Method of three-dimensional rapid prototyping through controlled layerwise deposition/extraction and apparatus therefor

• US 5,398,193 A
• Filed: 08/20/1993
• Issued: 03/14/1995
• Est. Priority Date: 08/20/1993
• Status: Expired due to Term

• Current Assignee: Optomec, Inc.
• Original Assignee: Alfredo O. Deangelis
• Inventors: deAngelis, Alfredo O.
• Primary Examiner(s): GORDON, PAUL P
• Application Number:
  US08/110,144
• Time in Patent Office: 571 Days
• Field of Search: 364/468, 364/474.24, 395/118, 395/119, 395/120, 264/10, 264/22, 264/23, 264/25, 264/40.1, 264/239, 264/241, 425/135, 425/140, 425/141
• US Class Current: 700/119
• CPC Class Codes: B29C 2791/001 Shaping in several steps
• CPC Class Codes: B29C 64/141 using only solid materials
• CPC Class Codes: B29C 64/188 involving additional operations performed on the added layers, e.g. smoothing, grinding or thickness control surface shaping B29C59/00; after-treatment of articles without altering their shape B29C71/00
• CPC Class Codes: B29C 64/336 of two or more materials
• CPC Class Codes: B29C 64/386 Data acquisition or data processing for additive manufacturing
• CPC Class Codes: B29C 64/40 Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof
• CPC Class Codes: B33Y 10/00 Processes of additive manufacturing
• CPC Class Codes: B33Y 30/00 Apparatus for additive manufacturing; Details thereof or accessories therefor
• CPC Class Codes: B33Y 40/00 Auxiliary operations or equipment, e.g. for material handling
• CPC Class Codes: B33Y 40/20 Post-treatment, e.g. curing, coating or polishing
• CPC Class Codes: B33Y 50/02 for controlling or regulating additive manufacturing processes

Abstract

A method of rapid prototyping through controlled layerwise deposition and extraction involving the precision control of material subtractive or removal processes in conjunction with material additive processes wherein each layer is formed by selectively depositing and removing portions of the layers in accordance with corresponding software slices of a computer model of the prototype part, and with complementary support material included in the layers and ultimately removed when the complete part has been fabricated.

Claims

1. A method of automated layerwise fabrication of a three-dimensional part from a computer model, through controlled deposition and extraction of materials, that comprises, producing a three-dimensional computer model representation of the part and, by software, slicing the representation into a plurality of successive layers corresponding to layers of predetermined thickness(es) of the part;

generating sequences of part and complementary support material(s) contours corresponding to each layer;

depositing material(s) for one or more of said contours onto a work surface within a processing enclosure;

material(s) processing said deposited contour(s) in order to achieve prespecified material properties for part and complementary contours;

removing portions of said material(s) from said part and complementary contour(s) under the control of the computer model representation corresponding thereto;

repeating the depositing, processing, and removing as necessary under the control of the computer model corresponding to the layer to complete an aggregate layer comprising part material contours within prespecified geometric and material property tolerances and complementary material(s) elsewhere on the aggregate layer;

completing the computer model layer by further processing said aggregate layer to ensure thickness tolerances and selective binding to the next aggregate layer;

repealing said controlled layer creation steps to build the entire part surrounded by the complementary material/s; and

removing said complementary material/s to obtain the fabricated part.

2. The method of claim 1 wherein the processing of said three-dimensional computer model into contours is done in a batch mode to obtain a full set of contours.

3. The method of claim 1 wherein the processing of said three-dimensional computer model for a given contour is performed as said given contour is needed by the process, with the slicing of the model occurring simultaneously with the part building.

4. The method of claim 1 wherein at least one of diagnostics and expert decision making are used to further process computer model data and define the computer model representation contours to facilitate the part-building process.

5. A method as claimed in claim 1 and in which the materials deposition is effected upon a pre-cut mask of complementary material, the cut of which corresponds to a corresponding software-slice contour, such that the mask is left in place as complementary support material toward the formation of the aggregate layer.

6. The method of claim 5 in which the precut masks are machined frames on a continuous film that advances over the work surface, or machined individual sheets that are sequentially positioned over the work surface.

7. The method of claim 5 in which a contour factorization approach is used such that there are no island contours for any given mask.

8. A method of claim 1 and in which the materials deposition is effected upon a pre-cut mask of material other than complementary material, and is removed prior to the formation of the aggregate layer.

9. The method of claim 1 in which a mask is formed by a conventional machining or a laser/energy beam machining system.

10. The method of claim 1 wherein at least one of the part and complementary sections which form the aggregate layer may consist of multiple materials.

11. The method of claim 1 wherein the deposition of material may be accomplished in discrete units corresponding to sections of a discretized work area.

12. The method of claim 1 wherein materials processing-and/or of the contours consists of heating the contours by one of conventional methods, laser/energy beam and/or chemically treating, mechanically processing the contours.

