Three-Dimensional Shaping Method

Information

  • Patent Application
  • 20160236278
  • Publication Number
    20160236278
  • Date Filed
    June 23, 2015
    9 years ago
  • Date Published
    August 18, 2016
    8 years ago
Abstract
A three-dimensional shaping method in which the powder supplying blade 2 is able to travel without any problems, in which a control system stores in advance a fine sintered region 11 so that any one of a cross-sectional area or a mean diameter in the horizontal direction, a shaping width and an undercut angle at the end is equal to or less than a predetermined extent, or the control system makes a determination in a sintering step, for said each element, so in the case of the raised sintered portions 12 forming on the upper side of the sintered region 11, a rotating cutting tool 3 cuts the raised sintered portions 12 entirely or partially, thereby achieving the object.
Description
FIELD OF THE INVENTION

The present invention relates to a three-dimensional shaping method in which lamination of a powder material and formation of a sintered layer based on the thus laminated powder material are sequentially repeated, thereby producing a processed article.


DESCRIPTION OF THE RELATED ART

In the described three-dimensional shaping method, it is adopted to repeat a process of sintering for a position at which a processed article is expected to be formed by scanning with the use of an optical beam, after step of formation of the powder layer.


Although the three-dimensional shaping method is accompanied with the characteristics and advantages to the maximum extent in that various types of shapes is adaptable in a processed article, it is unavoidable to often arise a case that a cross-sectional area in a horizontal direction or a mean diameter is equal to or less than a predetermined extent, a case that a shaping width is equal to or less than a predetermined extent, and a case that an undercut angle formed by an upper face and a lower inclined face at the edge is equal to or less than a predetermined extent.


In each of above-described cases, when a sintered region is irradiated with an optical beam, not only a previously expected sintered region is formed only on a powder layer which has already been formed, but also, as shown in FIGS. 11 (a), (b), it is unavoidable to often arise such a case that a raised sintered portion is formed at an upper side from a region of the powder layer.


In the case that such raised sintered portion is formed, when a powder supplying blade travels in order to form a powder layer on a next layer on the upper side of each layer to which sintering is performed, the raised sintered portion will, as shown in FIG. 11 (a), inevitably result in an accident such that the raised sintered portion collides with the powder supplying blade and a sintered region which has already been provided are deformed.


Furthermore, as shown in FIG. 11 (b), the powder supplying blade inevitably collides and stops.


In order to avoid the above-described problem, inevitably, in a stage before traveling of the powder supplying blade for forming a powder layer of the next step, it is necessary to cut the raised sintered portion entirely or partially by using a rotating tool.


In order to cope with each of the cases that has been described previously, a great amount of time and complicated know-how are necessary for clearly distinguishing in advance a region at which the raised sintered portion is formed and also for realizing cutting of the raised sintered portion prior to a step of forming a next powder layer.


Nevertheless, spending a great amount of time does not always lead to find out the raised sintered portion with certainty.


Furthermore, the know-how is based on accumulation of subjective experience at work sites, and no objective standard can be obtained from such know-how.


Taking account the above-described situation, it is impossible to find out conventional technologies for dealing with a raised sintered portion in dealing with possible formation of the raised sintered portion or the raised sintered portion which has already been formed.


For reference, Patent Document 1 explains a problem covering a raised sintered portion on three-dimensional shaping and a method for dealing with the problem (Paragraphs [0006], [0009] and [0045]). However, Patent Document 1 recognizes the problem as a problem of degree of wettability in a stage that a powder layer is irradiated with an optical beam and also dealt with the problem by using metal powder greater in wettability. Therefore, unlike the present invention, no consideration or measures are given to the raised sintered portion in each of the previously described cases.


In Patent Document 2, abnormal drive load with the use of a blade for keeping uniform the surface of a powder layer or an optical method is employed to detect a raised portion due to an abnormal sintered portion (Claim 3, Claim 4). Then, the raised portion due to an abnormal sintered portion is removed, while repeating formation of a sintered layer or after all the sintered layers are completely formed (the paragraph of [Solution] in [Abstract] and Claim 1).


However, where the drive load with use of the blade is employed to detect the raised portion due to an abnormal sintered portion, it is necessary to stop the drive of the blade. On the other hand, it is also quite difficult to detect the abnormal sintered portion perfectly by an optical method.


In Patent Document 3 as well, the abnormal protrusions are detected based on an increase in torque of a motor for driving a blade (Paragraph [0052] with regard to FIG. 6 and Claim 4) or detected by using an optical method for checking the presence or absence of received light (Paragraphs [0061] to [0063] with regard to FIG. 15 and Claim 5). However, as with Patent Document 2, Patent Document 3 also has unavoidable technological defects.


