Patent Grant
9126288
This application is a National Phase of PCT/JP2011/053623, filed Feb. 21, 2011, entitled, “LASER CUTTING METHOD, LASER CUTTING NOZZLE, AND LASER CUTTING DEVICE” which claims the benefit of Japanese Patent Application No. 2010-075744, filed Mar. 29, 2010, the contents of which are incorporated herein by reference in their entirety.
The prevent invention relates to a laser cutting method of cutting a workpiece by radiating a laser beam from an opening and spraying an assist gas surrounding the laser beam, a laser cutting nozzle and a laser cutting device.
As is well known, in a case of laser cutting a workpiece such as steel materials, cutting is performed as a laser beam irradiated from a laser oscillator is focused by a condenser lens, a cutting portion is heated, and an assist gas is sprayed from a nozzle so as to surround the laser beam to cover the cutting portion, so that combustion reaction occurs in the cutting portion, or cutting is performed as a metal melted by the laser is blown away.
Various technologies relating to a laser cutting nozzle used in the above laser cutting method have been disclosed to improve the processing efficiency (For example, see Patent Document 1).
Provided that an upstream side in a flow direction of an assist gas is referred to as a base end side and a downstream side is referred to as a front end side, the nozzle hole 102 has a tapered portion 103 whose diameter gradually decreases from a base end side of the nozzle main body 101 toward an opening 102A of a front end of the nozzle hole 102, a cylinder portion 104 connected to a front end side of the tapered portion 103, and a tapered portion 105 connected to a front end side of the cylinder portion 104 and having a diameter that gradually increases toward the opening 102A.
In addition, the base end side of the nozzle main body 101 is composed of a cylinder portion 108 in which a thread formed thereon for mounting on a laser cutting device is formed, a large-diameter portion 109 is formed on a front end side of the cylinder portion 108, and a tapered portion 110 whose diameter gradually decreases toward the opening 102A is formed on a front end side of the large-diameter portion 109.
By the configuration described above, the laser cutting nozzle 100 can perform the laser cutting efficiently.
However, in the case of cutting using the nozzle in the related art, if the roughness of the cutting plane is coarse, sometimes processing is necessary to reduce the surface roughness thereof after the workpiece is cut. Therefore, a laser cutting technology for reducing the surface roughness of the cutting plane becomes necessary.
In consideration of the above-mentioned circumstances, an object of the present invention is to provide a laser cutting method, a laser cutting nozzle and a laser cutting device which, when a workpiece is cut by a laser, makes the surface roughness of the workpiece small by suppressing the occurrence of cutting flaws on a cutting plane.
In order to accomplish the above object, the present invention proposes the following configuration.
According to a first aspect of the present invention, a laser cutting nozzle is configured such that a laser beam is irradiated through a nozzle hole formed in a nozzle main body from an opening of the nozzle hole, and an assist gas surrounding the laser beam is emitted. In addition, the nozzle hole includes a first control flow path, a second control flow path, and a third control flow path formed in sequence from the upstream toward the downstream in a flow direction of the assist gas. In addition, the first control flow path is connected to the second control flow path expanded to an outer peripheral side thereof, and the second control flow path is connected to the third control flow path reduced to an inner peripheral side thereof.
According to a second aspect of the present invention, in the laser cutting nozzle according to the first aspect of the present invention, the first control flow path, the second control flow path, and the third control flow path are each formed in a cylindrical shape and arranged coaxially, and when a diameter of the first control flow path is φA, a diameter of the second control flow path is φB, and a diameter of the third control flow path is φC, the equation φA<φC<φB is satisfied.
In accordance with the laser cutting nozzle according to the above invention, the surface roughness of the cutting plane becomes small in a simple configuration.
According to a third aspect of the present invention, in the laser cutting nozzle according to the second aspect of the present invention, a relation φA:φC=1:1.3−3.0 is satisfied.
In accordance with the laser cutting nozzle according to the above invention, the surface roughness of the cutting plane efficiently becomes small.
According to a fourth aspect of the present invention, in the laser cutting nozzle according to the third aspect of the present invention, a relation φC:φB=1:1.1−3.0 is satisfied.