13. The method of claim 1 wherein inside the processing enclosure one of a prespecified temperature profile and/or pressure profile, gas concentration profile, chemical profile and/or vibration profile is maintained over the work surface.

14. The method of claim 1 wherein solid, liquid, and gaseous contaminants/debris is maintained within prespecified levels within the processing enclosure.

15. The method of claim 1 wherein the work surface is maintained at a constant level relative to ground plane by defining the work surface as the top of a cylinder which is indexed down or up a prespecified amount after each layer is completed.

16. The method of claim 1 wherein the work surface consists of the top layer of the part where the part is being built on a stationary platform.

17. The method of claim 1 wherein one of the work surface and/or the materials deposition system, materials extraction system, interlayer processing system is capable of X,Y and/or Z motion.

18. The method of claim 1 wherein material is deposited via a molten material dispensing unit.

19. The method of claim 18 wherein the molten material dispensing involves dispensing molten material and mechanically aiding the binding of the molten material to the work surface, while adjusting temperature to control solidification of the deposited material.

20. The method of claim 18 wherein the molten material dispensing involves feeding materials in solid form as powder or wire and melting the material for subsequent molten deposition, with or without a reservoir of molten material.

21. The method of claim 18 wherein selective cooling is accomplished by one of a thermoelectric cooler, a flowing liquid, gas cooler, by directly blowing gas on the molten material.

22. The method of claim 1 wherein materials are deposited by thermal spraying such as arc and plasma spraying with subsequent additional fusion bonding effected by one of regional energy/heat profiles and by regional chemical processes.

23. The method of claim 1 wherein the materials are deposited by one of chemical and electrochemical processes, thermosetting material is dispensed in a pre-cured state onto the work surface, and cured by regional heat, material dispensed in a sol-gel/liquid solution state onto the work surface, and reduced/evaporated by regional heat.

24. The method of claim 1 wherein the material being deposited is selected from the group consisting of metals, plastics, waxes, ceramics, alloys, composites, graphite'"'"'s, glasses and inorganics.

25. The method of claim 1 in which the removal of materials is accomplished through one of conventional machining, and/or selected energy delivery and chemical/electrochemical machining.

26. The method of claim 1 wherein the processing enclosure, the removal of any debris or contaminants is accomplished through one of gas transport, liquid transport and/or magnetism and/or gravity and/or chemical dissolution and/or vaporization, combinations thereof.

27. The method of claim 1 wherein processing of the aggregate layer in order to achieve one of a prespecified layer thickness, enhanced material properties and binding is accomplished by one of conventional machining, selective energy delivery, and chemical/electrochemical machining.

28. The method of claim 1 wherein the complementary material is of lower melting temperature than the part material and can be removed by heating to a temperature greater than the melting point of the complementary material but less than the melting point of the part material.

29. The method of claim 1 wherein the complementary material is soluble in a solvent and can be removed through contact with the solvent.

30. The method of claim 29 wherein the complementary material is soluble in water such as a variety of inorganic salts, waxes and water soluble aluminum alloys.

31. The method of claim 29 wherein the complementary material is a glass such as borosilicate and is soluble in a solvent such as acetone, or a ceramic and is soluble in a variety of solvents.

32. The method of claim 1 wherein the complementary material is material that oxidizes rapidly under conditions that are non detrimental to the part material.

33. The method of claim 32 wherein the complementary material is a graphite based material that oxidizes rapidly under appropriate temperature and oxygen concentration levels.

34. The method of claim 1 wherein the complementary material is removable by one of thermal, mechanical cycling and/or shocking, by heating and/or a solution bath and induced rapid oxidation.

35. The method of claim 1 wherein the further processing is effected by at least one of machining off a sublayer to ensure thickness tolerances, roughening, polishing, surface heat treatment, surface alloying, and chemically enhancing the surface to ensure selective binding.

36. Apparatus for automated layerwise fabrication of a three-dimensional part from a computer model, through controlled deposition and extraction of materials having, in combination, means for producing a three-dimensional computer model representation of the part and, by software, slicing representation into a plurality of successive layers corresponding to layers of predetermined thickness(es) of the part;

means for generating sequences of part and complementary support material(s) contours corresponding to each layer;

means for depositing material(s) for one or more of said contours onto a work surface within a processing enclosure;

means for materials(s) processing said deposited contour(s) in order to achieve prespecified material properties for part and complementary contours;

means for removing portions of said material(s) from said part and complimentary contour(s) under the control of the computer model representation corresponding thereto;

means for repeating the depositing, processing, and removing as necessary under the control of the computer model corresponding to the layer to complete an aggregate layer comprising part material contours with prespecified geometric and material property tolerances and complementary material(s) elsewhere on the aggregate layer;

means for completing the computer model layering by further processing said aggregate layer to ensure thickness tolerances and selective binding to the next aggregate layer to build the entire part surrounded by the complementary material(s); and

means for removing said complementary material(s) to obtain the fabricated part.