Support and method of shaping workpiece and support
11097497 · 2021-08-24
Assignee
Inventors
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B29C64/135
PERFORMING OPERATIONS; TRANSPORTING
B29C64/386
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y50/00
PERFORMING OPERATIONS; TRANSPORTING
B29C67/0011
PERFORMING OPERATIONS; TRANSPORTING
B29C64/40
PERFORMING OPERATIONS; TRANSPORTING
B29C64/153
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C64/40
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B29C64/135
PERFORMING OPERATIONS; TRANSPORTING
B29C67/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A support for supporting a workpiece from below efficiently while reducing the amount of necessary materials, and a shaping method for shaping the workpiece and support efficiently includes a hollow state support for supporting a workpiece from below, and the hollow state support has a lattice form with crossing of straight linear or curved columnar bodies, wherein a sintered strength at a connecting region with the workpiece is lower than the sintered strength at the other regions.
Claims
1. A method of shaping a hollow state support for supporting a workpiece from below, employing a three-dimensional shaping system, comprising the steps of: a lamination step including the steps of repeating alternation of a powder layer-forming step and a sintering step in which a powder layer is sintered by irradiation with one of a moving laser beam and electron beam, and forming with said lamination step an object of shaping at an upper region as a workpiece and an object of shaping at a lower region as the hollow state support comprising a lattice form with curved columnar bodies in a regular spaced order, and all crossings occurring at the curved columnar bodies, with a sintered strength at a connecting region of the hollow state support with the workpiece being lower than a sintered strength at other regions of the hollow state support, and providing that a degree of sintering of each layer of the hollow state support is lower than a degree of sintering of each layer in the workpiece.
2. The method of shaping a support according to claim 1, further comprising the step of designing a shape of the support at each height position by one of a CAM system and CAE system to adapt a shape and weight of the workpiece.
3. The method of shaping a support according to claim 2, further comprising the step of using the one of the CAM system and CAE system to select a material that is to compose the support.
4. The method of shaping a support according to claim 2, further comprising the steps of forming a single notch formed horizontally at or near a top end thereof for inserting fingers of an operator when the support is to be cut off from the workpiece, and designing the notch by one of the CAM system and CAE system, such that the notch is provided over a plurality of adjacent vertically oriented support members of the hollow state support.
5. The method of shaping a support according to claim 1, further comprising the step of providing the degree of sintering of at least one powder layer formed between a top end of the support and a bottom end of the workpiece to be lower than the degree of sintering at other lower side shaping regions of the support.
6. The method of shaping a support according to claim 1, further comprising the step of omitting sintering in some powder layers among the plurality of powder layers formed between a top end of the support and a bottom end of the workpiece.
7. A method of shaping a hollow state support for supporting a workpiece from below, employing a three-dimensional shaping system, comprising the steps of: a lamination step including the steps of repeating alternation of a powder layer-forming step and a sintering step in which a powder layer is sintered by irradiation with one of a moving laser beam and electron beam, and forming with said lamination step an object of shaping at an upper region as a workpiece and an object of shaping at a lower region as the hollow state support comprising a lattice form with at least one of straight linear columnar bodies and curved columnar bodies crossing each other, with a sintered strength at a connecting region of the hollow state support with the workpiece being lower than a sintered strength at other regions of the hollow state support, designing a shape of the support at each height position by one of a CAM system and CAE system to adapt a shape and weight of the workpiece, and forming a single notch horizontally at or near a top end thereof for inserting fingers of an operator when the support is to be cut off from the workpiece, and designing the notch by one of the CAM system and CAE system, such that the notch is provided over a plurality of adjacent vertically oriented support members of the hollow state support, and providing that a degree of sintering of each layer of the hollow state support is lower than a degree of sintering of each layer in the workpiece.
8. The method of shaping a support according to claim 7, further comprising the step of using the one of the CAM system and CAE system to select a material that is to compose the support.
9. The method of shaping a support according to claim 7, further comprising the step of providing the degree of sintering of at least one powder layer formed between a top end of the support and a bottom end of the workpiece to be lower than the degree of sintering at other lower side shaping regions of the support.
10. The method of shaping a support according to claim 7, further comprising the step of omitting sintering in some powder layers among the plurality of powder layers formed between a top end of the support and a bottom end of the workpiece.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4) Note that the dotted lines indicate the state of control data transmission from a controller to different operating parts.
