Distortion prediction and minimisation in additive manufacturing

Patent metadata

Field	Value
Publication number	US-9950476-B2
Application number	US-201514731919-A
Country	US
Kind code	B2
Filing date	Jun 5, 2015
Priority date	Jun 5, 2014
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

A method of minimizing distortion in a workpiece is described that includes utilizing a computer system to carry out finite element analysis on a finite element thermo-mechanical model of the workpiece during and after fabrication by additive manufacturing to predict shape distortion and residual stress development in the workpiece, wherein the fabrication includes the fabrication step of depositing multiple layers of a material melted by a heat source along a deposit path on a substrate, and introducing alterations to the workpiece prior to or during fabrication to compensate for the predicted distortion.

First claim

The invention claimed is:

1. A method of minimising distortion in a workpiece, including the steps of:
in a computer system, carrying out finite element analysis on a finite element thermo-mechanical model of the workpiece during and after fabrication by additive manufacturing to predict shape distortion and residual stress development in the workpiece, wherein the fabrication includes the fabrication step of depositing multiple layers of a material melted by a heat source along a deposit path on a substrate;
minimising heat loss from the substrate and the deposited material during the fabrication by preventing an average temperature of the workpiece from falling by more than 10% between deposition of successive layers of the material; and
introducing alterations to the workpiece prior to or during fabrication to compensate for the predicted distortion.

2. A method according to claim 1 , wherein the fabrication further includes one or more of the following fabrication steps: preheating of the substrate, cooling of the workpiece and subsequent release of mechanical constraints on the workpiece.

3. A method according to claim 2 , wherein the heat source includes one or more of an electron beam, welding arc, plasma arc or laser beam.

4. A method according to claim 1 , wherein the alterations are made to one or more of the substrate geometry and the deposit path.

5. A method according to claim 1 , wherein the model includes a heat conduction element for modelling heat conduction in the substrate and the deposited material.

6. A method according to claim 1 , wherein the model includes a heat transfer element for modelling heat transfer from the workpiece to the exterior.

7. A method according to claim 6 , wherein the heat transfer element models heat transfer according to thermal radiation of the workpiece.

8. A method according to claim 7 , wherein the heat transfer element models heat transfer according to
q =εσ( T 4 −T amb 4 )

where q is the heat flux, T is the temperature and T amb is the ambient temperature, ε is the surface emissivity and σ is the Stefan-Boltzmann constant.

9. A method according to claim 7 , wherein the heat transfer element additionally models heat transfer according to thermal conduction of the workpiece.

10. A method according to claim 9 , wherein the heat transfer element models heat transfer according to
q=h ( T−T amb )
where q is the heat flux, h is the heat transfer coefficient, T is the temperature and T amb is the ambient temperature.

11. A method according to claim 1 , wherein the model includes an elastic deformation element using Hooke's law, Young's modulus, Poisson's ratio and the coefficient of thermal expansion of the material.

12. A method according to claim 1 , wherein the model includes a yielding behaviour element following the von Mises criterion.

13. A method according to claim 1 , wherein the model includes a yielding behaviour element following empirically deriving temperature dependant flow stress data.

14. A method according to claim 1 , wherein the model includes a material deposition element where deposition of the material is modelled at the liquidus temperature or slightly above the liquidus temperature with a small amount of superheat.

15. A method according to claim 1 , wherein the model includes a solidification element.

16. A method according to claim 1 , wherein the model includes a material deposition element where deposition of the material by application of an energy/heat source to melt the material is modelled.

17. A method according to claim 1 , and further including the step of:
using stress analysis information from the finite element analysis to identify local stress raisers that require relief during one or more of the fabrication stages using the heat source.

18. A method according to claim 1 , and further including the step of minimising heat loss from the substrate and the deposited material during one or more of the fabrication stages by applying insulation to the workpiece during and after fabrication.

19. A method according to claim 1 , and further including the step of minimising heat loss from the substrate and the deposited material during one or more of the fabrication stages by applying radiation reflection to the workpiece.

20. A method according to claim 1 , and further including the step of:
minimising the thermal gradient between the workpiece and the substrate by preheating the substrate before deposition of the material.

21. A method according to claim 1 , and further including the step of:
controlling mechanical boundary conditions during one or more of the fabrication stages by controlled reduction of clamping forces in line with varying critical stress as the part cools so as to minimise or avoid crack formation or other fabrication defects.

22. A method according to claim 1 , wherein the material is a metal or metal alloy.

23. A method according to claim 22 , wherein the metal alloy comprises any one or more of titanium, aluminium, nickel, vanadium, tantalum, copper, scandium, boron or magnesium.

24. A method according to claim 23 , wherein the metal alloy is titanium alloy Ti-6Al-4V.

25. An additive manufacturing apparatus for fabricating a workpiece, comprising:
a heat source, a wire feeder, a work table for supporting a substrate on which material is deposited, a movement mechanism for providing relative movement of the heat source, wire feeder and work table, and an evacuated chamber enclosing the heat source, wire feeder, work table and movement mechanism;
a control device for controlling operation of the heat source, wire feeder, work table and movement mechanism, wherein the control device is configured to minimize heat loss from the substrate and the deposited material during fabrication by preventing an average temperature of the workpiece from falling by more than 10% between deposition of successive layers of the material; and
a computer system including:
a main memory for storing computer readable code for a finite element analysis application module; and
at least one processor coupled to the main memory, said at least one processor executing the computer readable code in the main memory to cause the application module to carry out finite element analysis on a finite element thermo-mechanical model of the workpiece prior to and during fabrication to predict shape distortion and/or residual stress development in the workpiece.

Assignees

• Commw Scient Ind Res Org
• Boeing Co

Inventors

• Nguyen Vu Thua
• Lathabai Srinivasarao
• Feng Yuqing
• Miller Anthony
• Barnes John
• Coleman Gary
• Helvey Amy Marie

Classifications

• B29C64/393

  for controlling or regulating additive manufacturing processes · CPC title

• B33Y50/02

  for controlling or regulating additive manufacturing processes · CPC title

• B22F2999/00

  Aspects linked to processes or compositions used in powder metallurgy · CPC title

• B22F2203/03

  for feed-back · CPC title

• B22F10/85

  for controlling or regulating additive manufacturing processes · CPC title