Continuous linear production in a selective laser sintering system

Patent metadata

Field	Value
Publication number	US-9522501-B2
Application number	US-88663110-A
Country	US
Kind code	B2
Filing date	Sep 21, 2010
Priority date	Sep 21, 2010
Publication date	Dec 20, 2016
Grant date	Dec 20, 2016

Abstract

A method and apparatus for forming objects. Layers of precursor material may be placed on top of each other. The layers of precursor material may be selectively cured as the layers of precursor material are placed on top of each other to form an object and a frame associated with the object.

First claim

What is claimed is:

1. A method for forming objects, the method comprising:
placing layers of precursor material on top of each other;
selectively curing the layers of precursor material as the layers of precursor material are placed on the top of each other to form an object and a frame associated with the object, the frame comprising a plurality of base structures, wherein selectively curing the layers comprises:
determining whether a new base structure in the frame is needed;
responsive to a determination that the new base structure is needed, selectively curing the new layer of precursor material to form a portion of the object and a portion of the new base structure; and
responsive to an absence of the determination that the new base structure is needed, selectively curing the new layer of precursor material to form the portion of the object without forming the portion of the new base structure;

moving the frame to allow a new layer of precursor material to be placed on a prior layer of precursor material in the layers of precursor material that have been selectively cured; and
placing the new layer of precursor material on the prior layer of precursor material.

2. The method of claim 1 , wherein selectively curing the layers further comprises:
responsive to the determination that the new base structure is needed, repeating the steps of:
moving the frame to allow a new layer of precursor material to be placed on the prior layer of precursor material in the layers of precursor material that has been selectively cured;
placing the new layer of precursor material on the prior layer of precursor material; and
selectively curing the new layer of precursor material to form a portion of the object and a portion of the new base structure until the new base structure is completed.

3. The method of claim 1 further comprising:
responsive to the absence of the determination that the new base structure is needed, repeating the steps of:
moving the frame to allow the new layer of precursor material to be placed on the prior layer of precursor material in the layers of precursor material that have been selectively cured;
placing the new layer of precursor material on the prior layer of precursor material; and
selectively curing the new layer of precursor material to form a portion of the object without the new base structure until the new base structure is needed.

4. The method of claim 1 , wherein the step of responsive to the determination that the new base structure is needed further comprises:
responsive to the determination that the new base structure is needed, selectively curing the new layer of precursor material to form the portion of the object and the portion of the new base structure.

5. The method of claim 4 further comprising:
separating using cutters, each portion of the object from an associated base structure connected to the each portion of the object.

6. The method of claim 1 further comprising:
forming a base structure; and
placing the base structure in a movement system prior to placing the layers of precursor material on the base structure.

7. The method of claim 1 further comprising:
maintaining a desired temperature for the object as the object is formed in a chamber.

8. The method of claim 7 , wherein the step of maintaining the desired temperature for the object as the object is formed in the chamber further comprises:
maintaining the desired temperature for the object in different locations as the object is formed in the chamber using a plurality of heating and cooling elements.

9. The method of claim 1 further comprising:
cooling uncured precursor material to change a density of the uncured precursor material such that a flow of gas through the precursor material is reduced.

10. The method of claim 1 , wherein a movement system holds and moves the frame along an axis.

11. The method of claim 5 , wherein a separation system comprising cutters, separates the each portion of the object from the associated base structure connected to the each portion of the object.

12. A method for forming aircraft parts, the method comprising:
placing layers of precursor material on a base structure for a frame in which the layers of precursor material are selected from one of a powder, a liquid, a metal powder, a ceramic powder, and a plastic powder;
selectively curing the layers of precursor material using a curing system selected from one of a heating system, a laser, and an electron beam after placing the layers of precursor material on the base structure to form a portion of an aircraft part and a portion of the frame to form a prior layer of precursor material;
moving the frame to allow a new layer of precursor material to be placed on the prior layer of precursor material in the layers of precursor material that have been selectively cured, wherein the moving of the frame is performed by a movement system which holds and moves the frame along an axis;
placing the new layer of precursor material on the prior layer of precursor material;
determining whether a new base structure in the frame is needed;
responsive to a determination that the new base structure is needed, selectively curing the new layer of precursor material to form an additional portion of the aircraft part and a portion of the new base structure;
responsive to the determination that the new base structure is needed, repeating the steps of moving the frame to allow the new layer of precursor material to be placed on the prior layer of precursor material in the layers of precursor material that have been selectively cured; placing the new layer of precursor material on the prior layer of precursor material; and selectively curing the new layer of precursor material to form a portion of the aircraft part and the portion of the new base structure until the base structure is completed;
responsive to an absence of the determination that the new base structure is needed, selectively curing the new layer of precursor material to form the additional portion of the aircraft part without forming the new base structure;
responsive to the absence of the determination that the new base structure is needed, repeating the steps of moving the frame to allow the new layer of precursor material to be placed on the prior layer of precursor material in the layers of precursor material that have been selectively cured; placing the new layer of precursor material on the prior layer of precursor material; and selectively curing the new layer of precursor material to form the portion of the aircraft part without the new base structure until the new base structure is needed;
maintaining a desired temperature for the aircraft part as the aircraft part is formed in different locations in a chamber using a plurality of heating and cooling elements;
cooling uncured precursor material to change a density of the uncured precursor material such that a flow of gas through the precursor material is reduced; and
separating each portion of the aircraft part from an associated base structure connected to the each portion of the aircraft part using a separation system, wherein the separations system comprises cutters.

Assignees

• Lyons Brett Ian
• Boeing Co

Inventors

• Lyons Brett Ian

Classifications

• B33Y30/00

  Apparatus for additive manufacturing; Details thereof or accessories therefor · CPC title

• B29C64/153

  using layers of powder being selectively joined, e.g. by selective laser sintering or melting · CPC title

• B33Y50/02

  for controlling or regulating additive manufacturing processes · CPC title

• B29C64/357

  Recycling · CPC title

• B29C64/40

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