DESCRIPTION OF EMBODIMENTS OF THE INVENTION
(5) To compare again the construction of basic construction (1) and a lattice form produced by crossing the thin sheet-like supports described in Patent Document 2 (hereunder referred to as “thin sheet-like lattice form”), if it is considered that the linear crossing portions of the thin sheet-like lattice form exhibit the necessary indispensable function for supporting a weight while preventing their own deformation, the columnar lattice form employed by basic construction (1) is evaluated as a structure in which the region of the thin sheet itself is abstracted from the thin sheet-like lattice form, selecting linear crossing sections that support a weight while preventing deformation.
(6) By thus abstracting the region of the thin sheet itself while selecting linear crossing sections from the lattice form, it is possible to achieve both support of the load of the workpiece 2 and reduction in materials.
(7) In the case of a columnar lattice form, it is common to employ an embodiment with a uniform thickness, as shown in
(8) In this embodiment, the cross-sectional area of each region does not change, it is possible to avoid the excessive use of material for formation of extra regions with insignificant and unnecessary thicknesses, resulting from the use of prescribed thicknesses for small sections that is necessary to prevent breakage caused by concentration of strain at sections with small cross-sectional areas when the thickness is not uniform.
(9) In basic construction (1), for an embodiment in which the cross-sectional area in the horizontal direction gradually increases toward the lower side, it is possible to prevent overturning of the support 1 even when the location supporting the workpiece 2 is high, and this likewise applies to the lattice forms of
(10)
(11) As shown in
(12) In the case of a lattice form obliquely crossing with the vertical direction, a bending moment M is generated in each cross-section of the lattice form due to the load of the workpiece 2, and if the curvature radius with bending by bending moment M is represented as ρ, then the following basic general formula is valid:
ρ=(EI)/M [Formula 1]
(where E is the modulus of longitudinal elasticity, or Young's modulus, and I is the secondary moment of the cross-section).
(13) As clearly seen from this general formula, in order to reduce deformation with a larger value for the curvature radius p, a material may be selected having a cross-sectional shape (specifically, a cross-sectional circular shape) with a large Young's modulus E and a large secondary moment I.
(14) Such a material is selected based on whether, in concrete experimentation using lattice-shaped supports 1 conforming to different workpieces 2, the support 1 does not only not break but also essentially does not deform.
(15)
(16) For this embodiment, if the load of the workpiece 2 acting on the cross-section of each lattice form is represented as F and the length of displacement in the vertical direction at the top end of the cross-section of the lattice form is represented as x, then the following basic general formula is valid:
F/S=E(x/L) [Formula 2]
(where S is the cross-sectional area, E is the Young's modulus and L is the length of the support in the vertical direction).
(17) As clearly seen from this general formula, in order to reduce x which represents the degree of deformation, a material may be selected having a high Young's modulus for a given cross-sectional area S.
(18)
(19) In this embodiment, at the lower end and its vicinity, displacement occurs according to the general formula of [Formula 2] above, while the other regions resolve to a bending moment M according to the general formula of [Formula 1] above.
(20) In the case of this embodiment, the support 1 may support the workpiece 2 in a pressure-resistant state at the lower end and its vicinity, while at the upper end, it may support the workpiece 2 in a stable manner by the horizontal lattice sections.
(21) Such a material is selected based on whether, in concrete experimentation using lattice-shaped supports 1 conforming to different workpieces 2, the support 1 does not only not break but also essentially does not deform.
(22) From the viewpoint of convenience of removing the support 1 in basic construction (1), as shown in
(23) In the case of this embodiment, the operator inserts his/her own hand into the notch 11 to allow smooth removal of the support 1 from the workpiece 2.
(24) When the lattice form extends up to the top end of the support 1 in basic construction (1), support of the workpiece 2 may be unstable.
(25) Considering such conditions, basic construction (1) may employ an embodiment in which a flat surface or curved surface 14 for supporting the workpiece 2 is formed at the top end of the lattice form, as shown in
(26) When the workpiece 2 has been situated on the flat surface or curved surface 14, the support 1 supports the workpiece 2 in a stable manner.
(27) In the shaping method according to basic construction (2), as shown in
(28) In this three-dimensional shaping system, similar to a common three-dimensional shaping system, a laser beam or electron beam supply 5, a scanner 6, a powder supply tool 7, a squeegee 8, a table 9 and a controller 10 are employed as essential constituent elements.
