangement of the desired and other exemplary embodiments without departing from the spirit of the present innovations.
It will be understood that any described processes or steps within described processes may be combined with other disclosed processes or steps to form structures within the scope of the present disclosure. The exemplary structures and processes disclosed herein are for illustrative purposes and are not to be construed as limiting.
It is also to be understood that variations and modifications can be made on the aforementioned structures and methods without departing from the concepts of the present invention, and further it is to be understood that such concepts are intended to be covered by the following claims unless these claims by their language expressly state otherwise.
The present application is a continuation of and claims priority under 35 U.S.C. § 120 to commonly assigned, U.S. Pat. No. 11,517,955, issued Dec. 6, 2022, entitled TAPERED TRANSITION PILOT, which claims the priority benefits under the provisions of 35 U.S.C. § 119, basing said claim of priority on related U.S. Provisional Application No. 62/749,326 filed Oct. 23, 2018, which is incorporated in its entirety herein by reference.
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Number | Date | Country | |
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20230041897 A1 | Feb 2023 | US |
Number | Date | Country | |
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62749326 | Oct 2018 | US |
Number | Date | Country | |
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Parent | 16658192 | Oct 2019 | US |
Child | 17969236 | US |