Manufacturing of Components from Parts Made from Different Materials, Particularly of Space Transportation Components Such as Combustion Chambers for Thrusters

1 . A method for manufacturing of components from parts made from different materials, the method comprising:

producing a transition between one part made from a first material and another part made from a second material using an additive layer manufacturing method, wherein the additive layer manufacturing method comprises starting with the first material and then gradually changing a material composition to the second material.

2 . The method of claim 1 , wherein the additive layer manufacturing uses a powder bed, a powder feeding, or a wire feeding for producing the transition between the one part to the another part.

3 . The method of claim 2 , wherein the additive layer manufacturing method uses at least two individual powder feeders, wherein one powder feeder is configured to produce layers of the first material and another powder feeder is configured to produce layers of the second material.

4 . The method of claim 3 , wherein an energy source of the powder feeders are a laser or an electron beam.

5 . The method of claim 2 , wherein the gradually changing of the material composition from the first material to the second material comprises:

starting with a deposition of the first material by a powder feeding of the first material,

then gradually decreasing the powder feeding of the first material and at the same time gradually increasing a powder feeding of the second material, and

ending with an isolated deposition layer of the second material.

6 . The method of claim 2 , wherein the gradually changing of the material composition from the first material to the second material comprises:

starting with a deposition of the first material by wire feeding of the first material,

then gradually decreasing the wire feeding of the first material and at the same time gradually increasing a wire feeding of the second material, and

ending with an isolated deposition layer of the second material.

7 . The method of claim 2 , wherein the gradually changing of the material composition from the first material to the second material comprises

creating a powder bed of a pre-mix of the first and the second material with the material composition gradually changing from the first to the second material, and

selectively melting the entire created powder bed with a point heat source.

8 . The method of claim 1 , wherein the components are combustion chambers for thrusters.

9 . A device for manufacturing of components from parts made from different materials comprising:

a control computer; and

additive layer manufacturing means, controlled by the control computer, for producing a transition between one part made from a first material and another part made from a second material, wherein the additive layer manufacturing means produces the transition with a gradually changing material composition starting with the first material to the second material.

10 . The device of claim 9 wherein the additive layer manufacturing means comprise:

at least two individual powder feeders, wherein one powder feeder is configured to produce layers of the first material and another powder feeder is configured to produce layers of the second material.

11 . The device of claim 10 , wherein an energy source of the powder feeders are a laser or an electron beam.

12 . The device of claim 9 , wherein the additive layer manufacturing means produce transition with a gradually changing material composition starting with the first material to the second material by

starting with a deposition of the first material by a powder feeding of the first material,

then gradually decreasing of the powder feeding of the first material and at the same time gradually increasing a powder feeding of the second material, and

ending with an isolated deposition layer of the second material.

13 . The device of claim 9 , wherein the additive layer manufacturing means produce the transition with a gradually changing material composition starting with the first material to the second material by

starting with a deposition of the first material by wire feeding of the first material,

then gradually decreasing the wire feeding of the first material and at the same time gradually increasing wire feeding of the second material, and

ending with an isolated deposition layer of the second material.

14 . The device of claim 9 wherein the additive layer manufacturing means produce the transition with a gradually changing material composition starting with the first material to the second material by

creating a powder bed of a pre-mix of the first and the second material with material composition gradually changing from the first to the second material, and

selectively melting the entire created powder bed with a point heat source.

15 . The device of claim 9 , wherein the components include a combustion chamber for a thruster.