In accordance with the laser cutting nozzle according to the above invention, the surface roughness of the cutting plane becomes stably small. In other words, if φC:φB=1:1.1−3.0, when the value of φB/φC is 1.1 or more, the surface roughness of the cutting plane becomes stably small.
As a result of a cutting test, the upper limit value of φB/φC is not particularly limited. However, if the value of φB/φC is 3.0 or less, the outer shape of the laser cutting nozzle is prevented from being too much larger, and thus it is easy to handle the nozzle.
According to a fifth aspect of the present invention, in the laser cutting nozzle according to the third or fourth aspect of the present invention, if L2 is a control flow path length of the second control flow path, and L3 is a control flow path length of the third control flow path, the equation L2+L3≧2.0×φA is satisfied.
In accordance with the laser cutting nozzle according to the above invention, the equation L2+L3≧2.0×φA is satisfied. Therefore, the surface roughness of the cutting plane becomes efficiently small.
According to a sixth aspect of the present invention, a laser cutting device includes the laser cutting nozzle according to any one of the first to fifth aspects of the present invention.
According to a seventh aspect of the present invention, there is provided a laser cutting method of cutting a workpiece by irradiating a laser beam from an opening of a nozzle hole formed in a nozzle main body, and emitting an assist gas surrounding the laser beam. In addition, when the assist gas is sprayed from the opening through the nozzle hole, the assist gas passes sequentially through a first control flow path formed in the nozzle hole, a second control flow path connected to the first control flow path and expanded to an outer peripheral side thereof, and a third control flow path connected to the second control flow path and reduced to an inner peripheral side thereof.
In accordance with the laser cutting nozzle, the laser cutting device, and the laser cutting method according to the above invention, the surface roughness of the cutting plane becomes small.
In accordance with the laser cutting nozzle, the laser cutting device, and the laser cutting method according to the present invention, the surface roughness of the cutting plane becomes small.
Hereinafter, a first embodiment of the present invention will be described in detail with reference to
The laser cutting device 1 includes the nozzle 10, a laser oscillator 2, and an assist gas supplying device 3. A laser beam F generated by the laser oscillator 2 is irradiated from a nozzle hole 12 of the nozzle 10, and an assist gas G supplied from the assist gas supplying device 3 is emitted from the nozzle hole 12 so as to surround the laser beam F.
The laser beam F irradiated from the nozzle hole 12 is focused on a cutting portion 6 of a workpiece 5. And, the assist gas G sprayed from the nozzle hole 12 flows so as to surround the laser beam F, and the cutting portion 6 is coated by an atmosphere 7 of the assist gas G. Then, cutting is performed as a combustion reaction occurs by the assist gas G in the cutting portion 6 heated by the laser beam F, or cutting is performed as a metal melted by the laser is blown away.
The assist gas supplying device 3 supplies the assist gas G, which is generated as a gas, for example, such as O2, N2, Ar, Air, or He and a gas selected from H2 and He are mixed, to the nozzle 10 at a pressure of 0.01 to 3.0 MPa.
A base end side of a nozzle main body 11 is composed of a cylinder portion 21 in which a thread formed thereon for mounting on the laser cutting device is formed, a large-diameter portion 22 is formed on a front end side of the cylinder portion 21, and the nozzle hole 12 is formed coaxially with an axis O, and has an outer shape in which a tapered portion 23 whose diameter gradually decreases toward an opening 13 is formed on a front end side of the large-diameter portion 22.
If the upstream side of the assist gas flow direction is a base end side and the downstream side thereof is a front end side, an assist gas inlet port 12D, a first control flow path 12A, a second control flow path 12B, and a third control flow path 12C are formed in sequence from the base end side.
The assist gas inlet port 12D, the first control flow path 12A, the second control flow path 12B, and the third control flow path 12C are formed coaxially with the axis O.
A front end side of the assist gas inlet port 12D is composed of a tapered wall portion 15, which is a part of a conical shape formed in a tapered shape whose diameter gradually decreases toward the first control flow path 12A.
The first control flow path 12A, the second control flow path 12B, and the third control flow path 12C are composed of cylinder wall portions 16, 17 and 18 that are parallel to the axis O. In addition, the control flow paths are connected through stepped portions perpendicular to the axis O, as shown in
As shown in
In addition, it is preferable that relations of φA:φC=1:1.3−3.0, φC:φB=1:1.1−3.0, and L2+L3≧2.0×φA are satisfied.
