SYSTEM AND METHOD FOR DESIGNING AND MANUFACTURING OBJECTS HAVING AN OPTIMISED FREE-FORM WITH NOVEL COMPOSITE MATERIALS AND THE RESULTING OBJECT
20220314484 · 2022-10-06
Inventors
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B29C70/46
PERFORMING OPERATIONS; TRANSPORTING
B33Y50/00
PERFORMING OPERATIONS; TRANSPORTING
B22F8/00
PERFORMING OPERATIONS; TRANSPORTING
B27D1/083
PERFORMING OPERATIONS; TRANSPORTING
B29C43/02
PERFORMING OPERATIONS; TRANSPORTING
B22F10/85
PERFORMING OPERATIONS; TRANSPORTING
B29C64/393
PERFORMING OPERATIONS; TRANSPORTING
B27G11/00
PERFORMING OPERATIONS; TRANSPORTING
B29C43/003
PERFORMING OPERATIONS; TRANSPORTING
Y02P80/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
G05B19/4099
PHYSICS
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/00
PERFORMING OPERATIONS; TRANSPORTING
B29C70/30
PERFORMING OPERATIONS; TRANSPORTING
B29C33/3842
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A system and method for designing and manufacturing free-form objects made of composite material and optimised in their weight ratio and load capacity; a system for the design and manufacture of said objects, and the objects resulting from said method. Using three-dimensional (3D) design computer programs and computer calculation programs, the design of a composite material object is obtained, with a specific shape and orientation of its component fragments, optimised to be light and at the same time to meet a required specific mechanical and/or structural performance. Subsequently, a mould of at least two parts is obtained from this design and the parameters of said design are transformed into instructions so that one or more automated manufacturing machines deposit fragments of wood or another material onto the lower part of the mould in specific orientations, calculated to minimise the weight of the object and optimise its load capacity. Then, with the addition of one or more binders, the object is pressed between the parts of said mould. Finally, the new manufactured object is obtained by removing it from the mould.
Claims
1.-15. (canceled)
16. A method for manufacturing optimised free-form objects made of composite materials, that have been previously designed using computer programs for designing, simulating, analysing results, redesigning, simulating and analysing results N times in a data feedback loop, obtaining an optimised 3D design, and converting the digital information of the design into manufacturing instructions for machinery that operates with computerised numerical control (CNC), wherein the composite material comprises fragments of material and binder; wherein that it comprises the steps of: (a) providing a mould of at least two parts specific to the optimised design obtained through the design process for the design of the object; (b) depositing on the lower part of the mould the binder(s) and the fragments of material in intentional and specific coordinates and orientations according to the digital instructions calculated to optimise the resistance to any stresses to be borne by the resulting object; (c) pressing the fragments together with the binder between the parts of the mould; (d) separating the parts of the mould to remove the finished object.
17. The method of claim 16, wherein that after step (b) of depositing binder and fragments of material and before pressing the fragments together with the binder, the method also comprises: depositing, on the layer formed in step (b), one or more layers of binder and fragments of material in intentional and specific coordinates and orientations according to the digital instructions, depending on the formal and mechanical requirements of the object, to form multiple layers of composite material.
18. The method of claim 17, wherein that the binder and the fragments of material of each of the multiple layers have their own specific coordinates and orientations that are equal to or different from those of the other layers.
19. The method of claim 16, wherein that the thickness of the layers of material of the object obtained can be greater in some areas of the object than in others depending on the formal and mechanical requirements of the object.
20. The method of claim 16, wherein that the mould comprises membrane parts, and the membrane parts are brought together to apply force and press the deposited materials therebetween.
21. The method of claim 16, wherein that the fragments of material comprise at least one material from the group consisting of wood, materials of plant origin, materials of animal origin, materials of synthetic origin, materials of mineral origin, metal materials.
22. The method of claim 16, wherein that the fragments of material are of irregular shapes and sizes.
23. The method of claim 16, wherein that the fragments of material are of irregular shapes and sizes.
24. The method of claim 16, wherein that the fragments of material comprise a combination of at least two regular shapes and/or sizes.
25. The method of claim 16, wherein that the fragments of material are a combination of regular and/or irregular shapes and/or sizes.
26. The method of claim 16, wherein that the binder comprises at least one binder of the group consisting of an adhesive a thermoplastic material and vapour.
27. The method of claim 16, wherein that the pressing is performed without heat being applied.
28. The method of claim 16, wherein that the pressing is performed with heat being applied.
29. A system for manufacturing an optimised free-form three-dimensional object made of composite material, that has been previously designed using computer programs for designing, simulating, analysing results, redesigning, simulating and analysing results N times in a data feedback loop, obtaining an optimised 3D design, and converting the digital information of the design into manufacturing instructions for machinery that operates with computerised numerical control (CNC), wherein the composite material comprises fragments of material and binder; wherein that it comprises (a) a computer for storing one or more computer programs for design, calculation and analysis, and configured to send digital instructions to a deposition machine; (b) a mould of at least two parts, specific to the optimised design obtained through the design process for the object; (c) one or more machines for depositing material configured to deposit, on the lower part of the mould, the binder and fragments of material in specific coordinates and orientations calculated to optimise the resistance to any stresses to be borne by the resulting object, according to the digital instructions; (d) a press configured to press the fragments together with the binder between the parts of the mould.
