Additive layer manufacturing method for producing a three-dimensional object

Patent metadata

Field	Value
Publication number	US-9636869-B2
Application number	US-201414199556-A
Country	US
Kind code	B2
Filing date	Mar 6, 2014
Priority date	Mar 7, 2013
Publication date	May 2, 2017
Grant date	May 2, 2017

Abstract

An additive layer manufacturing method is disclosed for producing a three-dimensional object and to a corresponding object. Layers of a powder material are applied to a carrier and irradiated, before the following layer is applied, with a laser beam or particle beam selectively only in the areas of the layer which correspond to the three-dimensional object to be produced. Irradiation occurs such that the powder material in the corresponding areas is locally melted or sintered. A first portion is constructed before a second portion or the first portion is provided as a separate component, on which a support structure and second portion are constructed. The support structure is constructed in the form of a plurality of support legs, which extend from the first portion to the second portion and are connected thereto at their opposite ends and are spaced apart from one another at least along part of their length.

First claim

The invention claimed is:

1. An additive layer manufacturing method for producing a three-dimensional object, wherein in the method a plurality of layers of a powder material are applied one after another and one on top of another to a carrier and each layer is irradiated, before a following layer is applied, with a laser beam or particle beam selectively only in areas of the layer which correspond to the three-dimensional object to be produced, wherein the irradiation takes place such that the powder material in the corresponding areas is locally melted or sintered, wherein:
the object has a first portion, a second portion and a support structure between the first and the second portion, which connects the first and the second portion to one another, wherein in the course of the layer-by-layer construction of the object the first portion is constructed before the second portion or the first portion is provided as a separate component, on which the support structure and the second portion are constructed; and
in the method the support structure is constructed in a form of a plurality of support legs, which extend in each case from the first portion to the second portion and are connected to these at their opposite ends and are spaced apart from one another at least along part of their length.

2. The method according to claim 1 wherein the support legs are designed and arranged such that each support leg widens at least in a longitudinal section adjoining the second portion in a direction of construction defined by the layer-by-layer construction.

3. The method according to claim 2 , wherein during the layer-by-layer construction of the object:
all sections of the outer surfaces of the support legs which, viewed contrary to a direction of force of gravity, define an overhang do not exceed an inclination angle of 50° in relation to the direction of force of gravity; or
with exception of sections of the outer surfaces in areas of the outer surfaces, facing one another, of adjacent support legs at their ends facing the second portion, all sections of the outer surfaces of the support legs which, viewed contrary to the direction of force of gravity, define an overhang do not exceed an inclination angle of 50° in relation to the direction of force of gravity.

4. The method according to claim 1 , wherein the support legs are constructed such that,
for at least some adjacent ones of the support legs, their ends connected to the second portion are spaced apart from one another,
for at least some adjacent ones of the support legs, their ends connected to the second portion touch one another at the second portion and/or,
for at least some adjacent ones of the support legs, the outer surfaces, facing one another, of the ends, facing the second portion, of the respective adjacent support legs merge, forming an arc-shaped rounding, wherein the radius of curvature of the rounding is 7 mm at most.

5. The method according to claim 1 , wherein during the layer-by-layer construction of the object, except for areas of the outer surface of the second portion located between the support legs, all sections of the outer surfaces of the second portion which, viewed contrary to a direction of force of gravity, define an overhang do not exceed an inclination angle of 50° in relation to a direction of force of gravity, at least on the side of the second portion facing the first portion.

6. The method according to claim 1 , wherein the first portion and the second portion are functional sections, which fulfil a function going beyond a support function between two portions in a completed object.

7. The method according to claim 1 , wherein the first portion is a flat plate.

8. The method according to claim 7 , wherein the plate is oriented perpendicular to a direction of force of gravity during the layer-by-layer construction of the object.

9. The method according to claim 1 , wherein the second portion is an elongate element, the direction of extension of which during the layer-by-layer construction of the object extends at an angle of more than 45° to a direction of force of gravity at least along part of a length of the element.

10. The method according to claim 9 , wherein the elongate element is a tube or pipe or a cylindrical element.

11. The method according to claim 7 , wherein the second portion is an elongate element, the direction of extension of which during the layer-by-layer construction of the object extends at an angle of more than 45° to a direction of force of gravity at least along part of a length of the element and wherein the elongate element extends in a plane parallel to a plane defined by the plate.

12. The method according to claim 11 , wherein the elongate element is a tube or pipe or a cylindrical element.

13. The method according to claim 9 , wherein the support legs are constructed and arranged such that they are arranged in transverse and longitudinal rows perpendicular to one another in relation to the direction of extension of the elongate element.

14. The method according to claim 1 , wherein the support legs are constructed such that at least some of the support legs, directly adjoining the first portion, have an area in which they taper in a direction of construction defined by the layer-by-layer construction and which a longitudinal section of the respective support leg which widens in the direction of construction follows.

15. The method according to claim 1 , wherein selective laser melting (SLM), selective laser sintering (SLS), selective electron beam melting or selective electron beam sintering is used as the additive layer manufacturing method.

16. The method according to claim 1 , wherein the object is a hydraulic distribution system or a part of a hydraulic distribution system.

17. The method according to claim 1 , wherein the second portion is an elongate element, a direction of extension of which during the layer-by-layer construction of the object extends at an angle perpendicular to a direction of force of gravity at least along part of a length of the element.

18. The method according to claim 17 , wherein the elongate element is a tube or pipe or a cylindrical element.

19. The method according to claim 7 , wherein the second portion is an elongate element, a direction of extension of which during the layer-by-layer construction of the object extends at an angle perpendicular to a direction of force of gravity at least along part of a length of the element and wherein the elongate element extends in a plane parallel to a plane defined by the plate.

20. The method according to claim 19 , wherein the elongate element is a tube or pipe or a cylindrical element.

21. The method according to claim 17 , wherein the support legs are constructed and arranged such that they are arranged in transverse and longitudinal rows perpendicular to one another in relation to a direction of extension of the elongate element.

Assignees

• Airbus Operations Gmbh

Inventors

• Kroll Lothar
• Schubert Frank
• Blümer Sebastian
• Hummel Gerhard

Classifications

• B22F10/66

  by mechanical means · CPC title

• B22F10/62

  by chemical means · CPC title

• B22F10/47

  characterised by structural features · CPC title

• B22F10/385

  Overhang structures · CPC title

• B22F10/28

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