Meanwhile, in order to prevent a phenomenon of the cutting efficiency being lowered because the laser beam interferes with a nozzle inner wall portion, it is more preferable that the equation 5.0≧(L2+L3)/φA is satisfied.
Next, the operation of the nozzle 10 will be described with reference to
In the graph of
From
(1) If φC/φA=1.0 and φB/φA=1.0, the nozzle in the related art in which φA, φB, and φC are the same diameter is shown. In addition, the surface roughness of the cutting plane is naturally the same level as the related art (Δ).
(2) If φB>φC (=φB/φC>1.0)), that is, if φB/φA is above the straight line S1 and φC/φA>1.0, the surface roughness of the cutting plane becomes smaller than the nozzle in the related art.
Meanwhile, in
In the case of φC/φA being 1.1−1.3, the surface roughness of the cutting plane is gradually reduced from the state (∘) where the surface roughness Rz of the cutting plane is improved to 50-30 μm to the state ( ) where the surface roughness Rz of the cutting plane is greatly improved to 30 μm or less.
When φC/φA>1.3, the surface roughness of the cutting plane becomes the state ( ) where the surface roughness Rz of the cutting plane is greatly improved to 30 μm or less.
Meanwhile, through cutting experiments, it was confirmed that the surface roughness of the cutting plane was improved in the range of φC/φA=1.0−3.0.
(3) In the case of φB>φC (=φB/φC>1.3)), that is, if φB/φA is above the straight line S2 and φC/φA>1.3, the surface roughness of the cutting plane becomes the state ( ) where the surface roughness Rz of the cutting plane is greatly improved to 30 μm or less.
Next, the operation and effect of the nozzle 10 will be described with reference to
In
In this experiment, a nozzle in which the diameter φA of the first control flow path 12A is 4 mm, the diameter φB of the second control flow path 12B is 10 mm and the diameter φC of the third control flow path 12C is 7 mm was used.
Meanwhile, the surface roughness of the cutting plane was evaluated in the range of 5.0≧(L2+L3)/φA where the laser beam is not interfered with by the nozzle inner wall portion.
The following can be confirmed from
(1) The surface roughness of the cutting plane shows that it is better than the related art regardless of (L2+L3)/φA. As (L2+L3)/φA increases, the surface roughness of the cutting plane is reduced, thereby improving the quality.
(2) In the case of (L2+L3)/φA≧2.0, a remarkably stable cutting plane is obtained.
As described above, by satisfying the equation (L2+L3)/φA≧2.0, the surface roughness Rz of 30 μm or less is stably secured.
As described above, according to the nozzle 10 and the laser cutting device 1, the surface roughness of the cutting plane in the laser cutting becomes small.
As a result, it is not necessary to perform a process for further reducing the surface roughness of the cutting plane after the laser cutting. Therefore, the number of processes at the time of the laser cutting decreases, so the cost is reduced.
According to the nozzle 10, even though the consumption of the assist gas G is the same as the consumption in the nozzle in the related art, the surface roughness becomes small.
In addition, by satisfying the equation 5.0≧(L2+L3)/φA, interference between the irradiated laser beam F and the cylinder wall portions 16, 17 and 18 of the nozzle hole 12 is suppressed.
Next, a second embodiment of the present invention will be described with reference to
The nozzle 40 is different from the nozzle 10 in that in the nozzle 40 is formed, instead of the assist gas inlet port 12D formed in a tapered shape in the nozzle 10, an assist gas inlet port 42A, for example, which is connected to the first control flow path 12A through a stepped portion formed by a surface perpendicular to the axis O. Other than that, it is the same as the first embodiment, so the same reference numerals are attached and description will be omitted. The assist gas inlet port 42A is composed of a cylinder wall portion 45 that is parallel with the axis O.
Same as the nozzle 10, if the control flow path length of the first control flow path 12A is L1, the diameter of the first control flow path 12A is φA, the control flow path length of the second control flow path 12B is L2, the diameter of the second control flow path 12B is φB, the third control flow path length of the third control flow path 12C is L3 and the diameter of the third control flow path 12C is φC, the equation φA<φC<φB is satisfied.