PRIOR ART DOCUMENTS
Patent Documents

Patent Document 1: Japanese Published Unexamined Patent Application No. 2004-277877


Patent Document 2: Japanese Published Unexamined Patent Application No. 2004-277881


Patent Document 3: Us Patent Publication No. 2006/0208396


DISCLOSURE OF THE INVENTION
Problem(s) to be Solved by the Invention

An object of the present invention is to provide a configuration of a three-dimensional shaping method in which there is detected efficiently and reliably a raised sintered part that will develop typically from a fine sintered region in such a case that any one of a horizontal cross section or a mean diameter, a shaping width and an undercut angle between an upper face and a lower inclined face at the edge, of a sintered portion on each layer, is equal to or less than a predetermined extent, thus enabling a powder supplying blade to travel around a next layer positioned on the upper side of the layer concerned without any problems.


Means for Solving the Problems

In order to solve the above problems,


regarding the case that a cross-sectional area or a mean diameter of a sintered site in a horizontal direction is equal to or less than a predetermined extent, basic configurations of the present invention are composed of


(1)-1 a three-dimensional shaping method in which after formation of a powder layer with a predetermined thickness, a step for sintering the powder layer by an optical beam is performed at a predetermined number of times and, thereafter, a periphery thereof is cut, comprising that a control system stores in advance a region at coordinate positions in a horizontal direction and a height direction in which a cross-sectional area or a mean diameter of an expected sintered part in a horizontal direction is equal to or less than a predetermined extent, and when the region at the coordinate positions is present on an individual layer to be sintered, the control system temporarily stocks the region at the coordinate positions, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, a rotating cutting tool travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of a raised sintered portion forming on the upper side of the region at the coordinate position, the rotating cutting tool cuts the raised sintered portion entirely or partially, and


(1)-2 a three-dimensional shaping method in which after formation of a powder layer with a predetermined thickness, a step for sintering the powder layer by an optical beam is performed at a predetermined number of times and, thereafter, a periphery thereof is cut, and comprising that on an individual layer to be sintered, a control system determines a length of a shaping path formed by a continuous line for each scanning of the layer concerned by the optical beam and when the length is determined to be equal to or less than a predetermined extent, the control system temporarily stocks coordinate positions in a horizontal direction and a height direction at a region of the shaping path, whose length has been determined to be equal to or less than the predetermined extent, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, a rotating cutting tool travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of a raised sintered portion forming on the upper side of the region at the coordinate position, the rotating cutting tool cuts the raised sintered portion entirely or partially,


regarding the case that the shaping width of the sintered site is equal to or less than a predetermined extent, basic configurations of the present invention are composed of


(2)-1 a three-dimensional shaping method in which after formation of a powder layer with a predetermined thickness, a step for sintering the powder layer by an optical beam is performed at a predetermined number of times and, thereafter, a periphery thereof is cut, comprising that a control system stores in advance a region at coordinate positions in a horizontal direction and a height direction in which a horizontal width of an expected sintered part is equal to or less than a predetermined extent, and when the region at the coordinate positions is present on an individual layer to be sintered, the control system temporarily stocks the region at the coordinate positions, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, a rotating cutting tool travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of a raised sintered portion forming on the upper side of the region at the coordinate position, the rotating cutting tool cuts the raised sintered portion entirely or partially,


(2)-2 a three-dimensional shaping method in which after formation of a powder layer with a predetermined thickness, a step for sintering the powder layer by an optical beam is performed at a predetermined number of times and, thereafter, a periphery thereof is cut, comprising that on an individual layer to be sintered, a control system determines the number of parallel lines formed by folding back a continuous line for each scanning of the layer concerned by the optical beam, and when the number of the lines is determined to be equal to or less than a predetermined number of the lines, the control system temporarily stocks coordinate positions in a horizontal direction and a height direction at a region of a shaping path in which the number of the lines is determined to be equal to or less than a predetermined amount of lines, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade moving in a horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, a rotating cutting tool travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of a raised sintered portion forming on the upper side of the region at the coordinate position, the rotating cutting tool cuts the raised sintered portion is cut entirely or partially,


regarding the case that an undercut angle formed between an upper face and a lower inclined face at the end is equal to or less than a predetermined extent,


basic configurations of the present invention are composed of


(3)-1 a three-dimensional shaping method in which after formation of a powder layer with a predetermined thickness, a step for sintering the powder layer by an optical beam is performed at a predetermined number of times and, thereafter, a periphery thereof is cut, comprising that a control system stores in advance a region at coordinate positions in a horizontal direction and a height direction in which the undercut angle formed between the upper face and the lower inclined face at the edge of an expected sintered part is equal to or less than a predetermined extent, and when the region at the coordinate positions is present on an individual layer to be sintered, the control system temporarily stocks the region at the coordinate positions, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering concerned has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, a rotating cutting tool travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case that a raised sintered portion is formed which is positioned on the upper side of the region at the coordinate position, the rotating cutting tool cuts the raised sintered portion entirely or partially, and


