The device relates to a high performance cutting bade assembly for use in composite placement machines in which the composite material is cut while it is moving relative to the blade assembly.
Traditional high performance bi-metallic cutting blade assemblies in composite placement machines utilize a steel mounting body and harder carbon or diamond compound cutting insert brazed together with a butt or lap joint to bond the two materials together. Failures can occur along the bond line when the joint is subjected to cutting forces. Such failures are most likely to occur in cutting applications in which the material is being cut while it is moving normal to the cutting insert. After a certain number of cuts, the cutting inert becomes dull and needs to be replaced.
It would be desirable to have a bi-metallic cutter assembly that can be subjected to high cutting forces normal to the bond line between a cutting insert and a holder.
It would further be desirable to have a bi-metallic cutter assembly in which the cutting insert could be re-sharpened after becoming dull from use.
Turning now to the drawing figures,
The holder 12 includes a beam 17 which extends from one side of the holder 12 to the other. A first window 18 is formed on one side the beam 17 and a second window 19 is formed on the other side the beam. Other forms and shapes of holders may be used. The cutting insert 15 may be mounted on the beam 17 so that it extends into the first window 18. A leg 29 is formed on the lower portion of the beam as described more fully below. The leg 29 provides lateral support for the insert 15 when it is mounted on the beam 17. An actuator such as a lever, not shown, may engage the second window 19 to drive the cutter assembly in an up-and-down motion as required for the operation of the cutting assembly in a composite placement machine. Other methods of actuation may be used.
The hook profile 31 on the beam 17 engages and mates with the step profile 32 on the insert 15 which includes a first step 34, a second step 35, and a third step 36. The first step 34 on the insert is lower than the second step 35, and the first step 34 is higher than the third step 36. The third step 36 is lower than the second step 35. A first rise 38 on the insert 15 extends from the first step 34 to the second step 35, and a second rise 39 on the insert extends from the second step 35 to the third step 36. The second rise 39 is greater than the first rise 38. The widths of the three steps 34, 35, and 36 are approximately equal to one another. The first rise 38 and the second rise 39 are parallel to one another, and the first step 34, the second step 35 and the third step 36 are perpendicular to the first rise 38 and the second rise 39.
The three feet 24-26 on the beam 17 mate with the three steps 34-36 on the insert. The combined width of the three feet 24-26 on the beam is equal to the combined width of the three steps 34-36 on the insert, and may be equal to the thickness 40 of the cutting insert. The length of the first rise 38 and the second rise 39, when added together, is greater than the thickness 40 of the cutting insert 15.
The cutting insert 15 has a length L measured from the third step 36 to the bottom of the cutting insert 15, whereby the length of the cutting insert 15 allows the cutting insert to be re-sharpened at least three times before the cutting insert needs to be replaced. Dotted lines 44-46 show the approximate profile of the cutting insert 15 after first, second, and third re-sharpening, respectively.
The cutting insert 15 may be brazed in place on the beam 17 of the mounting body 12. The labyrinth joint 20 presents a larger surface area for the purpose of increasing the braze/bonding strength between the cutting insert 15 and beam 17. The first rise 38 on the insert 15 between the first step 34 and second step 35, and the second rise 39 between the second step 35 and third step 36 more than doubles the surface area contact between the insert 15 and the beam 17 compared to the area contact between the horizontal surfaces of the steps 34-36 and the feet 24-26 alone. This provides increased surface area for brazing material to bond the cutting insert 15 and the beam 17 together, and as a result an increased brazing bond is formed compared to the brazing bond between the first, second, and third feet 24-26 with the first, second, and third steps 34-36.
In use, one or more of the cutter assemblies 10 may be mounted in a composite placement machine 47 to apply composite material 42 onto an application surface. Each cutting assembly 10 operates in conjunction with an anvil 48 by being driven in a cutting direction 56 to sever composite material 42 as the material is delivered to the application surface. The labyrinth joint 20 for the cutting insert 15 provides a high integrity j oint between the insert 15 and the beam 17 by providing lateral mechanical support for the cutting insert 15 during the cut. As shown in
The movement of the composite material 42 in the material direction 50 as it is being cut exerts an upward force 52 on the cutting insert 15 that is opposite to the cutting direction 56 and a rightward lateral force 54 that is parallel to the material direction as shown in
Having thus described the device, various modifications and alterations will occur to those skilled in the art, which modifications and alterations will be within the scope of the device as defined by the appended claims.
This application claims the benefit of priority from International Patent Application No. PCT/US17/58009 filed on Oct. 26, 2017 and U.S. Provisional Patent Application No. 62/414,213 filed October 28, 2016, the entire contents of which are hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/US2017/058009 | 10/24/2017 | WO |
Number | Date | Country | |
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62414213 | Oct 2016 | US |