METHOD FOR FORMING MULTI-MATERIAL MECHANICAL FUNCTIONAL MEMBER IN ADDITIVE MANUFACTURING AND PRODUCT

Abstract

A method for forming a multi-material mechanical functional member in additive manufacturing. The method includes the following steps: S1: dividing an object to be formed into a plurality of portions, analyzing and measuring mechanical properties of each portion, and constructing a unit cell library; S2: forming a lattice structure by using a unit cell structure in the unit cell library to obtain the lattice structure corresponding to each portion; S3: selecting a raw material of the lattice structure, measuring and comparing mechanical properties of each lattice structure with the mechanical properties of each portion of the object to be formed, where when the mechanical properties of each portion are satisfied, the lattice structure is the required lattice structure, otherwise, step S2 is repeated; and S4: forming a three-dimensional model by a method of additive manufacturing to accordingly obtain the required object to be formed.

Claims

1. A method for forming a multi-material mechanical functional member in additive manufacturing, comprising: S1: dividing an object to be formed comprising a plurality of types of materials into a plurality of portions according to the different types of materials, analyzing and measuring mechanical properties of each portion, and constructing a database comprising a plurality of unit cell structures, that is, a unit cell library; S2: selecting one unit cell structure from the unit cell library for each portion of the object to be formed and forming a lattice structure by using the unit cell structure to obtain the lattice structure corresponding to each portion of the object to be formed; S3: selecting a raw material of the lattice structure, measuring and comparing mechanical properties of each lattice structure with the mechanical properties of each portion of the object to be formed in step S1, wherein when the mechanical properties of the lattice structure corresponding to each portion are not less than the mechanical properties of each portion of the object to be formed in step S1, the lattice structure is the required lattice structure, otherwise, step S2 is repeated; S4: assembling the lattice structures corresponding to the portions obtained in step S3 into a three-dimensional model of the object to be formed, wherein the three-dimensional model is formed by a method of additive manufacturing to accordingly obtain the required object to be formed.

2. The method for forming the multi-material mechanical functional member in additive manufacturing according to claim 1, wherein the raw material in step S3 of selecting the raw material of the lattice structure is a material, that is, the raw materials of the lattice structures corresponding to the portions are the same and all are the selected materials.

3. The method for forming the multi-material mechanical functional member in additive manufacturing according to claim 1, wherein a method of measuring the mechanical properties of each portion in step S1 is implemented through experimental measurement or finite element simulation.

4. The method for forming the multi-material mechanical functional member in additive manufacturing according to claim 1, wherein mechanical parameters of the unit cell structures in the unit cell library are known in step S1, and the mechanical parameters comprise Young's modulus, bulk modulus, and shear modulus.

5. The method for forming the multi-material mechanical functional member in additive manufacturing according to claim 1, wherein each unit cell structure in the unit cell library is preferably a simple cube, a face-centered cube, a body-centered cube, a regular octahedron, an octet truss, or a triply periodic minimal surface in step S1.

6. The method for forming the multi-material mechanical functional member in additive manufacturing according to claim 1, wherein the step of assembling the lattice structures into the three-dimensional model of the object to be formed in step S4 further comprises: setting connection structures at connection interfaces of different portions, such that the three-dimensional model obtained after assembly meets mechanical property requirements of the overall object to be formed.

7. The method for forming the multi-material mechanical functional member in additive manufacturing according to claim 1, wherein the method of additive manufacturing is selected according to the selected raw material in step S4, laser selective sintering or a laser sintering technology is selected for a metal material, fused deposition modeling is used for engineering plastics, and photocuring molding is selected for a photosensitive material.

8. A product prepared and obtained through the method according to claim 1.

9. A product prepared and obtained through the method according to claim 2.

10. A product prepared and obtained through the method according to claim 3.

11. A product prepared and obtained through the method according to claim 4.

12. A product prepared and obtained through the method according to claim 5.

13. A product prepared and obtained through the method according to claim 6.

14. A product prepared and obtained through the method according to claim 7.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0022] FIG. 1 is a flow chart of a method for forming a multi-material mechanical functional member in additive manufacturing according to a preferred embodiment of the disclosure.

[0023] FIG. 2 is a schematic diagram of direct connection between side surfaces of a face-centered cubic lattice structure and an octet-truss lattice structure according to a preferred embodiment of the disclosure.

[0024] FIG. 3 is a diagram of direct connection between sides of a simple cubic lattice structure and a modified regular octahedral lattice structure according to a preferred embodiment of the disclosure, where (a) is a schematic diagram of connection, and (b) is a modified connection plane view of the regular octahedral lattice structure connected to the simple cubic structure.

[0025] FIG. 4 is a schematic diagram of indirect connection between side surfaces of the simple cubic lattice structure and the regular octahedral lattice structure through a solid plate according to a preferred embodiment of the disclosure.

[0026] FIG. 5 is a schematic diagram of a multi-material mechanical functional member to be formed constructed according to a preferred embodiment of the disclosure.