(3)-2 a three-dimensional shaping method in which after formation of a powder layer with a predetermined thickness, a step for sintering the powder layer by the optical beam is performed at a predetermined number of times and, thereafter, a periphery thereof is cut, comprising that on an individual layer to be sintered, a scanning position at the end of a scanning site of an optical beam is increased horizontally in region and in a state of projecting to a greater extent than a scanning position at the edge of the optical beam on an immediately preceding sintered layer positioned so as to be adjacent to a lower side of the layer concerned at a position lower than the scanning position concerned, and also a height width between both ends thereof is divided by a horizontal width to calculate a ratio, and when the ratio is determined to be equal to or less than a predetermined number, a control system temporarily stocks coordinate positions in a horizontal direction and a height direction at the projection end in which the ratio is determined to be equal to or less than the predetermined extent and in a vicinity region thereof, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering concerned has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, a rotating cutting tool travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of a raised sintered portion forming on the upper side of the region at the coordinate position, the rotating cutting tool cuts the raised sintered portion entirely or partially.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a plan view to explain for leading out a general formula in Example 1.



FIG. 2 is a plan view to explain for leading out a general formula derived in Example 2.



FIG. 3 is a perpendicular sectional view to explain a numerical value of a ratio in Example 3.



FIG. 4 shows a flowchart of forming each sintered layer of the basic configuration (1)-1.



FIG. 5 shows a flowchart of forming each sintered layer of the basic configuration (1)-2.



FIG. 6 shows a flowchart of forming each sintered layer of the basic configuration (2)-1.



FIG. 7 shows a flowchart of forming each sintered layer of the basic configuration (2)-2.



FIG. 8 shows a flowchart of forming each sintered layer of the basic configuration (3)-1.



FIG. 9 shows a flowchart of forming each sintered layer of the basic configuration (3)-2.



FIG. 10 is a side view which shows effects of the present invention in accordance with the basic configurations (1)-1 and (1)-2.



FIG. 11 is a side view which explains problems of a raised sintered portion in conventional technologies, and (a) shows a case that a cross-sectional area or a mean diameter in the horizontal direction is equal to or less than a predetermined extent, while (b) shows a case that an undercut angle between an upper face and a lower inclined face at the end is equal to or less than a predetermined extent.





DESCRIPTION OF THE SYMBOLS




  • 1: Shaped article


  • 11: Sintered region


  • 12: Raised sintered portion


  • 2: Powder supplying blade


  • 3: Tool


  • 4: Powder layer



MODE FOR CARRYING OUT THE INVENTION

Each of the basic configurations (1)-1 and (1)-2 is a method for dealing with the formation of a raised sintered portion 12 resulting from the fact that a cross-sectional area or a mean diameter of a sintered part in the horizontal direction is equal to or less than a predetermined extent. Each of the basic configurations (2)-1 and (2)-2 is a method for dealing with the formation of the raised sintered portion 12 resulting from the fact that a shaping width of the sintered part is equal to or less than a predetermined extent. Each of the basic configurations (3)-1 and (3)-2 is a method for dealing with the formation of the raised sintered portion 12 resulting from the fact that an undercut angle formed between an upper face and a lower inclined face at the end of the sintered part is equal to or less than a predetermined extent.


Of the above-described respective methods, each of the basic configurations (1)-1, (2)-1 and (3)-1 stands on that the control system stores in advance the region at coordinate positions in the horizontal direction and the height direction so that a value described in each of the above-described cases is equal to or less than a predetermined extent, and when a raised sintered portion 12 is formed on the upper side of a sintered region 11, a rotating cutting tool 3 cuts the raised sintered portion 12 entirely or partially according to control based on the storage. On the other hand, each of the basic configurations (1)-2, (2)-2 and (3)-2 stands on that the control system determines whether or not a value described in each of the above-described cases is equal to or less than a predetermined extent, and when the raised sintered portion 12 is formed on the upper side of the sintered region 11, the rotating cutting tool 3 cuts the raised sintered portion 12 entirely or partially according to control based on the determination.


