IP Library › Granted Patent US 10,259,163
Granted Patent B2
US 10,259,163 · App. 14/947,600 · Granted Apr 16, 2019

Method and system for adapting a 3D printing model

Inventors: Wolfgang Eilken (Hamburg, DE); Memis Tiryaki (Hamburg, DE); Henning Felgenhauer (Hamburg, DE)
Assignee: AIRBUS OPERATIONS GMBH
B29C64/386G06T19/20B33Y10/00B33Y50/00G06T2219/2021
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Quick Facts
Patent No.
US 10,259,163
App. No.
14/947,600
Granted
Apr 16, 2019
Kind
B2
Abstract

A method for adapting a 3D printing model includes calculating a layer representation model on the basis of a 3D object model of an object; determining a plurality of overhang regions in the layer representation model where the boundary edges of first layers extend over the boundary edges of second layers, the first layers being directly adjacent and subsequent to the second layers when going into the build-up direction of the layer representation model; determining a local overhang angle in each of the plurality of overhang regions; adapting the layer representation model by re-defining the boundary edges of layers in the overhang regions so that the local overhang angle remains below a predetermined overhang threshold angle; and outputting the adapted layer representation model as 3D printing model to the 3D printing apparatus.

Claims (26)

1. A method for adapting and using a 3D printing model, the method comprising:

calculating a layer representation model on the basis of a 3D object model of an object, the layer representation model being built up from a multitude of coplanar and confined adjacent layers, wherein the build-up direction corresponds to a printing direction of a 3D printing apparatus;

determining a plurality of overhang regions in the layer representation model where the boundary edges of first layers extend over the boundary edges of second layers, the first layers being directly adjacent and subsequent to the second layers when going into the build-up direction of the layer representation model, each of the plurality of overhang regions corresponding to an upper arc of a cylindrical cavity structure or a spheroid cap of a spheroidal cavity structure in the 3D object model of the object;

determining a local overhang angle in each of the plurality of overhang regions, the local overhang angle being defined as the angle between the normal axis of the coplanar layers in build-up direction and the local tangent between the boundary edges of two adjacent layers;

adapting the layer representation model by re-defining the boundary edges of layers in the overhang regions so that the local overhang angle remains below a predetermined overhang threshold angle;

outputting the adapted layer representation model as a 3D printing model to the 3D printing apparatus; and

operating the 3D printing apparatus to print a structural component in accordance with the outputted 3D printing model.

2. The method according to claim 1 , wherein adapting the layer representation model includes re-defining the boundary edges of layers in the overhang regions so that the upper arc of the cylindrical cavity structure is re-defined as triangular prism.

3. The method according to claim 1 , wherein adapting the layer representation model includes re-defining the boundary edges of layers in the overhang regions so that the spheroid cap of a spheroidal cavity structure is re-defined as cone.

4. The method according to claim 2 , wherein adapting the layer representation model includes re-defining the boundary edges of layers in the overhang regions so that the whole cylindrical cavity structure is re-defined as triangular prism.

5. The method according to claim 1 , wherein adapting the layer representation model includes re-defining the boundary edges of layers in the overhang regions so that the whole cylindrical cavity structure is re-defined as Reuleaux triangular prism.

6. A 3D printing system for adapting and using a 3D printing model, the system comprising:

a computer-executable calculation module of a data processing apparatus, configured to receive 3D object model of an object as input and to calculate a layer representation model on the basis of the received 3D object model, the layer representation model being built up from a multitude of coplanar and confined adjacent layers, wherein the build-up direction corresponds to a 3D printing direction;

a computer-executable determination module of the data processing apparatus, coupled to the calculation module and configured to receive the calculated layer representation model, to determine a plurality of overhang regions in the layer representation model where the boundary edges of first layers extend over the boundary edges of second layers, the first layers being directly adjacent and subsequent to the second layers when going into the build-up direction of the layer representation model, each of the plurality of overhang regions corresponding to an upper arc of a cylindrical cavity structure or a spheroid cap of a spheroidal cavity structure in the 3D object model of the object, and to determine a local overhang angle in each of the plurality of overhang regions, the local overhang angle being defined as the angle between the normal axis of the coplanar layers in build-up direction and the local tangent between the boundary edges of two adjacent layers;

a computer-executable adaptation module of the data processing apparatus, coupled to the determination module and configured to adapt the layer representation model by re-defining the boundary edges of layers in the overhang regions so that the local overhang angle remains below a predetermined overhang threshold angle, and to output the adapted layer representation model as a 3D printing model; and

a 3D printing apparatus coupled to receive the outputted 3D printing model, and configured to print a structural component in accordance with the outputted 3D printing model.

7. The system according to claim 6 , wherein the adaptation module is configured to re-define the boundary edges of layers in the overhang regions so that the upper arc of the cylindrical cavity structure is re-defined as triangular prism.

8. The system according to claim 6 , wherein the adaptation module is configured to re-define the boundary edges of layers in the overhang regions so that the spheroid cap of a spheroidal cavity structure is re-defined as cone.

9. The system according to claim 7 , wherein the adaptation module is configured to re-define the boundary edges of layers in the overhang regions so that the whole cylindrical cavity structure is re-defined as triangular prism.

10. The system according to claim 6 , wherein the adaptation module is configured to re-define the boundary edges of layers in the overhang regions so that the whole cylindrical cavity structure is re-defined as Reuleaux triangular prism.

11. A non-transitory computer-readable medium comprising computer-executable instructions which, when executed on a data processing apparatus, cause the data processing apparatus to perform a method for adapting a 3D printing model, the method comprising:

calculating a layer representation model on the basis of a 3D object model of an object, the layer representation model being built up from a multitude of coplanar and confined adjacent layers, wherein the build-up direction corresponds to a printing direction of a 3D printing apparatus;

determining a plurality of overhang regions in the layer representation model where the boundary edges of first layers extend over the boundary edges of second layers, the first layers being directly adjacent and subsequent to the second layers when going into the build-up direction of the layer representation model, each of the plurality of overhang regions corresponding to an upper arc of a cylindrical cavity structure or a spheroid cap of a spheroidal cavity structure in the 3D object model of the object;

determining a local overhang angle in each of the plurality of overhang regions, the local overhang angle being defined as the angle between the normal axis of the coplanar layers in build-up direction and the local tangent between the boundary edges of two adjacent layers;

adapting the layer representation model by re-defining the boundary edges of layers in the overhang regions so that the local overhang angle remains below a predetermined overhang threshold angle; and

outputting the adapted layer representation model as a 3D printing model to the 3D printing apparatus for printing a structural component in accordance with the outputted 3D printing model.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 5, 2016
From: EILKEN, WOLFGANG; TIRYAKI, MEMIS; FELGENHAUER, HENNING
To: AIRBUS OPERATIONS GMBH
Reel/Frame 037732/0586 →
Priority Claims (1)
EP 14194746 · Nov 25, 2014 · regional
Continuity (1)
Related Publication 20160144574A1 · May 26, 2016
Cited By (2)
US 12,191,637 US 12,337,386