Method of manufacturing a wall

Patent metadata

Field	Value
Publication number	US-9498848-B2
Application number	US-201314108742-A
Country	US
Kind code	B2
Filing date	Dec 17, 2013
Priority date	Jan 30, 2013
Publication date	Nov 22, 2016
Grant date	Nov 22, 2016

Abstract

A method of manufacturing an annular wall ( 46 ) of a combustion chamber ( 15 ) comprises depositing layers of a metal sequentially one upon the other to form layers of a spiral wall ( 45 ) of the combustion chamber ( 15 ). Each layer of metal is deposited in a spiral pathway ( 122 ). The ends (E 1 , E 2 ) of the spiral wall ( 45 ) of the combustion chamber ( 15 ) are joined together to form the annular wall ( 46 ) of the combustion chamber ( 15 ). The ends (E 1 , E 2 ) of the spiral wall ( 45 ) of the combustion chamber ( 15 ) are at the opposite ends of the spiral pathway ( 122 ).

First claim

The invention claimed is:

1. A method of manufacturing a wall, the method comprising
(a) depositing layers of a metal sequentially one upon the other to form layers of a spiral wall, depositing each layer of metal in a spiral pathway, and
(b) abutting and joining the ends of the spiral wall to form an annular wall, the ends of the spiral wall being at the opposite ends of the spiral pathway.

2. The method as claimed in claim 1 wherein step (b) comprises rolling the spiral wall into a ring before joining the ends of the spiral wall together.

3. The method as claimed in claim 1 wherein step (a) comprises controlling the deposition of the layers of metal to form apertures in the spiral wall.

4. The method as claimed in claim 1 wherein step (a) comprises:
(i) depositing a layer of a metal powder onto a platform,
(ii) directing a radiation beam in at least one spiral pathway onto the layer of metal powder deposited in step (i) to melt and sinter the metal powder to form a layer of the spiral wall,
(iii) depositing a further layer of a metal powder onto the previously deposited layer of metal powder,
(iv) directing a radiation beam in at least one spiral pathway onto the layer of powder metal deposited in step (iii) to melt and sinter the metal powder to form a further layer of the spiral wall and to bond the further layer of metal powder to the previously deposited layer of metal powder, and
(v) repeating steps (iii) and (iv) a plurality of times to build up the spiral wall.

5. The method as claimed in claim 4 wherein step (ii) is selected from the group consisting of directing a laser beam onto the layer of metal powder, directing a microwave beam onto the layer of metal powder and directing an electron beam onto the layer of metal powder.

6. The method as claimed in claim 4 wherein step (iv) is selected from the group consisting of directing a laser beam onto the layer of metal powder, directing a microwave beam onto the layer of metal powder and directing an electron beam onto the layer of metal powder.

7. The method as claimed in claim 4 wherein step (a) is performed in a fused powder bed apparatus, the fused powder bed apparatus having base dimensions of 250 mm by 250 mm and the diameter of the annular wall is greater than 250 mm.

8. The method as claimed in claim 1 wherein step (a) comprises:
(i) depositing a layer of a molten metal in at least one spiral pathway onto a platform to form a layer of the spiral wall,
(ii) depositing a further layer of molten metal in at least one spiral pathway on the previously deposited layer of molten metal to form a further layer of the spiral wall and to bond the further layer of the spiral wall to the previously deposited layer of the spiral wall, and
(iii) repeating step (ii) a plurality of times to build up the spiral wall.

9. The method as claimed in claim 8 wherein steps (i) and (ii) comprise depositing the layer of molten metal using a welding torch.

10. The method as claimed in claim 9 comprising depositing the layer of molten metal using a TIG welding torch.

11. The method as claimed in claim 8 wherein steps (i) and (ii) comprise depositing the layer of molten metal by direct laser deposition.