In the basic configuration (1)-1, the control system stores in advance the region at the coordinate positions in the horizontal direction and the height direction in which the cross-sectional area or the mean diameter of the expected sintered part in the horizontal direction is equal to or less than a predetermined extent.


Precisely, the basic configuration (1)-1 stands on that in the case of the raised sintered portion 12 forming on the upper side of the sintered region 11, the sintered portion 12 is cut entirely or partially by a process for each layer described in the flowchart shown in FIG. 4 on the basis of the above-described storing.


Explaining in detail, when each layer is sintered, the region at the coordinate positions in the horizontal direction and the height direction which has been stored by the control system is present on the layer concerned, the control system temporarily stocks the region at the coordinate positions, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade 2 moving in the horizontal direction for forming a powder layer 4 on a next layer on the upper side of the layer concerned, the rotating cutting tool 3 travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof on the basis of instructions of the control system, thereby, in the case of the raised sintered portion 12 forming on the upper side of the region at the coordinate position, the rotating cutting tool 3 cuts the sintered portion 12 entirely or partially.


However, determination on whether or not the region concerned corresponds to a region at the coordinate positions in which the cross-sectional area or the mean diameter in the horizontal direction is equal to or less than a predetermined extent and instructions for the rotating cutting tool 3 on the basis of the determination are all carried out according to an unit of sintered section on each sintered layer.


Usually, π mm2 is set as a baseline of the cross-sectional area which is equal to or less than a predetermined extent. In most cases, 2 mm is set as a baseline of the mean diameter which is equal to or less than a predetermined extent.


In the basic configuration (1)-2, on sintering each layer, the control system determines whether or not the length of a shaping path formed by a continuous line for each scanning by an optical beam on the layer concerned is equal to or less than a predetermined extent.


The above-described determination is based on an empirical rule that a diameter of an optical beam and a line width on scanning are fixed for each scanning by the optical beam and, therefore, the length of the shaping path determines a cross-sectional area or a mean diameter in the horizontal direction.


The method for the basic configuration (1)-2 based on the above-described determination stands on that in the case of the raised sintered portion 12 forming on the upper side of the sintered region 11, the sintered portion is cut entirely or partially by a process for each layer described in the flowchart of FIG. 5.


Explaining in detail, when the above-described length is determined to be equal to or less than a predetermined extent, the control system temporarily stocks the coordinate positions in the horizontal direction and the height direction at the region of the shaping path in which the length is determined to be equal to or less than the predetermined extent, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade 2 moving in the horizontal direction for forming a powder layer 4 on a next layer positioned on the upper side the layer concerned, the rotating cutting tool 3 travels around the region of the coordinate position in the horizontal direction and an outer peripheral vicinity thereof on the basis of instructions of the control system, thereby, in the case of the raised sintered portion 12 forming on the upper side of the region of the coordinate position, the rotating cutting tool 3 cuts the raised sintered portion 12 entirely or partially.


However, the determination on whether or not the length of the shaping path is equal to or less than a predetermined extent and instructions for a rotating and cutting tool 3 based on the determination are all carried out according to an unit of sintered section on each sintered layer.


It is noted that an example of specifically setting the length of the shaping path is as will be described later in Example 1.


In the basic configuration (2)-1, the control system stores in advance the region at the coordinate positions in the horizontal direction and the height direction in which the shaping width of an expected sintered part is equal to or less than a predetermined extent.


Precisely, the basic configuration (2)-1 stands on that in the case of the raised sintered portion 12 forming on the upper side of the sintered region 11, the sintered portion 12 is cut entirely or partially by the process for each layer described in the flowchart of FIG. 6 on the basis of the above-described storage.


Explaining in detail, the region at coordinate positions in a horizontal direction and a height direction stored by the control system exists in the layer concerned on sintering, the control system temporarily stocks the region at the coordinate positions, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade 2 moving in the horizontal direction for forming a powder layer 4 on a next layer on the upper side of the layer concerned, the rotating cutting tool 3 travels around the region of the coordinate position in the horizontal direction and an outer peripheral vicinity thereof on the basis of instructions of the control system, thereby, in the case of the raised sintered portion 12 forming on the upper side of the region at the coordinate position, the rotating cutting tool 3 cuts the raised sintered portion 12 entirely or partially.


However, determination on whether or not the region concerned corresponds to the region at the coordinate position in which a cutting width is equal to or less than a predetermined extent and instructions for the rotating cutting tool 3 on the basis of the determination are all carried out according to an unit of sintered section on each sintered layer.


