Method for forming center link of connecting rod for variable displacement engine
A method includes powder forging and machining a workpiece that is fractured to divide the workpiece into separate components. In a green form in which the workpiece is formed of compacted powdered metal and has a body that is generally shaped as a parallelepiped with a pair of end faces. The body defines a bore, a pair of V-notches and a pair of channels. The V-notches are formed into the bore parallel to the central axis of the bore and cooperate to define a separation plane. Each of the channels is formed in an associated one of the end faces at a location where the separation plane intersects the end face. During forging, the channels are closed but create a stress riser that aids in directing the fracture when the components are separated from one another.
1. A method comprising:
forming a green workpiece from a powdered metal material, the green workpiece having a body that is generally shaped as a parallelepiped with a peripheral end surface and a pair of end faces that are separated from one another by the peripheral end surface, the body defining a first bore, a second bore, a third bore, a pair of V-notches, and a pair of channels, the first, second and third bores each having a central axis that is perpendicular to the end faces, the central axes of the first, second and third bores being disposed in a common plane such that the second bore is disposed between the first and third bores, the V-notches being formed into the second bore parallel to the central axis of the second bore and cooperating to define a separation plane that is offset from the common plane about the central axis of the second bore by a predetermined offset angle, the predetermined offset angle being an acute dihedral angle between the separation plane and the common plane, wherein a distance between the second bore and the peripheral end surface along the separation plane is greater than a minimum distance between the second bore and the peripheral end surface, each of the channels being formed in an associated one of the end faces at a location where the separation plane intersects the end face;
sintering the green workpiece to form a sintered workpiece;
forging the sintered workpiece to form a forged workpiece in which the channels are at least substantially closed; and
inserting a fracturing tool into the second bore; and
driving the fracturing tool apart while the fracturing tool is inserted into the second bore to fracture the forged workpiece along the separation plane into first and second forged components.
2. The method of claim 1 , wherein the channels in the green workpiece have a depth and a width that are each less than or equal to 3 mm.
3. The method of claim 2 , wherein the depth and the width are each less than or equal to 2 mm.
4. The method of claim 1 , wherein prior to inserting the fracturing tool into the second bore, the method further comprises machining the forged workpiece.
5. The method of claim 4 , wherein machining the forged workpiece comprises sizing the first bore to a predetermined first diameter, sizing the second bore to a predetermined second diameter and sizing the third bore to a predetermined third diameter.
6. The method of claim 4 , wherein machining the forged workpiece comprises tapping a pair of holes, each of the holes being formed perpendicular to the separation plane.
7. The method of claim 1 , wherein the body of the green workpiece defines a pair of annular thrust faces, each of the annular thrust faces being disposed on an associated one of the end faces, and wherein each of the channels has a pair of channel portions, each of the channel portions extending between an associated one of the V-notches and the peripheral end surface.
8. The method of claim 1 , wherein at least one of the channels is formed with a flat bottom.
9. The method of claim 8 , wherein the at least one of the channels is formed with a rectangular or square lateral cross-sectional shape.
10. A method comprising:
forming a green workpiece from a powdered metal material, the green workpiece having a body with a peripheral end surface and a pair of end faces that are separated from one another by the peripheral end surface, the body defining a first bore, a second bore, a third bore, a pair of notches, and a pair of channels, the first, second and third bores each having a central axis that is perpendicular to the end faces, the central axes of the first, second and third bores being disposed in a common plane such that the second bore is disposed between the first and third bores, the notches being formed into the second bore parallel to the central axis of the second bore and cooperating to define a separation plane that is offset from the common plane about the central axis of the second bore by a predetermined offset angle, the predetermined offset angle being an acute dihedral angle between the separation plane and the common plane, each of the channels being formed in an associated one of the end faces at a location where the separation plane intersects the end face;
sintering the green workpiece to form a sintered workpiece;
forging the sintered workpiece to form a forged workpiece in which the channels are at least substantially closed; and
inserting a fracturing tool into the second bore; and
driving the fracturing tool apart while the fracturing tool is inserted into the second bore to fracture the forged workpiece along the separation plane into first and second forged components.
11. The method of claim 10 , wherein a distance between the second bore and the peripheral end surface along the separation plane is greater than a minimum distance between the second bore and the peripheral end surface.
12. The method of claim 10 , wherein at least one of the channels is formed with a flat bottom.
13. The method of claim 12 , wherein the at least one of the channels is formed with a rectangular or square lateral cross-sectional shape.
14. The method of claim 10 , wherein the channels in the green workpiece have a depth and a width that are each less than or equal to 3 mm.
15. The method of claim 14 , wherein the depth and the width are each less than or equal to 2 mm.
16. The method of claim 10 , wherein prior to inserting the fracturing tool into the second bore, the method further comprises machining the forged workpiece.
17. The method of claim 16 , wherein machining the forged workpiece comprises sizing the first bore to a predetermined first diameter, sizing the second bore to a predetermined second diameter and sizing the third bore to a predetermined third diameter.
18. The method of claim 16 , wherein machining the forged workpiece comprises tapping a pair of holes, each of the holes being formed perpendicular to the separation plane.
19. The method of claim 10 , wherein the body of the green workpiece defines a pair of annular thrust faces, each of the annular thrust faces being disposed on an associated one of the end faces, and wherein each of the channels has a pair of channel portions, each of the channel portions extending between an associated one of the notches and the peripheral end surface.