12. The method as claimed in claim 1 wherein the annular wall is an annular wall of a combustion chamber.

13. The method as claimed in claim 12 wherein step (a) comprises controlling the deposition of the layers of metal to form apertures in the spiral wall.

14. The method as claimed in claim 13 wherein the apertures in the spiral wall are selected from the group consisting of dilution apertures, cooling apertures and mounting apertures.

15. The method as claimed in claim 12 wherein step (a) comprises depositing additional layers of a metal sequentially one upon the other to form layers of an additional spiral wall, each of the additional layers of metal being deposited in a spiral pathway, the additional spiral wall being spaced radially from the spiral wall, and depositing metal so as to interconnect the spiral wall and the additional spiral wall.

16. The method as claimed in claim 15 wherein step (a) comprises controlling the deposition of the additional layers of metal to form apertures in the additional spiral wall.

17. The method as claimed in claim 16 wherein the apertures in the additional spiral wall are selected from the group consisting of dilution apertures and cooling apertures.

18. The method as claimed in claim 12 wherein step (a) comprises depositing layers of metal sequentially one upon the other to form a first spiral wall, a second spiral wall spaced from the first spiral wall and interconnecting structure connecting the first spiral wall and the second spiral wall to form a hollow spiral wall, and step (b) comprises abutting and joining the ends of the hollow spiral wall to form a hollow annular wall.

19. The method as claimed in claim 18 wherein step (a) comprises controlling the deposition of the layers of metal to form apertures in the first spiral wall and the second spiral wall.

20. The method as claimed in claim 19 wherein the apertures in the first spiral wall and the second spiral wall are selected from the group consisting of dilution apertures and cooling apertures.

21. The method as claimed in claim 1 wherein the annular wall is an annular casing.

22. The method as claimed in claim 21 wherein the annular casing is selected from the group consisting of a fan casing, a compressor casing, a combustion casing, a turbine casing and a combined combustion and turbine casing.

23. The method as claimed in claim 21 comprising forming at least one annular flange, the annular flange is selected from the group consisting of an annular flange extending radially inwardly from the annular casing and an annular flange extending radially outwardly from the annular casing.

24. The method of manufacturing a plurality of wall portions, the method comprising
(a) depositing layers of a metal sequentially one upon the other to form layers of a spiral wall, depositing each layer of metal in a spiral pathway, and
(b) cutting the spiral wall into portions to form the plurality of wall portions.

25. The method as claimed in claim 24 wherein step (b) comprises rolling the spiral wall flat before cutting the spiral wall into the plurality of wall portions.

26. A method of manufacturing a wall, the method comprising
(a) depositing layers of a metal sequentially one upon the other to form layers of a spiral wall, and
(b) abutting and joining the ends of the spiral wall to form an annular wall, the ends of the spiral wall being at the opposite ends of the spiral wall,
wherein step (a) comprises:
(i) depositing a layer of a metal powder onto a platform,
(ii) directing a radiation beam onto the layer of metal powder deposited in step (i) and scanning the radiation beam across the layer of metal powder in a predetermined pattern to melt and sinter the metal powder to form a layer of the spiral wall,
(iii) depositing a further layer of a metal powder onto the previously deposited layer of metal powder,
(iv) directing a radiation beam onto the layer of powder metal deposited in step (iii) and scanning the radiation beam across the layer of metal powder in a predetermined pattern to melt and sinter the metal powder to form a further layer of the spiral wall and to bond the further layer of metal powder to the previously deposited lay

Assignees

• Rolls Royce Plc

Inventors

• Garry Ian Murray

Classifications

• B22F5/009 Primary

  of turbine components other than turbine blades (of turbine blades B22F5/04) · CPC title

• B22F12/41

  characterised by the type, e.g. laser or electron beam · CPC title

• B22F10/32

  of the atmosphere, e.g. composition or pressure in a building chamber · CPC title

• B22F10/30

  Process control · CPC title

• B22F10/25

  Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS] · CPC title