Method of manufacturing a stator component

1. A method for manufacturing a stator component that is intended for a jet engine and intended in operation to guide a gas flow and to transfer loads, comprising

constructing the component of at least two sections in the direction of its circumference, casting the sections in separate pieces,

positioning the at least two sections adjacent to each other,

joining the at least two sections together by welding,

casting each section of the at least two sections in such a shape that a first, radially and axially extending wall element and a second, radially and axially extending wall element are arranged at a distance from each other, an inner plate and an outer plate are disposed at opposite ends of and substantially perpendicular to the first and second wall elements, the first and second walls elements defining between them a gas duct defining a flow path extending in an axial direction of the component, and

joining two wall elements, one from each of two adjacent sections, to each other to form together a radially and axially extending strut, which is closed for an incoming axial flow so that there will be no axial flow path between the joined wall elements.

2. A method according to claim 1 , wherein a surface of each section of the at least two sections that is intended to be welded, extends at least partially around a body of the section and is arranged at its periphery.

3. A method according to claim 2 , wherein the surface of each section of the at least two sections that is intended to be welded extends in both a radial and an axial direction.

4. A method according to claim 3 , wherein the part of the welding surface that forms a change of direction between radial and axial direction is evenly rounded off.

5. A method according to claim 2 , wherein the surface of each section of the at least two sections that is intended to be welded is continuous.

6. A method according to claim 2 , wherein the surface of each section of the at least two sections that is intended to be welded is essentially the same thickness in cross section over a whole length of the surface.

7. A method according to claim 2 , wherein other parts of each section of the at least two sections adjacent to the surface that is intended to be welded are set back in the direction of the circumference in relation to the welding surface.

8. A method according to claim 1 , comprising casting each section of the at least two sections in such a shape that it has at least one rib that extends in a direction of the circumference and projects in an axial direction.

9. A method according to claim 8 , wherein the at least one rib extends in such a way that, for each section of the at least two sections, there is a gap in a direction of the circumference between an end of the rib and an edge of the section.

10. A method according to claim 9 , comprising, after the at least two sections have been placed adjacent to each other in the direction of the circumference, joining the sectors by welding together adjacent edges of the sections between ends of the ribs.

11. A method according to claim 10 , comprising, after the welding together, filling the space between two adjacent rib edges by deposition of material so that the ribs form a continuous structure in the direction of the circumference.

12. A method according to claim 1 , comprising casting two sections that are intended to be joined together in such shapes that ends of the two sections in a direction of the circumference have designs that complement each other, in order that, when they are placed next to each other, they will at least essentially fit tightly against each other.

13. A method according to claim 1 , comprising casting two sections that are intended to be joined together in such shapes that end surfaces of ends of the two sections extend in a direction of the circumference parallel to a plane in a radial direction.

14. A method according to claim 1 , comprising joining two adjacent sections together by laser welding from an outside of at least one of the sections.

15. A method according to claim 1 , comprising casting each section of the at least two sections with wall elements that form a continuous structure in a radial direction.

16. A method according to claim 1 , comprising casting each section of the at least two sections in such a shape that the first wall element and the second wall element are arranged in relation to each other in such a way that in the intended position in the component they at least partially extend essentially in the radial direction of the component.

17. A method according to claim 1 , wherein the stator component is intended for a gas turbine.