[0027] FIG. 6 is a schematic diagram of a single-material functional member prepared by the multi-material mechanical functional member shown in FIG. 5 according to the method of the disclosure according to a preferred embodiment of the disclosure.

[0028] FIG. 7 is a top view of FIG. 6 constructed according to a preferred embodiment of the disclosure.

DESCRIPTION OF THE EMBODIMENTS

[0029] In order to make the objectives, technical solutions, and advantages of the disclosure clearer and more comprehensible, the disclosure is further described in detail with reference to the drawings and embodiments. It should be understood that the specific embodiments described herein serve to explain the disclosure merely and are not used to limit the disclosure. In addition, the technical features involved in the various embodiments of the disclosure described below can be combined with each other as long as the technical features do not conflict with each other.

[0030] As shown in FIG. 1, a method for forming a multi-material mechanical functional member in additive manufacturing is provided, and the method includes the following steps. Mechanical properties of different portions of a multi-material mechanical functional member are measured. A raw material for preparing a single-material mechanical functional member is selected. A unit cell library is constructed, and a lattice structure formed by an appropriate unit cell type, size, and periodic array mode are selected. Mechanical properties of the formed lattice structure are measured, and if requirements are not satisfied, selection of the unit cell type, size, and periodic array mode of the lattice structure executed in the previous step is repeated. If the requirements are satisfied, the single-material mechanical functional member is are prepared by an additive manufacturing technology.

[0031] Further, mechanical properties of various portions of the multi-material mechanical functional member is performed, and such measurement of the mechanical properties is performed through experiments or finite element simulation (FEM).

[0032] Different portions of the multi-material mechanical functional member have varying mechanical properties, and the portions with the same mechanical properties are treated as an entity. Therefore, the multi-material mechanical functional member has a (a=1, 2, 3, 4, . . . , and n) entities of different mechanical properties. The mechanical properties of the a entities which are obtained by dividing the multi-material mechanical functional member are calculated directly by experimental measurement or CAD modeling and then are imported into FEM software.

[0033] Further, the raw material for preparing the single-material mechanical functional member is selected, and such selection includes reasonable selection which is made according to the mechanical properties possessed by each portion of the multi-material functional member, costs of the raw material, and an application scenario of the functional member.

[0034] Since mechanical properties of a lattice unit cell prepared based on a single material are less than those of a solid material, a range of tunable mechanical properties of a lattice structure prepared based on a single material is less than that of a solid single material. Therefore, the corresponding mechanical properties of a selected single material need to be greater than those of any one of the a entities obtained by dividing the multi-material mechanical functional member. If more than 1 raw material meets the above requirement, selection may be reasonably made according to the costs of the raw material and the application scenario of the single-material mechanical functional member.

[0035] Further, regarding the construction of the unit cell library, selection of the lattice structure formed by the appropriate unit cell type, size, and periodic array mode includes reasonable combination of a self-designed unit cell or use of an existing unit cell.

[0036] A material library is required to include a variety of lattice unit cells, and lattice unit cell types are independently designed using CAD. The mechanical properties of the unit cell calculated in the finite element simulation (FEM) software include mechanical parameters such as Young's modulus, bulk modulus, and shear modulus. According to the calculation results, change curves and equations of mechanical parameters with conditions (truss size, unit cell diameter, etc.) are summarized and imported into mathematical calculation software such as MATLAB. Mathematical calculation software such as the MATLAB may be used to manually change the unit cell size and periodic array mode and calculate the change law of the changed mechanical parameters. The lattice unit cells that are designed by researchers are adopted, such as a simple cube (SC), face-centered cube (FCC), body-centered cube (BCC), regular octahedron, octet truss, and triply periodic minimal surface (TPMS), etc., and change formulas of the corresponding mechanical properties with the unit cell size and periodic array mode are stored in the mathematical calculation software such as the MATLAB.

[0037] According to the size and mechanical properties of the 1.sup.4 entity obtained by dividing the input multi-material functional member as well as the mechanical parameters of the selected single material, an appropriate unit cell type, size, and periodic array mode are designed, and there are b.sub.1 (b=1, 2, 3, 4, . . . , n) types of matched lattice structures formed by corresponding unit cell type, size, and periodic array mode. One of the lattice structures is selected to replace the 1.sup.st entity obtained by dividing the multi-material mechanical functional member of multiple materials, and the remaining b.sub.1-1 lattice structures are treated as candidates. In the same way, the above method is also applied to the 2.sup.nd, 3.sup.rd, 4.sup.th, . . . , and a.sup.th entities obtained by dividing the multi-material mechanical functional member. Finally, a lattice structures are selected to replace the a entities obtained by dividing the multi-material mechanical functional member. The remaining b.sub.2-1, b.sub.3-1, b.sub.4-1, . . . , and b.sub.a-1 lattice structures are treated as candidates.

[0038] Further, the mechanical properties of the selected a lattice structures are measured, including verification of whether the mechanical properties of the lattice structures meet the requirements.