In most cases, 2 mm is usually set as a baseline of the shaping width which is equal to or less than a predetermined extent.


In the basic configuration (2)-2, on sintering each layer, the control system determines the number of parallel lines formed by folding back a continuous line for each scanning by an optical beam on the layer concerned and determines that the number is equal to or less than a predetermined number. The above-described determination is based on an empirical rule that a diameter of an optical beam and a line width for each scanning on an individual layer are fixed and, therefore, the shaping width is inevitably determined by the number of the lines.


The basic configuration (2)-2 based on the above-described determination stands on that in the case of the raised sintered portion 12 forming on the upper side of the sintered region 11, the raised sintered portion 12 is cut entirely or partially by the process for each layer which is described in the flowchart of FIG. 7.


Explaining in detail, when the above-described number is determined to be equal to or less than a predetermined number, the control system temporarily stocks coordinate positions in a horizontal direction and a height direction at the region of the shaping path in which the number is determined to be equal to or less than the predetermined extent, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade 2 moving in the horizontal direction for forming a powder layer 4 on a next layer positioned on the upper side of the layer concerned, the rotating cutting tool 3 travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof on the basis of instructions of the control system, thereby, in the case where a raised sintered portion 12 forming on the upper side of the region at the coordinate position, the rotating cutting tool 3 cuts the sintered portion 12 entirely or partially.


However, determination on whether or not the number is equal to or less than a predetermined number and instructions for the rotating cutting tool 3 on the basis of the determination are all carried out according to an unit of sintered section on each sintered layer.


It is noted that an example of specifically setting the number of the lines is as will be described later in Example 2.


In the basic configuration (3)-1, the control system stores in advance a region at coordinate positions in which an undercut angle formed between an upper face and a lower inclined face at the end of the sintered part is equal to or less than a predetermined extent.


Precisely, the basic configuration (3)-1 stands on that in the case of the raised sintered portion 12 forming on the upper side of the sintered region 11, the sintered portion 12 is cut entirely or partially by the process for each layer described in the flowchart of FIG. 8 on the basis of the above-described storing.


Explaining in detail, the region at coordinate positions in the horizontal direction and the height direction, after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade 2 moving in the horizontal direction for forming a powder layer 4 on a next layer positioned on the upper side of the layer concerned, the rotating cutting tool 3 travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof on the basis of instructions of the control system, thereby, in the case of a raised sintered portion 12 forming on the upper side of the region at the coordinate position, the rotating cutting tool 3 cuts the raised sintered portion 12 entirely or partially.


It is noted that determination on whether or not the region concerned corresponds to the region at the coordinate positions in which the undercut angle is equal to or less than a predetermined extent and instructions for the rotating cutting tool 3 on the basis of this determination are all carried out according to an unit of sintered section on each sintered layer.


Furthermore, inmost cases, 45 degrees is set as a baseline of the undercut angle which is equal to or less than a predetermined extent.


In the basic configuration (3)-2, on an individual layer to be sintered, a scanning position at the edge of a scanning site of an optical beam is increased horizontally in region and in a state of projecting to a greater extent than a scanning position at the edge of the optical beam on an immediately preceding sintered layer positioned so as to be adjacent to a lower side of the layer concerned at a position lower than the scanning position concerned, and also a height width between both ends thereof is divided by a horizontal width to calculate a ratio, and whether or not the ratio is equal to or less than a predetermined number is used as a base for determination. This is based on an empirical rule that where the ratio is equal to or less than a predetermined number, the undercut angle is also equal to or less than a predetermined extent.


However, both cases are adopted corresponding one case that a scanning direction at the edge of an optical beam on each layer and a scanning direction at the end of the optical beam on a next layer positioned on the upper side of the layer concerned are in the same direction and the other case that they are in the opposite direction from each other.


With the above-described both cases taken into account, the method for the basic configuration (3)-2 stands on that in the case of the raised sintered portion 12 forming on the upper side of the sintered region 11, the sintered portion 12 is cut entirely or partially by the process for each layer described in the flowchart of FIG. 9.


