Fiber reinforced plastic (FRP) materials are widely used in aerospace industry due to its high specific strength and high specific stiffness. FRP materials are composite materials consisting of soft resin matrix and high strength fiber reinforcement. Typical fiber reinforcements include carbon fibers (CFRP), glass fibers (GFRP), Kevlar fibers, and the like. FRP materials are often processed into a laminated structure. FRP materials have excellent in-plane strength, but low inter-laminar strength. Fibers tend to delaminate during machining.
One approach to reduce the fiber delamination is to use an orbital drilling process. Orbital drilling is a holemaking operation by milling in which the center of an end mill orbits about the center of the intended hole while spinning on its own axis and moving in the axial direction. Orbital drilling is also called as circular milling or helical interpolation.
Thus, there is a need to provide a cutting tool that minimizes fiber delamination when machining fiber reinforced plastic materials.
Briefly, according to this invention, there is provided an end mill for orbital drilling of fiber reinforced plastics comprising a shank having a shank diameter; a neck having a neck diameter; and a cutting head having a cutting diameter, a corner radius, a dish angle and a back radius, wherein the neck diameter is about 65 percent to about 90 percent of the cutting diameter, the dish angle is between about 2 degrees to about 6 degrees, and the corner radius is between about 3 percent to about 8 percent of the cutting diameter.
In another embodiment, an end mill for orbital drilling of fiber reinforced plastics has a dish angle between about 2 degrees and about 6 degrees; a helix angle of between about 5 degrees and about 18 degrees; a radial rake angle between about 5 degrees and about 15 degrees; a gashing axial rake angle between about 3 degrees and about 10 degrees; and a primary clearance angle between about 10 degrees and about 18 degrees.
Further features of the present invention, as well as the advantages derived therefrom, will become clear from the following detailed description made with reference to the drawings in which:
Tool Geometry
Referring to
As best seen in
Tool Configurations
In general, the end mill has a dish angle between about 2 degrees to about 6 degrees, a helix angle between about 5 degrees to about 18 degrees, an end teeth radial rake angle between about 0 degrees to about 15 degrees, a peripheral teeth radial rake angle between about 8 degrees to about 16 degrees; a gashing axial rake angle between about 3 degrees to about 10 degrees, and a primary clearance angle between about 10 degrees to about 18 degrees.
The principles of the tool geometry described above can be applied to various cutting tool configurations. To this end, a number of different tool configurations of the end mill 10 were tested and compared using the principles of the tool geometry described above.
In one example shown in
As shown in
In another example shown in
As shown in
In yet another example, the same tool geometry for the 2-flute center cutting end mill was applied to a 4-flute center-cutting end mill 300 shown in
Diamond Coating
The fiber reinforcement used in FRP materials is very abrasive and can cause very short life in an uncoated carbide tool. To improve tool life, a diamond coating of about 12 μm thick is applied to the above mentioned end mills. In one embodiment, the end mill 10 is made from a tungsten carbide (WC) substrate with cemented cobalt (Co) in a range between about 3 to 10 wt. % and a diamond coating having a thickness in a range between about 8 to 20 μm deposited by using a chemical vapor deposition (CVD) process. Testing shows that tool life can be increased by 20 times using the diamond coating. The end mill 10 can also be made of a polycrystalline diamond (PCD) material.
It will be appreciated that the principles of the tool geometry can be applied to both non-center cutting and center cutting end mills for orbital drilling of FRP materials.
The documents, patents and patent applications referred to herein are hereby incorporated by reference.
While the invention has been specifically described in connection with certain specific embodiments thereof, it is to be understood that this is by way of illustration and not of limitation, and the scope of the appended claims should be construed as broadly as the prior art will permit.
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