ADDITIVE LAYER MANUFACTURED ANVIL FOR ROTARY CUTTING UNIT
20170151611 ยท 2017-06-01
Assignee
Inventors
- Jacques Joseph Philippe Secondi (Monsteroux-Milieu, FR)
- Pierre-Luc Paul Andre DIJON (Aubrives sur Vareze, FR)
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/25
PERFORMING OPERATIONS; TRANSPORTING
C23C24/103
CHEMISTRY; METALLURGY
International classification
B22F3/105
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
C04B41/45
CHEMISTRY; METALLURGY
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
An anvil for a rotary cutting unit includes a shaft having an outside surface and at least one cladded layer applied to at least one portion of the outside surface of the shaft. A method of producing the anvil includes the steps of applying a wear resistant powder material to at least one portion of the outer surface and heating the wear resistant powder material with, for example a laser, to melt the powder and to fuse it into at least one layer on the shaft.
Claims
1. A method of producing an anvil for a rotary cutting unit comprising the steps of: providing a shaft, the shaft having an outer surface; applying a wear resistant powder material to at least one portion of the outer surface; and heating the wear resistant powder material to fuse it into at least one layer on the at least one portion of the outer surface.
2. The method according to claim 1, wherein the shaft is made of a material selected from the group of low carbon steel, medium carbon steel and tool steel.
3. The method according to claim 2, further comprising the step of machining a plurality of apertures in the shaft to reduce its weight.
4. The method according to claim 1, wherein the wear resistant powder material is selected from the group of tool steel powder, high speed stool powder and cemented carbide powder.
5. The method according to claim 1, wherein the step of heating the wear resistant powder material comprises applying a laser beam to melt and fuse the wear resistant powder material to the at least one portion of the outer surface of the shaft.
6. The method according to claim 1, wherein the wear resistant powder material is a mixture of powders.
7. The method according to claim 1, wherein the wear resistant material is a wire of pre-alloyed powder material and the heating step comprises supplying an electrical arc to melt the pre-alloyed powder material and fuse it into the at least one layer.
8. The method according to claim 1, wherein the at least one layer has a thickness of 0.5 to 15 mm.
9. The method according to claim 1, wherein at least two layers are applied successively one on top of each other.
10. The method according to claim 1, wherein the at least one layer includes at least one groove machined therein.
11. The method according to claim 1, wherein the at least one layer is disposed on the entire outer surface of the shaft.
12. The method according to claim 1, wherein the at least one layer is disposed on a plurality of working portions of the shaft.
13. The method according to claim 1, further comprising the step of heating the shaft after forming the at least one layer on the at least one portion thereof.
14. The method according to claim 1, further comprising the step of machining the at least one layer fused on the outer surface of the shaft.
15. The method according to claim 1, wherein the wear resistant material has a hardness of 55 to 70 HRC.
16. An anvil for a rotary cutting unit made according to the method of claim 1.
17. A rotary cutting unit comprising an anvil made according to the method of claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
[0031]
DETAILED DESCRIPTION
[0032] Typically rotary cutting apparatuses include a rotary cutter and an anvil. As shown in
[0033]
[0034] Shaft 20 has opposed ends 22 that are hard enough to support roller bearings or ball bearings (not shown) for rotatably supporting the same in the cutting unit. A cylinder 24 made of low or medium carbon steel can be shrink-fitted on shaft 20.
[0035] Alternatively, as shown in
[0036] As shown in
[0037] The composition of the material of the cladded layer can be mainly based on nickel. Chromium, vanadium and titanium can be added from 0 to 20% in weight. For example, a Ni-based alloy with the composition in weight % of Cr-15%; Fe-4%; Si-4.25%; B-3%; Co-7% and the balance of Ni would reach 60 HRC and be fully dense. Another example, could be Ni; Cr-17%; Si-4%; Fe-4%; B-3.5% and C-1%. Both of which are commercially available.
[0038] The components can be present in a metallic form, alloyed or not, or combined with carbon in carbide phases. Iron, silicon, boron, manganese, copper, aluminum, molybdenum, tungsten, tantalum and niobium can be added in the range of 0 to 8% in weight and can be present in a metallic form, alloyed or not, or combined with carbon in carbide phases. Carbon is present in the range of 0.1 to 2% in solid solution or in carbide phases.