Explaining in detail, on an individual layer to be sintered, a scanning position at the edge of a scanning site of an optical beam is increased horizontally in region and in a state of projecting to a greater extent than a scanning position at the end of the optical beam on an immediately preceding sintered layer positioned so as to be adjacent to a lower side of the layer concerned at a position lower than the scanning position concerned, and also a height width between both ends is divided by a horizontal width to calculate a ratio, and when the ratio is determined to be equal to or less than a predetermined number, the control system temporarily stocks the coordinate positions in the horizontal direction and the height direction at the projection end in which the ratio is determined to be equal to or less than the predetermined extent and an adjacent region thereof, and also after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade 2 moving in the horizontal direction for forming a powder layer 4 on a next layer on the upper side of the layer concerned, the rotating cutting tool 3 travels around the region at the coordinate position in the horizontal direction and an outer peripheral vicinity thereof on the basis of instructions of the control system, thereby, in the case where a raised sintered portion 12 is formed which is positioned on the upper side of the region at the coordinate position in the horizontal direction, cutting the sintered portion entirely or partially.


However, the height width and the horizontal width are different in baseline of setting method, depending on the scanning direction of the optical beam.


Precisely, upon setting the height width and the horizontal width between both ends, where the scanning direction of the optical beam at each end and in the vicinity thereof is along the direction at the end concerned, the coordinate position on traveling at the end concerned is given as a baseline, and where the scanning direction of the optical beam at each end and in the vicinity thereof is not along the direction at the end concerned, the coordinate position at the end of a folding-back region at the end of the optical beam is given as a baseline.


However, determination on whether the ratio is equal to or less than a predetermined number or not and instructions for the rotating cutting tool 3 on the basis of the determination are all carried out according to an unit of sintered section on each sintered layer.


It is noted that an example of specifically setting the ratio is as described later in Example 3.


In the present invention based on each of the basic configurations, even though the raised sintered portion 12 has been formed, as shown in FIG. 10, in a stage before the formation of a next layer positioned on the upper side of the layer concerned, the cutting tool 3 is rotated to cut the raised sintered portion 12 entirely or partially, thus it is possible to avoid collision between the powder supplying blade 2 and the raised sintered portion 12 on a next layer positioned on the upper side of the layer concerned. It is therefore possible to achieve the three-dimensional shaping in an extremely efficient manner.


It is noted that FIG. 10 shows the basic configuration (1)-1 and the basic configuration (1)-2, but the above-described collision can also be avoided in the cases of basic configuration (2)-1, the basic configuration (2)-2, the basic configuration (3)-1 and the basic configuration (3)-2.


Hereinafter, a description will be given with reference to examples.


EXAMPLES
Example 1

In the basic configuration (1)-2, when the diameter of an optical beam in the vicinity of the coordinate region is given as d mm, the width between scanning lines associated with folding-back of the optical beam is given as w mm, and the number of parallel traveling lines associated with folding-back of the optical beam is given as N, Example 1 is characterized in that the length of the shaping path formed for each of the optical beams is expressed by the formula shown below.






N{π(1−d2/4)−(N−1)wd}/{(N−1)w+d}mm  [Formula 1]


The reason for the length of the shaping path expressed by the formula shown below is as follows:






N{π(1−d2/4)−(N−1)wd}/{(N−1)w+d}mm  [Formula 2]


As shown in FIG. 1, in the case that a mean length of the N lines traveling in parallel is L mm, a width of the region surrounded by lines on both sides along the direction orthogonal to the parallel direction is expressed as (N−1)w.


As shown in FIG. 1, each of the (N−1) folding-back regions projects only by a radius of an optical beam of d/2 in the line direction at both ends of each of the N lines.


So, an area of the region which is surrounded by the N lines and also includes the above-described projection regions is expressed as (N−1)w(L+d) mm.


A region projects only by the radius of an optical beam of d/2 in the orthogonal direction also in each of two outside lines in the N lines. A total area of these projecting regions is approximately Ld mm.


Furthermore, at both ends of each of the two outside lines, as shown in FIG. 1, four regions exist with the state surrounded by a quarter circular arc. A total area of the four regions is expressed as πd2/4 mm.


Therefore, as described in the basic configuration (1)-1, where π mm2 is set as an ordinarily adopted baseline in which a cross-sectional area in the horizontal direction is equal to or less than a predetermined extent, the formula shown below is established.





(N−1)w(L+d)+Ld+πd2/4=π  [Formula 3]


And, the formula shown below can be led out.






L={π(1−d2/4)−(N−1)wd}/{(N−1)w+d}mm  [Formula 4]


Therefore, when an entire length of the line in which the mean width of the N lines is given as L mm is given as L″, the formula shown below can be obtained.