Further, it is preferable that relations φA:φC=1:1.3−3.0, φC:φB=1:1.1 −3.0, and the equation L2+L3≧2.0×φA are satisfied.
In order to prevent a phenomenon of the cutting efficiency being lowered by the laser beam being interfered with by the nozzle inner wall portion, it is more preferable that the equation 5.0≧(L2+L3)/φA is satisfied, as in the first embodiment.
Also in the case of using the nozzle 40, the same operation and effect are obtained as with the nozzle 10.
In addition, since the configuration of the nozzle 40 is simple, the nozzle 40 can be easily manufactured. Therefore, the manufacturing cost is reduced.
The present invention is not limited to the above embodiments, but various changes may be made without departing from the spirit of the present invention.
In the embodiments described above, for example, a case in which the assist gas inlet port 12D is configured by a part of a conical shape, and the assist gas inlet port 42A is configured in a cylindrical shape. However, the assist gas inlet ports 12D and 42A may be formed in other than the conical shape or a cylindrical shape. For example, instead of the assist gas inlet port 12D or the assist gas inlet port 42A, the inner wall surface of the assist gas inlet port may be formed as a curved surface of a hemispherical surface, a parabolic surface, or the like formed symmetrically about an axis corresponding to the axis of the nozzle bodies 11 and 41.
In addition, it may be a configuration in which an assist gas inlet port is formed in the nozzle mounting portion of the laser cutting device and an assist gas inlet port is not formed in the nozzle 10.
In the embodiments described above, the case in which the first control flow path 12A, the second control flow path 12B, and the third control flow path 12C are connected through the stepped portion perpendicular to the axis O. However, the first control flow path 12A, the second control flow path 12B, and the third control flow path 12C may be connected, for example, through an inclined plane with respect the a plane perpendicular to the axis O with acceptable level.
In addition, in the embodiments described above, the case in which the first control flow path 12A, the second control flow path 12B, and the third control flow path 12C are composed of the cylinder wall portions 16, 17 and 18 coaxial with the axis O. However, instead of these cylinder wall portions 16, 17 and 18, any one or all of the first control flow path 12A, the second control flow path 12B, and the third control flow path 12C may be formed in a tapered shape wall portion, a barrel-shaped wall portion, a drum-shaped wall portion and the like, or other shape.
In addition, the cylinder wall portions 16, 17 and 18 may be formed in a shape of polygon or ellipse or a shape including these.
Any one or all of the first control flow path 12A, the second control flow path 12B, and the third control flow path 12C may be arranged in positions that are not coaxial with the axis O. For example, they may be arranged eccentrically with respect to the axis O.
The dimensional relations for the diameter and length of the first control flow path 12A, the second control flow path 12B, and the third control flow path 12C shown in the above embodiments may not satisfy the above-mentioned equations. For example, the relations and the equation are not limited to φA:φC=1:1.3−3.0, φC:φB=1:1.1−3.0, and L2+L3≧2.0×φA. In other words, some or all of the above relations may not be satisfied.
The shape of the nozzles 10 and 40 may be any shape.
In the embodiments described above, the cases in which the assist gas inlet ports 12D and 42A for introducing the assist gas G to the nozzle holes 12 and 42 open on the base end sides of the nozzle bodies 11 and 41. However, the inlet of the assist gas G of the assist gas inlet ports 12D and 42A may be formed on side portions of the nozzle bodies 11 and 41.
According to the laser cutting nozzle, laser cutting device and laser cutting method according to the present invention, a cutting plane with a reduced surface roughness is obtained.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2010-075744 | Mar 2010 | JP | national |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/JP2011/053623 | 2/21/2011 | WO | 00 | 9/27/2012 |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2011/122159 | 10/6/2011 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 5609781 | Kaga et al. | Mar 1997 | A |
| 5818009 | Nakata et al. | Oct 1998 | A |
| Number | Date | Country |
|---|---|---|
| 061900582 | Jul 1994 | JP |
| 07214368 | Aug 1995 | JP |
| 2003164984 | Jun 2003 | JP |
| Entry |
|---|
| International Search Report, PCT/JP2011/053623, dated May 24, 2011. |
| Number | Date | Country | |
|---|---|---|---|
| 20130015168 A1 | Jan 2013 | US |