[0039] As used herein, the term cladded or cladding refers to the process of depositing material by which a powdered or wire feedstock material is melted and consolidated by use of a laser, electrical arc, plasma arc, induction plasma, high velocity oxygen fuel (HVOF) or even a simple flame as a heating source, in order to coat a surface with the applied material.
[0040] Optional features can be ground or machined on the cladded layer 30, for example, grooves 34 can be provided to prevent oil contamination on trailing surfaces when the anvil is driven by the rotary cutter.
[0041] Cladded layer 30 can be applied to the entire outer surface 18 of cylinder 24 or shaft 28 as shown in
[0042] Referring to the embodiment of
[0043] As described above, the method of the present invention can be used to produce an anvil for a rotary cutting unit wherein the wear resistant material is used only where it is needed and the base shaft can be reused. Referring to
[0044] In step 44 a wear resistant powder material can be applied to at least one portion of the outer surface. As described above, the wear resistant material can be a powder or a wire. It is made of a wear-resistant and tough material, for instance a Ni-based alloy as described above or a pre-alloyed material. Alternatively, the wear resistant material could be supplied in the shape of a pre-alloyed wire in the case of steels.
[0045] The wear resistant material is sprayed and simultaneously heated at the outer surface of the shaft in step 46 to fuse it into at least one layer on the at least one portion of the outer surface, using for example, an additive layer manufacturing (ALM) method.
[0046] ALM is used to deposit material by using a laser beam to melt a metallic material and fuse the same on a base structure. By applying subsequent layers, one on top of each other, a structural component can be created. The pulses of the laser can control the thickness and width of the layer.
[0047] As described above, the wear resistant material can be applied at predetermined positions on outer surface of the shaft by directing the wear resistant material and heat source, for example, a laser, at the desired locations on the anvil shaft.
[0048] It should be appreciated that hard facing and other technology can be used to form the layers. A laser, plasma, HVOF or electrical arc or a simple flame can be used as a heating source.
[0049] Starting powder and cladding parameters can be controlled in order to improve the microstructure. Parameters such as heating power, material's flow rate, distance to the surface, impact speed and deposition speed are key to control quality (cracks, pores, oxide content). Additional features like protective gas, and pre-heating of the shaft can be used to control the layer's quality. The protective gas can be supplied directly in the gaseous form or can be obtained from precursors that are present in the powder or in the cored wire. It should be appreciated that other features can be used and the present disclosure is not limited to these specifically, but it should be understood to include those known to one with ordinary skill.
[0050] Regarding the starting powder, the control of size distribution can be adapted to the deposition process. Regarding wire, its diameter needs to be appropriate for the process. Further, in the case where macro-pores or micro-pores or such are revealed by grinding, this would affect the cut. For example, some types of anvils are used to cut different type of non-wovens. Some of these are made of fibers as thin as 10 m and the presence of pores would prevent the cutting pressure from being applied thereto.
[0051] The thickness of the cladded layer(s) can vary from 0.5 to 15 mm. At the higher thicknesses it is usually required to clad several layers of the wear-resistant material to reach such thickness.
[0052] Depending on the cladded material, it can be also important to have complementary appropriate heat treatments, in order to guarantee metallurgical quality and dimensional stability (for instance tempering operations).
[0053] A finishing operation, typically grinding, can be performed on the cladded layer(s) to perfect the geometry thereof. Grooves or other features can be formed thereon, as discussed above.
[0054] It should be appreciated that the method of the present invention could be used to clad layers to form a tube and then the tube mounted on the shaft or cylinder by shrink fitting or other method.
[0055] Forming an anvil with an ALM process, as described above, offers significant advantages. For example, the noble, wear resistant material is used only where it is needed and the base shaft can be reused, i.e., when the anvil has been used and cannot be cut anymore, the shaft/cylinder can be reground to refresh the surface and allow further use. Thus the anvil can be reground several times until the layer of noble wear resistant material is completely removed. Thereafter, it is possible to re-clad the shaft, grind it and to give it a new use life.
[0056] Although the present embodiment(s) has been described in relation to particular aspects thereof, many other variations and modifications and other uses will become apparent to those skilled in the art. It is preferred therefore, that the present embodiment(s) be limited not by the specific disclosure herein, but only by the appended claims.