L′=NL=N{π(1−d2/4)−(N−1)wd}/{(N−1)w+d}mm  [Formula 5]


Example 2

In the basic configuration (2)-2, Example 2 is characterized in that where a diameter of an optical beam is given as d mm and a width between scanning lines associated with the folded-back optical beam is given as w mm, the number of the lines in the sintered region 11 is a maximum value of integer in terms of a numerical value of 1+(2−d)/w.


The reason for the formula shown below established as the shaping width can be explained as follows with reference to FIG. 2.





1+(2−d)  [Formula 6]


As apparent from FIG. 2, a width of the sintered region 11 formed by N traveling lines of parallel optical beams is expressed as (N−1)w+d.


Therefore, as described in the basic configuration (2)-1, where 2 mm is set as an ordinarily adopted baseline in which the shaping width is equal to or less than a predetermined extent, the formula shown below is established,





(N−1)w+d=2  [Formula 7]


and the formula shown below can be obtained.






N=1+(2−d)/w  [Formula 8]


Example 3

In the basic configuration (3)-2, Example 3 is characterized in that a ratio which is obtained by dividing a height width between both ends by a horizontal width is 1:1.


The grounds thereof are demonstrated by the fact that, as shown in FIG. 3, the undercut angle forms 45 degrees when the ratio is 1:1.


Effect of the Invention

In the present invention which is composed of the basic configurations (1)-1, -2, (2)-1, -2 and (3)-1, -2, a cause for forming a raised sintered portion on each layer is detected in advance efficiently and reliably, and the sintered portion is cut entirely or partially by a rotating cutting tool in a stage before the formation of a next layer positioned on the upper side of the layer concerned. Thereby, it is possible to prevent in advance problems in forming a powder layer on a next layer positioned on the upper side of the layer concerned.


The three-dimensional shaping method of the present invention is able to provide efficient shaping without any problems in traveling of a powder supplying blade, even if a raised sintered portion is formed by sintering a fine sintered region in such a manner that any one of a cross-sectional area or a mean diameter in the horizontal direction, a shaping width and an undercut angle at the edge is made equal to or less than a predetermined extent. Therefore, the method has a great range of applications.