[0039] Irregular lattice structures may be formed after lattice unit cell arrays. The mechanical properties calculated based on the lattice unit cells in MATLAB may deviate from actual applications, which needs to be further verified by finite element simulation (FEM). If the mechanical properties conform to the corresponding a multi-material entities, a three-dimensional spatial combination may be directly performed on the a lattice structures. If the mechanical properties do not meet the requirements, the step regarding the lattice unit cell library is repeated to select an alternate lattice structure until a single-material mechanical functional member with similar mechanical properties to the multi-material mechanical functional member is formed.

[0040] Further, the three-dimensional space combination is performed on the a lattice structures, including direct superposition combination and indirect superposition combination.

[0041] When two structures have similar unit cell sizes and side surfaces of the two structures may be directly connected, the side surfaces are directly superimposed in a longitudinal direction or in a vertical direction. As shown in FIG. 2, taking a face-centered cubic lattice structure (FCC) and an octal-truss lattice structure as an illustration as an example, a side frame of the FCC structure is directly combined with a side frame of the octet truss. When the two structures have similar unit cell sizes, but side surfaces of the two structures may not be directly connected, the side surfaces are directly superimposed in the longitudinal direction or in the vertical direction. The combination of a simple cubic lattice structure (SC) and a regular octahedral lattice structure shows that the two structures cannot be directly combined in a horizontal direction or in the vertical direction. It can be seen that the side surface of the FCC lattice structure is a square frame, there is no solid structure inside the frame, and a side solid portion of the regular octahedral lattice structure is located in the center of the square frame. Since there is no solid structure around the square frame, a combined structure may not be formed. As shown in (a) and (b) of FIG. 3, by removing some regions of the regular octahedral lattice structure and changing the position of the side solid portion of the regular octahedral lattice structure, the modified position of the side solid portion of the regular octahedral lattice structure may be combined with the solid frame of the square side of the simple cubic (SC) lattice structure. The corresponding mechanical parameters of the modified combined lattice structure may fluctuate, so only approximate mechanical properties may be obtained by this method.

[0042] The side surfaces of the two structures are directly superimposed in the longitudinal direction or in the vertical direction. When the unit cell sizes of the two structures are considerably different, a stable combination may not be formed by direct superposition or by modifying the side surfaces of the lattice structures. The side surfaces may be connected through addition of a solid plate. Taking the connection of the simple cubic (SC) lattice structure with a larger unit cell size and a regular octahedral lattice structure with a smaller unit cell size as an example, as shown in FIG. 4, a solid plate is added at the connection for indirect connection, and a thickness of the solid plate is selected according to needs. Only approximate mechanical properties may be obtained through this method. The purpose of addition of the solid plate is to ensure a smooth transition of the mechanical properties of the connected portion of the two lattice structures and to reduce stress concentration.

[0043] In the above methods, the connection is performed directly or indirectly. The connection is rigid, and in some cases, there are obvious sharp corners, which is easy to cause stress concentration. The sharp corners of the connection may be removed or smooth transition processing may be performed as required, or a self-designed connection method may also be used.

[0044] Further, the manufacturing of a single-material mechanical functional member having a mixture of various lattice structures includes selection of a reasonable additive manufacturing method according to material types.

[0045] A single-material mechanical functional member based on a mixture of various lattice structures exhibits a complex shape. For a large member, such member may be manufactured by investment casting, molten gas injection, physical vapor deposition, sheet metal technology, and other processing methods. However, a multi-material mechanical functional member has a small size and complex shape. As such, it is difficult to obtain a good internal lattice unit cell through the above processing technologies, and there are obvious stress fluctuations when an external force is applied. Therefore, the additive manufacturing (AM) technology that can produce high precision and obtain a good surface is selected to replace the above traditional processing technology. Reasonable additive technology means are selected according to the material types. Selective laser melting (SLM) and laser sintering technology (SLM) are suitable for titanium alloys, stainless steels, aluminum alloys, and other metal materials. Fused deposition modeling (FDM) is suitable for engineering plastics such as PLA and nylon, and light curing molding (SLA) is suitable for photosensitive materials such as photosensitive resin.

[0046] As shown in FIG. 5, a multi-material mechanical functional member is provided, which is formed by a cube periphery and a cylinder core portion of two different materials. As shown in FIG. 6, a single material mechanical functional member formed by two lattice structures consisting of a cube periphery and a cylindrical core portion is provided. As shown in FIG. 7, it is a top view after the combination of the two lattice structures. The appearance of the single-material mechanical functional member after the combination of the two lattice structures is similar to that of the multi-material mechanical functional member, and the required mechanical properties may be achieved by adjusting the material type and the unit cell type, size, and array mode later.

[0047] A person having ordinary skill in the art should be able to easily understand that the above description is only preferred embodiments of the disclosure and is not intended to limit the disclosure. Any modifications, equivalent replacements, and modifications made without departing from the spirit and principles of the disclosure should fall within the protection scope of the disclosure.