30. The system of claim 29, wherein that the mould comprises membrane parts, and the membrane parts are configured to apply force and press the deposited materials therebetween.
31. The system of claim 29, wherein that the fragments of material comprise at least one material from the group consisting of wood, materials of plant origin, materials of animal origin, materials of synthetic origin, materials of mineral origin, metal materials.
32. The system of claim 29, wherein that the binder comprises at least one binder of the group consisting of an adhesive, a thermoplastic material and vapour.
33. An optimised free-form three-dimensional object made of composite material, that has been previously designed using computer programs for designing, simulating, analysing results, redesigning, simulating and analysing results N times in a data feedback loop, obtaining an optimised 3D design, and converting the digital information of the design into manufacturing instructions for machinery that operates with computerised numerical control (CNC), wherein the composite material comprises fragments of material and binder; wherein that (a) the fragments of material are in intentional and specific coordinates and orientations according to the digital instructions calculated to optimise the resistance to any stresses to be borne by the resulting object; (b) a binding material is combined with the fragments of material; (c) the fragments of material and the binder make up a pressed layer of composite material with high mechanical and/or structural performance in specific orientations.
34. The three-dimensional object of claim 33, wherein that it comprises multiple pressed layers of composite material of fragments of material and binder wherein the fragments of material of the multiple layers are laid in intentional and specific coordinates and orientations according to the digital instructions.
35. The three-dimensional object of claim 33, wherein that the fragments of material contained in the composite material comprise at least one material from the group consisting of wood, materials of plant origin, materials of animal origin, materials of synthetic origin, materials of mineral origin, metal materials.
36. The three-dimensional object of claim 33, wherein that the binder comprises at least one binder of the group consisting of an adhesive a thermoplastic material and vapour.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0016]
[0017]
[0018]
[0019]
[0020]
[0021]
[0022] It should be noted that the figures are not drawn to scale, and that for illustrative purposes the elements, their parts and the steps are represented by similar reference numerals in all figures. It should also be noted that the figures are only intended to facilitate the description of some of the preferred embodiments, and do not illustrate the other possible embodiments, or every aspect of the embodiments described, so the figures do not limit the scope of this disclosure.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
[0023] Because the materials and manufacturing systems and methods that are currently available are deficient in the manufacture of objects that combine characteristics of high mechanical and/or structural performance with being light, and/or are deficient in characteristics of lower environmental impact and sustainability, it may be desirable to develop a new system and method for designing and manufacturing optimised free-form objects with novel composite materials and the resulting object, which manages to manufacture objects that combine properties of high mechanical and/or structural performance with being light, also having characteristics of lower environmental impact and sustainability, and that can be used in a wide variety of industries that increasingly require objects with these characteristics, such as construction, transportation, furniture, appliances and others.
[0024] For example, in one of the applications mentioned herein, mention is made of the transportation industry and its need to lighten the weight of vehicle components in order to save fuel and/or energy, and consequently emit less CO2.
[0025]
[0026]
[0027]
[0028] In another embodiment, both parts of the mould can move towards one another until the deposited material is pressed. In other embodiments, it can consist of vacuum moulds. In further embodiments, the mould can have more than 2 parts.
[0029]
[0030]
[0031]
[0032] In block (61) the formal and structural requirements of the object to be manufactured are obtained. In this step, information is received on the required characteristics for the object, both regarding its shape, maximum and minimum dimensions, mechanical performance requirements, maximum weight and other quantifiable variables that the object must have once finished. For example, following the embodiment illustrated in
[0033] In block (62) the parameters that the object must meet are defined, based on the information on the requirements for the object obtained in the previous step. Continuing with the example of the previous paragraph, in this step the requirements are transformed into specific shape parameters, and into numerical parameters with specific maximums and minimums for the object, such as width, height, thickness, weight, vertical load to be supported, traction and other loads to be supported.
[0034] In block (63) the parameters defined in the previous step (62) are entered into one or more computer programs and transformed into an initial digital design that then goes through digital simulations, analysis of results and redesign N times in a feedback loop until obtaining the optimised digital three-dimensional design that meets all the formal and structural requirements in the most efficient way found. This process defines: the general shape of the design for the object; the type and sizes of fragments to be used; the material of the fragments (preferably wood); the size of the fragments; the binder(s) to be used; and, very importantly, the orientation of the fragments according to their shape and the orientation of their fibres, strands or component parts.
[0035] In block (64), the optimised digital three-dimensional design is transformed by a computer program into operating instructions for machinery that operates with computerised numerical control (CNC).
[0036] In block (65) a mould is obtained, specific to the optimised design obtained through the previous processes.
[0037] In block (66) the digital instructions are sent to the CNC machinery so that it deposits the selected materials in the mould. These instructions are data of 3D coordinates and the orientation of each fragment that will be deposited at said coordinates, the detail of whether or not binder will be used, and if binder is used then also the data of 3D coordinates and the respective amounts of binder that will be deposited at the respective coordinates with respect to the mould.
[0038] In block (67) the instructions sent to the CNC machinery are executed. It is in this step that the fragments and binders are deposited on the mould.
[0039] In block (68) the step of pressing the deposited materials begins. In this step the materials deposited in the mould are pressed with force.
[0040] In block (69) the parts of the mould are separated to obtain the finished object.