Claims
  • 1. A three-dimensional shaping method comprising the steps of: after formation of a powder layer with a predetermined thickness, sintering the powder layer by an optical beam a predetermined number of times and,thereafter, cutting a periphery thereof,storing by a control system in advance a region at coordinate positions in a horizontal direction and a height direction in which one of a cross-sectional area and a mean diameter of an expected sintered part in a horizontal direction is equal to or less than a predetermined extent, andwhen the region at the coordinate positions is present on an individual layer to be sintered, temporarily stocking the region at the coordinate positions by the control system, andcausing a rotating cutting tool, after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, to travel around the region at the coordinate positions in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of raised sintered portions forming on the upper side of the region at the coordinate positions, so that the rotating cutting tool cuts the raised sintered portions one of entirely and partially.
  • 2. The three-dimensional shaping method according to claim 1, wherein one of: the cross-sectional area is π mm2 andthe mean diameter is 2 mm.
  • 3. A three-dimensional shaping method comprising the steps of: after formation of a powder layer with a predetermined thickness, sintering the powder layer by an optical beam a predetermined number of times and,thereafter, cutting a periphery thereof, andon an individual layer to be sintered, determining by a control system a length of a shaping path formed by a continuous line for each scanning of the layer concerned by the optical beam andwhen the length is determined to be equal to or less than a predetermined extent, temporarily stocking coordinate positions in a horizontal direction and a height direction at a region of the shaping path by the control system, whose length has been determined to be equal to or less than the predetermined extent, andcausing a rotating cutting tool, after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, to travel around the region at the coordinate positions in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of raised sintered portions forming on the upper side of the region at the coordinate positions, so that the rotating cutting tool cuts the raised sintered portions one of entirely and partially.
  • 4. The three-dimensional shaping method according to claim 3, wherein, when a diameter of an optical beam in the vicinity of the coordinate position is given as d mm, a width between scanning lines associated with folding-back of the optical beam is given as w mm and the number of parallel traveling lines formed associated with the folding-back of the optical beam is given as N, the length of the shaping path for each scanning by the optical beam is expressed by the formula shown below. N{π(1−d2/4)−(N−1)wd}/{(N−1)w+d}mm
  • 5. A three-dimensional shaping method comprising the steps of: after formation of a powder layer with a predetermined thickness, sintering the powder layer by an optical beam a predetermined number of times and,thereafter, cutting a periphery thereof,storing by a control system in advance a region at coordinate positions in a horizontal direction and a height direction in which a horizontal width of an expected sintered part is equal to or less than a predetermined extent, andwhen the region at the coordinate positions is present on an individual layer to be sintered, temporarily stocking the region at the coordinate positions by the control system, andcausing a rotating cutting tool, after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, to travel around the region at the coordinate positions in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of raised sintered portions forming on the upper side of the region at the coordinate positions, so that the rotating cutting tool cuts the raised the sintered portions one of entirely and partially.
  • 6. The three-dimensional shaping method according to claim 5, wherein the width is 2 mm.
  • 7. A three-dimensional shaping method comprising the steps of: after formation of a powder layer with a predetermined thickness, sintering the powder layer by an optical beam a predetermined number of times and,thereafter, cutting a periphery thereof,on an individual layer to be sintered, determining by a control system the number of parallel lines formed by folding back a continuous line for each scanning of the layer concerned by the optical beam, andwhen the number of the lines is determined to be equal to or less than a predetermined number of the lines, temporarily stocking coordinate positions in a horizontal direction and a height direction at a region of a shaping path in which the number of the lines is determined to be equal to or less than a predetermined number of lines by the control system, andcausing a rotating cutting tool, after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering has been completed and the lowest position of a powder supplying blade moving in a horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, to travel around the region at the coordinate positions in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of raised sintered portions forming on the upper side of the region at the coordinate positions, so that the rotating cutting tool cuts the raised sintered portions one of entirely and partially.
  • 8. The shaping method by an optical beam according to claim 7, wherein, when a diameter of the optical beam is given as d mm and a width between scanning lines associated with folding-back of the optical beam is given as w mm, the number of the lines at a sintered region is a maximum value of integer in terms of a numerical value of 1+(2−d)/w.
  • 9. A three-dimensional shaping method comprising the steps of: after formation of a powder layer with a predetermined thickness, sintering the powder layer by an optical beam a predetermined number of times and,thereafter, cutting a periphery thereof,storing by a control system in advance a region at coordinate positions in a horizontal direction and a height direction in which the undercut angle formed between the upper face and the lower inclined face at the edge of an expected sintered part is equal to or less than a predetermined extent, andwhen the region at the coordinate positions is present on an individual layer to be sintered, temporarily stocking the region at the coordinate positions by the control system, andcausing a rotating cutting tool, after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering concerned has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, to travel around the region at the coordinate positions in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case that raised sintered portion is formed which is positioned on the upper side of the region at the coordinate positions, so that the rotating cutting tool cuts the raised the sintered portions one of entirely and partially.
  • 10. The three-dimensional shaping method according to claim 9, wherein the angle is 45 degrees.
  • 11. A three-dimensional shaping method comprising the steps of: after formation of a powder layer with a predetermined thickness, sintering the powder layer by an optical beam a predetermined number of times and,thereafter, cutting a periphery thereof,on an individual layer to be sintered, increasing a scanning position at the edge of a scanning site of an optical beam horizontally in region and in a state of projecting to a greater extent than a scanning position at the edge of the optical beam on an immediately preceding sintered layer positioned so as to be adjacent to a lower side of the layer concerned at a position lower than the scanning position concerned, anddividing a height width between both edges thereof by a horizontal width to calculate a ratio, andwhen the ratio is determined to be equal to or less than a predetermined number, temporarily stocking coordinate positions in a horizontal direction and a height direction at the projection edge in which the ratio is determined to be equal to or less than the predetermined number and in a vicinity region thereof by a control system, andcausing a rotating cutting tool, after sintering of the layer concerned is completed, at an intermediate height position between the position of the surface on which the sintering concerned has been completed and the lowest position of a powder supplying blade moving in the horizontal direction for forming a powder layer on a next layer on the upper side of the layer concerned, to travel around the region at the coordinate positions in the horizontal direction and an outer peripheral vicinity thereof according to instructions of the control system, thereby, in the case of raised sintered portions forming on the upper side of the region at the coordinate positions, so that the rotating cutting tool cuts the raised the sintered portions one of entirely and partially.
  • 12. The three-dimensional shaping method according to claim 11, wherein, when on setting a height width and a horizontal width between both ends thereof, the scanning direction of an optical beam at each end and in the vicinity thereof is along the direction at the end concerned, coordinate positions on traveling at the end concerned is given as a baseline, and where the scanning direction of the optical beam at each end and in the vicinity thereof is not along the direction at the end concerned, giving coordinate positions at the end of a folding-back region at the end of the optical beam as a baseline.
  • 13. The three-dimensional shaping method according to claim 11, wherein the ratio is 1:1.
Priority Claims (1)
Number Date Country Kind
2015-027553 Feb 2015 JP national