Ultrasonic object consolidation

• US 6,519,500 B1
• Filed: 03/23/2000
• Issued: 02/11/2003
• Est. Priority Date: 09/16/1999
• Status: Expired due to Term

• Current Assignee: Solidica, Inc.
• Original Assignee: Solidica, Inc.
• Inventors: White, Dawn
• Primary Examiner(s): Picard, Leo P.
• Assistant Examiner(s): CABRERA, ZOILA E
• Application Number:
  US09/532,432
• Time in Patent Office: 1,055 Days
• Field of Search: 700/117-123, 700/182, 156/73-- 7
• US Class Current: 700/119
• 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 70/00 Materials specially adapted for additive manufacturing
• CPC Class Codes: B33Y 80/00 Products made by additive manufacturing
• CPC Class Codes: C22C 13/00 Alloys based on tin
• CPC Class Codes: G05B 19/00 Programme-control systems
• CPC Class Codes: G05B 19/4099 Surface or curve machining, making 3D objects, e.g. desktop manufacturing
• CPC Class Codes: G05B 2219/45206 Ultrasonic drill, mill, machining
• CPC Class Codes: G05B 2219/45238 Tape, fiber, glue, material dispensing in layers, beads, filling, sealing
• CPC Class Codes: G05B 2219/49011 Machine 2-D slices, build 3-D model, laminated object manufacturing LOM
• CPC Class Codes: G05B 2219/49015 Wire, strang laying, deposit fluid, welding, adhesive, hardening, solidification, fuse
• CPC Class Codes: G05B 2219/49016 Desktop manufacturing [DTM]; Solid freeform machining [SFM]; Solid freeform fabrication [SFF]
• CPC Class Codes: G05B 2219/49017 DTM desktop manufacturing, prototyping
• CPC Class Codes: G05B 2219/49026 SDM shape deposition manufacturing for multimaterial layers
• CPC Class Codes: G05B 2219/49032 Bond layers with glue, solder, welding, brazing in LOM
• CPC Class Codes: G05B 2219/49039 Build layer of different, weaker material between support and prototype
• CPC Class Codes: G05B 2219/49241 2-5-D lace cutting, work in xy and increment in z, repeat
• CPC Class Codes: Y02P 90/02 Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]

Abstract

A system and a method of fabricating a three-dimensional object on a substrate includes adding material layers incrementally and consolidating the layers by using ultrasonic vibrations and pressure. The layers are placed in position to shape the object by a material feeding unit, and they come in various forms, including flat sheets, segments of tape, strands of filament or single dots of material. The material may be plastic or metallic, and composition may vary discontinuously or gradually from one layer to the next, creating a region of functionally gradient material. The invention permits the construction and repair of dense objects, including fiber-reinforced composites and aerospace structures. Excess material may be removed one or more layers are bonded, including following end of the process after the final object is fabricated. The layers are fed sequentially and additively according to a layer-by-layer computer-model description of the object, which is generated by a computer-aided design/manufacturing (CAD/CAM) system. Ultrasonic welding equipment applicable to the invention preferably includes an ultrasonic generator, a transducer, a booster and a head unit or sonotrode.

Claims

1. A method of fabricating an object through ultrasonic consolidation, comprising the steps of:

providing a description of the object to be fabricated;

providing a plurality of material layers having contact surfaces therebetween;

forming the object in accordance with the description by trasmitting ultrasonic vibrations to one or more of the contact surfaces, thereby consolidating the layers of material directly to one another without melting the material in bulk; and

removing any excess material.

2. The method of claim 1, wherein the material layers are composed of sheets, elongated tapes, filaments, dots or droplets.

3. The method of claim 1, wherein successive layers of the material define a discontinuous or gradual change in material composition.

4. The method of claim 1, wherein the step of ultrasonically consolidating the material layers uses energy having a direction which is substantially perpendicular or parallel to the layers.

5. The method of claim 1, wherein the description of the object is provided in the form of a computer-aided design or manufacturing (CAD/CAM) file.

6. The method of claim 1, wherein a layer is cut into a shape corresponding to the description of the object prior to the step of ultrasonically bonding that layer.

7. The method of claim 1, wherein a plurality of layers are ultrasonically bonded then trimmed in accordance with the description of the object.

8. The method of claim 1, wherein the layers are ultrasonically bonded one layer at a time.

9. The method of claim 1, wherein alternating layers of reinforcement fibers and metallic powder are used to fabricate a metal-matrix composite object.

