Additive manufacturing system and method of additive manufacture utilizing layer-by-layer thermo-mechanical analysis

Patent metadata

Field	Value
Publication number	US-9925724-B2
Application number	US-201514790941-A
Country	US
Kind code	B2
Filing date	Jul 2, 2015
Priority date	Jul 3, 2014
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

A method of operating an additive manufacturing system utilizing a layer-by-layer thermo-mechanical analysis system includes the steps of pre-modeling a structure or workpiece into a plurality of slices stacked from a bottom slice to a top slice of the plurality of slices, assuming a second slice modeled immediately below a first slice is a rigid substrate, and run a response force analysis for the first slice. The analysis system may reiterate this process for each slice calculating a force distribution map for each slice, and adding the force distribution maps to a total response force map of the entire structure. The additive manufacturing system may then use the total response force map to optimize material properties for selected regions of each slice to a sacrificial support structure and/or the final product.

First claim

What is claimed is:

1. A method of additive manufacturing a structure, comprising:
pre-modeling the structure into a plurality of stacked slices;
performing a response force analysis between a top slice and an adjacent lower second slice, wherein the analysis models the second slice as a rigid substrate; and
performing a response force analysis between the second slice and an adjacent lower third slice, wherein the analysis no longer models the second slice as a rigid substrate and models the third slice as a rigid substrate.

2. The method according to claim 1 comprising the further steps of:
determining if the second slice has an unsupported area; and
calculating a second response force distribution map of the unsupported area of the second slice.

3. The method according to claim 2 comprising the further step of:
calculating a total response force map from the first and second response force distribution maps.

4. The method according to claim 3 comprising the further step of:
design material properties of the structure based at least in-part by the total response force map.

5. The method according to claim 4 , wherein material properties include density distribution of mass.

6. The method according to claim 4 , wherein material properties include material composition.

7. The method according to claim 4 , wherein the design of material properties is limited by the functional requirements of the structure during design intended operation.

8. The method according to claim 4 , wherein the design of material properties prevents over-constraint of the unsupported areas.

9. The method according to claim 4 , wherein the design of material properties prevents warpage of slices as a result of additive manufacturing.

10. The method according to claim 4 , wherein the design of material properties prevents delamination between slices.

11. The method according to claim 3 , comprising the further step of:
incorporating a sacrificial support structure as part of the structure to support the unsupported areas.

12. The method according to claim 3 , wherein the additive manufacturing is direct metal laser sintering.

13. The method according to claim 3 , wherein the additive manufacturing is electron beam melting.

14. A method of additive manufacturing a structure, comprising:
pre-modeling the structure into a plurality of stacked slices;
performing a response force analysis between a top slice and an adjacent lower second slice, wherein the analysis models the second slice as a rigid substrate;
determining if the top slice has an unsupported area; and
calculating a first response force distribution map of the unsupported area of the top slice.

15. An additive manufacturing system comprising:
a build table for supporting a structure;
an energy gun for successively melting a plurality of slices of the structure over one-another, with the build table and the energy gun constructed and arranged to move away from one-another as each slice of the plurality of slices is manufactured; and
an electric controller constructed and arranged to model the structure into the plurality of slices and having a layer-by-layer thermo-mechanical analysis system for determining optimized material properties of at least a portion of the structure;
wherein the layer-by-layer thermo-mechanical analysis system models a second slice immediately below a first slice of the plurality of slices as a rigid substrate, runs a response force analysis for the first slice, determines if the first slice has an unsupported area and if so calculates a first response force distribution map of the unsupported a of the first slice, then models a third slice of the plurality of slices immediately below the second slice as a rigid substrate, runs a response force analysis for the second slice, determines if the second slice has an unsupported area and if so calculates a second response force distribution map of the unsupported area of the second slice, and calculates a total response force map from the first and second response force distribution maps.

16. The additive manufacturing system set forth in claim 15 , wherein the controller is constructed and arranged to control the energy gun based at least in-part on the optimized material properties for each slice.

17. The additive manufacturing system set forth in claim 15 further comprising:
a spreader for placing a layer of powder over the last manufactured slice, wherein the controller is constructed and arranged to control the spreader for altering powder material composition based at least in-part on the optimized material properties for each slice.

18. The additive manufacturing system set forth in claim 15 wherein the energy gun is a laser gun.

19. The additive manufacturing system set forth in claim 15 wherein the energy gun is an electron beam gun.

20. The additive manufacturing system set forth in claim 15 , wherein the layer-by-layer thermo-mechanical analysis system determines the location and optimized material properties of at least one sacrificial support structure of the structure.

Assignees

• United Technologies Corp

Inventors

• Long Yu

Classifications

• G05B2219/35134

  3-D cad-cam · CPC title

• Y02P80/40

  Minimising material used in manufacturing processes · CPC title

• B29C64/40 Primary

  Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof · CPC title

• G05B19/4099

  Surface or curve machining, making three-dimensional [3D] objects, e.g. desktop manufacturing · CPC title

• B23K15/0086

  welding for purposes other than joining, e.g. build-up welding · CPC title