IP Library › Granted Patent US 10,919,227
Granted Patent B2
US 10,919,227 · App. 16/965,033 · Granted Feb 16, 2021

Manufacturing system for use in space

Inventor: Austin James Cook (Balderstone, GB)
Assignee: BAE Systems plc
B29C64/357B23K26/342B23K26/38B23Q1/64B29C64/118B29C64/245B29C64/25B29C64/393B33Y30/00B33Y40/20B33Y50/02B33Y70/00B64G1/22B29K2069/00B29K2079/085
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Quick Facts
Patent No.
US 10,919,227
App. No.
16/965,033
Granted
Feb 16, 2021
Kind
B2
Abstract

A system comprising: an additive manufacturing apparatus configured to perform an additive manufacturing process using a feedstock supplied thereto, thereby to produce an article; a feedstock storage module configured to supply feedstock to the additive manufacturing apparatus; a machining apparatus configured to perform a machining process; a controller configured to control operation of the additive manufacturing apparatus and the machining apparatus; and are cycling module configured to receive a waste material and to produce the feedstock therefrom, and to transfer the produced feedstock to the feedstock storage module. The additive manufacturing apparatus and the machining apparatus comprise a common heat source, the additive manufacturing apparatus configured to use the common heat source to perform the additive manufacturing process, and the machining apparatus configured to use the common heat source to perform the machining process.

Claims (35)

1. A system comprising:

an additive manufacturing apparatus configured to perform an additive manufacturing process using a feedstock supplied thereto, thereby to produce an article;

a feedstock storage module configured to supply feedstock to the additive manufacturing apparatus;

a machining apparatus configured to perform a machining process;

a controller configured to control operation of the additive manufacturing apparatus and the machining apparatus; and

a recycling module configured to receive a waste material and to produce the feedstock therefrom, and to transfer the produced feedstock to the feedstock storage module; wherein

the additive manufacturing apparatus and the machining apparatus comprise a common heat source, the additive manufacturing apparatus is configured to use the common heat source to perform the additive manufacturing process, and the machining apparatus is configured to use the common heat source to perform the machining process.

2. The system of claim 1 , wherein the system is for in-space manufacture of articles.

3. The system of claim 1 , wherein the system is arranged for launch delivery into space.

4. The system of claim 1 , wherein the additive manufacturing apparatus comprises stabilisation means for stabilising a workpiece during the additive manufacturing process.

5. The system of claim 1 , wherein the machining apparatus comprises stabilisation means for stabilising an object undergoing a machining process.

6. The system of claim 5 , wherein the additive manufacturing apparatus comprises stabilisation means for stabilising a workpiece during the additive manufacturing process; and

wherein the stabilisation means of the additive manufacturing apparatus is the same as the stabilisation means of the machining apparatus.

7. The system of claim 1 , wherein the additive manufacturing apparatus and the machining apparatus are located in a common hermetic enclosure.

8. The system of claim 1 , wherein the additive manufacturing apparatus is configured to, using the common heat source, implement the additive manufacturing process to build the article onto a build tray, and the machining apparatus is configured to, using the common heat source, cut the built article from the build tray.

9. The system of claim 1 , wherein the recycling module is configured to receive at least some of the waste material from the additive manufacturing apparatus, the waste material being waste material from the additive manufacturing process.

10. The system of claim 1 , wherein the recycling module is configured to receive the waste material from the machining apparatus, the waste material being waste material from the machining process.

11. The system of claim 1 , wherein the common heat source comprises one or more lasers.

12. The system of claim 1 , wherein the feedstock comprises one or more materials selected from the group of materials consisting of: tungsten, titanium, aluminium, copper, polyetherimide, and polycarbonate.

13. The system of claim 1 , wherein

the system further comprises a storage module configured to store one or more articles that are to be repaired or modified by the additive manufacturing apparatus;

one or both of the additive manufacturing apparatus and the machining apparatus is configured to receive an article to be repaired from the storage module.

14. The system of claim 1 , wherein the system further comprises an inspection module configured to measure a surface of the article.

15. The system of claim 1 , wherein the additive manufacturing apparatus is a wire-based or filament-based additive manufacturing apparatus and the feedstock comprises a wire or a filament.

16. The system of claim 1 , wherein either:

the additive manufacturing process is a plastics-based additive manufacturing process and the feedstock comprises a plastic; or

the additive manufacturing process is a metal-based additive manufacturing process and the feedstock comprises a metal.

17. The system of claim 1 , wherein the system is located on a vehicle configured to be launched into space.

18. An entity comprising the system of claim 1 , the entity being an entity selected from the group of entities consisting of a space vehicle, a satellite, and a space station.

19. The entity of claim 18 , wherein

the entity is configured to dock, in space, with a further entity; and

the recycling module is configured to receive the waste material from the further entity when it is docked with the entity and/or the entity is configured to send the article to the further entity when it is docked with the entity.

20. The entity of claim 18 , wherein

the entity is configured to dock, in space, with a further entity; and

the storage module is configured to receive the article to be repaired from the further entity when it is docked with the entity and/or the entity is configured to send the repaired article to the further entity when it is docked with the entity.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 6, 2020
From: COOK, AUSTIN JAMES
To: BAE SYSTEMS PLC
Reel/Frame 053420/0839 →
Priority Claims (2)
EP 18157631 · Feb 20, 2018 · regional
GB 1802704 · Feb 20, 2018 · national
Continuity (1)
Related Publication 20200406551A1 · Dec 31, 2020
Cited By (9)
US 12,198,356 US 12,203,371 US 12,215,926 US 12,297,792 US 12,298,042 US 12,371,919 US 12,404,042 US 12,467,421 US 12,729,019