10. The method of claim 9, further including the step of consolidating the metallic powder through laser-aided heating.

11. The method of claim 9, further including at least one layer of metallic foil.

12. The method of claim 9, wherein the fibers are continuous ceramic fibers.

13. The method of claim 9, wherein the object is a fiber-reinforced composite tape.

14. The method of claim 9, wherein the reinforcement fibers assume a direction determined by the description of the object.

15. The method of claim 9, wherein the reinforcement fibers cross each other in successive layers for added strength.

16. The method of claim 1, wherein:

the material is provided in the form of a tape having a width.

17. The method of claim 16, wherein the description of the object takes the width of the tape into account.

18. The method of claim 1, wherein:

the object includes an overhanging, cantilevered or enclosed feature; and

support material is used to support the feature.

19. The method of claim 18, wherein the support material is sufficiently rigid to permit the ultrasonic consolidation of subsequent layers.

20. The method of claim 18, wherein ultrasonic vibrations are not damped by the support material.

21. The method of claim 18, wherein the support material is a low-melting-point alloy including solders, copper-based brazes, nickel-based brazes or titanium-based brazes.

22. The method of claim 18, wherein the support material is a different high melting point material which ultrasonically consolidates under very different conditions from the alloy which is being used to produce the object.

23. The method of claim 18, wherein the support material is supplied in the form of tapes or sheets which are ultrasonically consolidated to form a support structure.

24. The method of claim 18, wherein the support material is roughened through mechanical or chemical processing to ensure that adjacent, unconsolidated layers do not slip against each in the presence of ultrasonic vibrations.

25. The method of claim 18, wherein the support material is cut and applied to ensure that it can be shaken or otherwise easily removed from the object being fabricated.

26. The method of claim 18, wherein the support material is applied as a liquid, but hardens to produce a rigid support structure.

27. The method of claim 26, wherein slip-cast ceramics, freeze-cast ceramics, solgels, or hard, sufficiently high-melting point waxes are used as the support material.

28. The method of claim 1, further including the step of providing a computer-controlled actuation system operative to automatically place the material layers in position prior to consolidation.

29. The method of claim 1, wherein the object is a repair of an existing article.

30. A method of fabricating an object through ultrasonic consolidation, comprising the steps of:

a) providing a description of the object to be fabricated;

b) providing a plurality of material layers having contact surfaces therebetween;

c) bonding the material layers directly to one another by transmiting ultrasonic vibrations to one or more of the contact surfaces to form a section of the object without melting the material in bulk;

d) repeating steps b) and c) to form a plurality of sections of the object;

e) ultrasonically bonding at least two sections of the object at a time until the object is formed; and

f) removing any excess material from the object.

31. The method of claim 30, wherein the material layers are dots of material, and the dots are cut from a filament.

32. The method of claim 30, wherein the description of the object is provided in the form of a computer-aided design (CAD) file, and wherein the method includes the additional step of:

providing a computer-controlled actuation system to place the material layers in position to form the object.

33. The method of claim 30, wherein at least two successive layers of the material define a discontinuous or gradual change in material composition.

34. A system for fabricating an object through ultrasonic consolidation, comprising:

a memory for storing a description of the object;

a material feeder for providing successive layers of material with contact surfaces therebetween;

a source of ultrasonic vibrations operative to join one or more layers of the material directly to one another at their contact surfaces without melting the material in bulk; and

a controller operative to coordinate the addition of successive layers through the material feeder and control the source of ultrasonic vibrations to consolidate the layers in accordance with the description of the object.

35. The system of claim 34, further including an actuation system for imparting relative motion between the material feeder and source of ultrasonic vibrations sufficient to fabricate three-dimensional objects.

36. The system of claim 34, further including a material-removing unit for removing excess material not required to form the object.

37. The system of claim 36, wherein the material-removing unit includes a knife, drill, laser beam, milling machine or ultrasonic machining tool.

38. The system of claim 34, wherein the material is plastic.

39. The system of claim 38, wherein the ultrasonic vibrations have direction perpendicular to the plane of the contact surfaces.

40. The system of claim 34, wherein the material is metal.

41. The system of claim 40, wherein the ultrasonic vibrations have direction parallel to the plane of the contact surfaces.

42. The system of claim 34, wherein the material is provided in the form of sheets, tapes, filaments, dots or droplets.

43. The system of claim 34, further including:

a support-material feeder; and

a support-material removing unit for removing excess support material not required to form the object.

44. The system of claim 34, wherein the object is a repair to an existing article.