Methods for fabricating strain wave gear flexsplines using metal additive manufacturing

Patent metadata

Field	Value
Publication number	US-11198181-B2
Application number	US-201815918831-A
Country	US
Kind code	B2
Filing date	Mar 12, 2018
Priority date	Mar 10, 2017
Publication date	Dec 14, 2021
Grant date	Dec 14, 2021

Abstract

Methods for the fabrication of metal strain wave gear flexsplines using a specialized metal additive manufacturing technique are provided. The method allows the entire flexspline to be metal printed, including all the components: the output surface with mating features, the thin wall of the cup, and the teeth integral to the flexspline. The flexspline may be used directly upon removal from the building tray.

First claim

The invention claimed is:

1. A method for fabricating a strain wave gear flexspline comprising:
using an additive manufacturing process for manufacturing metal to form an entirety of the strain wave gear flexspline as a single piece, wherein the strain wave gear flexspline is a cylindrical shape comprising:
depositing a bottom defining a circumference on a build platform,
wherein the bottom of the cylindrical shape is a circle with a thickness of at least one build layer,
further depositing a cylindrical wall disposed atop the bottom and defining a cylindrical volume, wherein the cylindrical wall is oriented perpendicularly to the build platform during fabrication, and
forming gear teeth disposed along the wall's edge, wherein
the cylindrical wall has a thickness of between 0.05 and 2 mm; and
the strain wave gear flexspline is fabricated in a vertical orientation by depositing layer by layer in a continuous seamless circle;

wherein the material physical properties of grain size, toughness, hardness, fracture toughness, fatigue limit, ductility, elastic modulus, and any combinations thereof of the strain wave gear flexspline within any single deposition layer are the same and are axially symmetric;
wherein the material physical properties of grain size, toughness, hardness, fracture toughness, fatigue limit, ductility, elastic modulus, and any combinations thereof of the strain wave gear flexspline in at least two adjacent deposition layers are different such that the mechanical properties of the strain wave gear flexspline vary between the bottom and the gear teeth; and
wherein the additive manufacturing process is powder bed fusion printing or direct energy deposition printing.

2. The method of claim 1 , wherein the strain wave gear flexspline is attached to the building platform for support during fabrication only at the bottom during fabrication.

3. The method of claim 1 , wherein the wall thickness of the strain wave gear flexspline is between 0.05 and 1 mm.

4. The method of claim 1 , wherein the additive manufacturing process comprises a laser and the flexspline has a cup shape with a base and gear teeth on the cylindrical wall on one side of the cup, wherein the thickness of the cup wall is within 15% of the spot size of the laser.

5. The method of claim 1 , wherein the additive manufacturing process comprises a laser and the cup wall is fabricated using a single width of the laser scanning or a single wire deposition extrusion process.

6. The method of claim 1 , wherein at least one of the composition, or microstructure of the strain wave gear flexspline are uniform in the direction parallel to the building platform but vary in the direction perpendicular to the building platform.

7. The method of claim 1 , wherein the strain wave gear flexspline is fabricated from a material with a fracture toughness between 30 and 150 MPa m 1/2 .

8. The method of claim 1 , wherein the material of the strain wave gear flexspline along the direction perpendicular to the building platform has a variable fracture toughness between 30 and 150 MPa m 1/2 .

9. The method of claim 1 , wherein the elastic limit of the strain wave gear flexspline ranges from 0.1-2%.

10. The method of claim 1 , wherein the strain wave gear flexspline comprises at least two regions with the same chemical composition but distinct physical properties of grain size, toughness, hardness, fracture toughness, fatigue limit, ductility, elastic modulus, and any combinations thereof disposed along the direction perpendicular to the building platform.

11. The method of claim 1 , wherein the strain wave gear flexspline comprises at least two regions of different chemical compositions disposed along the direction perpendicular to the building platform.

12. The method of claim 1 , wherein a gear teeth region of the strain wave gear flexspline comprising the gear teeth comprises a material that is chemically, physically, or both, different from the rest of the strain wave gear flexspline, and wherein the gear teeth region is more resistant to wear than the rest of the strain wave gear flexspline.

13. The method of claim 1 , wherein a gear teeth-less region of the strain wave gear flexspline that excludes gear teeth comprises a material that is chemically, physically, or both, different from the gear teeth region of the strain wave gear flexspline, and wherein the gear teeth-less region is more resistant to fracture than the rest of the strain wave gear flexspline.

14. The method of claim 1 , wherein a material used in the fabrication of the strain wave flexspline is introduced from a building head during direct energy deposition printing.

15. The method of claim 1 , wherein the additive manufacturing process utilizes a material in one of the forms chosen from the group consisting of:
powder, wire, molten metal, liquid metal, metal in a binder, metal in dissolvable inks, metal bound in polymer, sheet metal, or any combination thereof.

16. The method of claim 1 , wherein the gear teeth have a vertically oriented curvature.

17. The method of claim 1 , further comprising a post-fabrication process selected from the group consisting of:
chemical treatment to smooth the surface of the gear teeth and the inner surface of the cup wall;
mechanically grinding, sanding or polishing to reduce surface roughness;
coating with another metal;
heat treating to alter one or more material properties chosen from the group consisting of physical properties of grain size, toughness, hardness, fracture toughness, fatigue limit, ductility, elastic modulus, and any combinations thereof, porosity, temper, precipitate growth as compared to the as-fabricated state; and
any combination thereof.

18. The method of claim 1 , wherein the strain wave gear flexspline is fabricated from an alloy, a bulk metallic glass or metallic glass composite based on one or more elements chosen from the group consisting of: Fe, Ni, Zr, Ti, Cu, Al, Nb, Ta, W, Mo, V, Hf, Au, Pd, Pt, Ag, Zn, Ga, Mg, or any combination thereof.

19. The method of claim 1 , wherein the strain wave gear flexspline is fabricated from a metal matrix composite, and wherein the porosity or the chemical composition of the metal matrix composite, or both, is uniform in the direction parallel to the building platform but variable in the directing perpendicular to the building platform.

20. The method of claim 1 , wherein the strain wave gear flexspline is fabricated from both a crystalline metal alloy and a metallic glass alloy, and wherein the two materials are interchanged in the directing perpendicular to the building platform.

21. The method of claim 1 , wherein the strain wave gear flexspline is fabricated from a high melting temperature alloy with a melting temperature greater than 1,500 Celsius.

22. The method of claim 21 , wherein the high melting temperature alloy is Inconel or an alloy based on one of the elements chosen from the list: Nb, Ta, W, Mo, V, any combination thereof.

23. The method of claim 1 , wherein the gear teeth have a curved shape.

24. The method of claim 1 , wherein the flexspline has a cup shape with a base and gear teeth on the cylindrical wall on one side of the cup.

25. The method of claim 1 , wherein the additive manufacturing process comprises an electron beam.

Assignees

• California Inst Of Techn

Inventors

• Hofmann Douglas C
• Pate Andre M

Classifications

• B23F5/163 Primary

  the tool and workpiece being in crossed axis arrangement, e.g. skiving, i.e. "Waelzschaelen" · CPC title

• B22F10/28 Primary

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• B22F10/66

  by mechanical means · CPC title

• B22F10/64

  by thermal means (control of energy beam parameters for post heating B22F10/364) · CPC title

• B22F10/25

  Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS] · CPC title