(29) Normally, the shape of the support 1 at each height position is designed for shaping by a CAM system or CAE system to adapt the shape and load of the workpiece 2.
(30) When the shape is specifically designed using a CAM system or CAE system, the most suitable shape to adapt the shape and load of a given workpiece 2 is selected based on previously accumulated data.
(31) However, when the shape at different heights is to be designed adapting a new shape and load of a workpiece 2, the nearest data and the shape of the support 1 at different heights corresponding to those data are selected from the previously accumulated data of workpiece 2 shape and load, and a program is employed that corrects the dimensions of the shape at different height positions selected as described above, based on proportional distribution using the proportion between the two sets of data, to allow further automatic design.
(32) An embodiment may of course be employed in which the notch 11 shown in
(33) With basic construction (2) using a CAM and CAE system, therefore, it is possible to very efficiently shape the support 1.
(34) Similar to the requirement for selection of the material composing the workpiece 2 to adapt the function of the workpiece 2, a suitable material is also preferably selected for the support 1 as well, for support of the workpiece 2.
(35) In basic construction (2), an appropriate material may be selected to adapt the thickness of the support 1 and the direction at each height position.
(36) The support 1 and workpiece 2 will naturally differ in the properties of the necessary materials.
(37) That is, since the strength required per unit volume is lower for the support 1 than for the workpiece 2, an embodiment may be employed in which the degree of sintering of the support 1 is lower than the degree of sintering of the workpiece 2.
(38) A specific method for obtaining different degrees of sintering for this purpose may be selected from among:
(39) (1) a method of setting the thickness of the support 1 to be larger than the thickness of the workpiece 2 at each laminating unit 4,
(40) (2) a method of using the same thickness for the laminating units 4, and setting the radiation dose of the laser beam or electron beam per unit area for the support 1 to be lower than for the workpiece 2, and
(41) (3) a method of setting the thicknesses of the laminating units 4 and the radiation dose per unit area to be the same, while conducting irradiation every several laminating units for the support 1 and conducting irradiation every single laminating unit for the workpiece 2.
(42) Based on this selection, it is possible to select a condition for basic construction (2) which does not require as powerful a degree of sintering for the workpiece 2 as for the support 1, thereby allowing efficient production to be carried out.
(43) A description will be given below according to Examples.
Example 1
(44) As a feature of Example 1, the degree of sintering of one or several powder layers formed between the top end of the support 1 and the bottom end of the workpiece 2 is lower than the degree of sintering at the other lower side shaping regions of the support 1.
(45) In Example 1 having this feature, at the stage of completion of the single step in which the support 1 and the workpiece 2 have both been shaped, a region is formed between them wherein the degree of sintering is lower than the degree of sintering of the support 1, and it is possible to easily separate the two.
(46) The small degree of sintering referred to here, which is sufficient for the need, is a degree of sintering that may barely maintain bonding between the workpiece 2 and the support 1 without separation between them even when vibration is produced during working of the workpiece 2.
(47) The criteria for setting such a sintered state may only be confirmed by accumulated experimentation based on trial and error for combinations of different workpieces 2 and the support 1.
Example 2
(48) As a feature of Example 2, in order to finally achieve the feature described above, sintering is omitted in some of the powder layers among the plurality of powder layers formed between the top end of the support 1 and the bottom end of the workpiece 2.
(49) Even if sintering is omitted for some of the powder layers, the sintering of the other regions may maintain bonding between the unsintered powder layers, although the degree of bonding is very minimal compared to that by the actual sintering.
(50) As a result, Example 2 also allows easy separation between the support 1 and the workpiece 2.
(51) The region range for the degree to which sintering of some of the powder layers may be omitted while still allowing maintenance of the bonded state between the support 1 and the workpiece 2 and easy separation, must also be confirmed by accumulated experimentation based on trial and error.
INDUSTRIAL APPLICABILITY
(52) Thus, the present invention achieves both the necessary strength and low economic cost for a support that supports a workpiece, while also creating efficient production conditions for both workpieces and supports, and it is therefore of tremendous value in the field of machine tools.
REFERENCE SIGNS LIST
(53) 1: Support 11: Notch 14: Flat surface or curved surface 2: Workpiece 3: Container 4: Laminating unit by powder layer 5: Laser beam or electron beam supply 6: Scanner 7: Powder supply tool 8: Squeegee 9: Table 10: Controller