Object consolidation employing friction joining

• US 6,457,629 B1
• Filed: 10/04/2000
• Issued: 10/01/2002
• Est. Priority Date: 10/04/1999
• Status: Active Grant

• Current Assignee: Solidica, Inc.
• Original Assignee: Solidica, Inc.
• Inventors: White, Dawn
• Primary Examiner(s): Dunn, Tom
• Assistant Examiner(s): DUNN, COLLEEN P
• Application Number:
  US09/679,163
• Time in Patent Office: 727 Days
• Field of Search: 228/112.1, 228/114.5, 228/159, 228/160, 228/163, 228/170, 228/185, 228/2.1, 228/2.3, 228/49.2, 219/76.1, 219/76.12, 219/137.R, 219/137.2
• US Class Current: 228/112.1
• CPC Class Codes: B23K 20/10 making use of vibrations, e.g. ultrasonic welding
• CPC Class Codes: B23K 20/103 using a roller
• CPC Class Codes: B23K 20/1215 for other purposes than joining, e.g. built-up welding
• CPC Class Codes: B29C 64/106 using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
• CPC Class Codes: B29C 64/118 using filamentary material being melted, e.g. fused deposition modelling [FDM]
• 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 64/40 Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof
• CPC Class Codes: B29C 73/02 using liquid or paste-like material B29C73/16 takes precedence
• 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: G05B 19/4099 Surface or curve machining, making 3D objects, e.g. desktop manufacturing
• CPC Class Codes: G05B 2219/49007 Making, forming 3-D object, model, surface
• CPC Class Codes: G05B 2219/49015 Wire, strang laying, deposit fluid, welding, adhesive, hardening, solidification, fuse

Abstract

Friction heating and bonding are used to consolidate sequentially applied metals, plastics or composites to previously deposited material so as to form a bulk deposit in a desired shape. Monolithic or composite sheets, tapes and filaments can be consolidated using the approach. A system according to the invention includes a source of friction; a mechanism for applying a forging load between a feedstock power supply and a work surface; a work-head, which may have various configurations depending on the geometry of the feedstock to be used; a material feeding system; and a computer-controlled actuation system which controls the placement of material increments added to an object being built. A computer model of the object to be built is used to generate commands to produce the object additively and automatically. The approach provides a solid, freeform fabrication technique that requires no tooling, operates in the solid state, and creates a bond directly at the faying surfaces (i.e., acts only at the location where bonding/consolidation of the material increments is desired).

Claims

1. A method of fabricating an object through sequential material deposition, comprising the steps of:

providing a description of the object to be fabricated;

providing a material feedstock;

sequetially depositing increments of the material and consolidating the increments in accordance with the description of the object using frictional energy to create a localized plastic flow, mushy zone, or melted region at the interface between the previously deposited material and each new increment until the object is formed without melting the material in bulk; and

removing any excess material.

2. The method of claim 1, further including the step of applying pressure to the material increments during consolidation.

3. The method of claim 1, further including the step of applying heat to the increment prior to consolidation.

4. The method of claim 1, further including the step of inducing high-frequency acoustic vibrations the increment during the consolidation thereof.

5. The method of claim 1, wherein the material is provided in the form of sheets, elongated tapes, filaments, dots or droplets.

6. The method of claim 1, wherein material increments define a discontinuous or gradual change in material composition.

7. 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.

8. The method of claim 1, wherein the process passes the energy through the material increment during the deposition thereof.

9. The method of claim 1, wherein the material is provided in the form of thin layers, and one or more of the layers are cut into a shape corresponding to the description of the object prior to the step of consolidating the layer.

10. The method of claim 1, wherein the material is provided in the form of thin layers, and one or more of the layers are consolidated then trimmed in accordance with the description of the object.

11. The method of claim 1, wherein the material is provided in the form of a plurality of thin layers which a re consolidated one layer at a time.

12. The method of claim 1, wherein alternating layers of reinforcement fibers and metallic powders, foils, or a combination thereof, are used to fabricate a metal-matrix composite object.

13. The method of claim 1, wherein:

the material is provided in the form of a tape having a width; and

the description of the object takes the width of the tape into account.

14. The method of claim 1, wherein:

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

support material is used to support the feature.

15. The method of claim 14, wherein the support material has a melting point which is different than the material used to form the object.

16. The method of claim 15, wherein the support material is:

an alloy including solders, copper-based brazes, nickel-based brazes or titanium-based brazes, or

a granular ceramic or other electrically insulating material, including silica, zirconia, alumina, salts, clays, plasters.

17. 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.

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

19. A system for fabricating an object using sequential material deposition, comprising:

a memory for storing a description of the object;

a material feeder for providing material increments with faying surfaces therebetween;

a source of frictional energy operative to join the material increments without melting the material in bulk; and

a controller operative to coordinate the successive deposition of material increments through the material feeder and control the source of energy to consolidate the material in accordance with the description of the object.

20. The system of claim 19, further including an actuation system for imparting relative motion between the material feeder and energy source.

21. The system of claim 19, further including a material-removing unit for removing excess material not required to form the object.

22. The system of claim 19, wherein the material-removing unit includes a knife, drill, laser beam, milling machine or ultrasonic machining tool.

23. The system of claim 19, wherein the feeder is operative to provide the material in the form of sheets, tapes, filaments, dots or droplets.

24. The system of claim 19, further including:

a support-material feeder; and

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

25. The system of claim 19, wherein the object is a repair to an existing article.