Method for assembling a stator stage of a gas turbine engine

1. A method for assembling a stator stage of a gas turbine engine, comprising at least one vane segment and at least a central section, wherein the vane segment comprises at least one wall segment and a gap, wherein the at least one wall segment restricts the gap in at least one direction, wherein the central section comprises at least one circumferential slot and an axial through hole passing in a direction basically perpendicular to a circumferential direction of the slot through the slot, the method comprising:

inserting an adjustment pin into the through hole, wherein the adjustment pin comprises two end sections and a middle portion extending between the end sections and having at least one action device,

inserting the at least one wall segment of the vane segment in the slot of the central section so that the gap is circumferentially aligned with the through hole of the central section,

rotating the adjustment pin in its circumferential direction so that the central section is correctly positioned in the stator stage through interaction of the at least one wall segment with the at least one action device of the adjustment pin,

deforming a deformable part of the adjustment pin so that the now deformed part establishes a force fit with at least one segment of a corresponding structure of the central section, and thereby

locking the adjustment pin and thus the central section in a fixed position in the stator stage.

2. The method according to claim 1 ,

wherein at least one section of the deformable part of the adjustment pin is deformed.

3. The method according to claim 1 ,

wherein the deformable part is embodied as a protrusion of at least one end section of the adjustment pin and extends in an axial direction of the adjustment pin and at least partially along a circumference of the at least one end section.

4. The method according to claim 1 ,

wherein the corresponding structure of the central section is a groove, wherein the deformed part of the adjustment pin is locked in the groove of the central section, and/or wherein the corresponding structure is a groove extending in an outer surface of the central section and in circumferential direction of the central section.

5. The method according to claim 1 ,

wherein at least two deformed sections of the deformed part are built during the deformation and wherein the central section comprises at least two circumferential grooves in an outer surface of the central section and wherein each deformed section is locked in one of the two circumferential grooves.

6. The method according to claim 1 ,

wherein the deformable part of the adjustment pin is arranged in such a way in the through hole to be accessible from an outside of the stator stage.

7. The method according to claim 1 ,

wherein the action device of the adjustment pin is embodied as an eccentrically arranged middle portion and wherein the eccentric middle portion contacts the at least one wall segment of the vane segment to correctly position the central section in the stator stage.

8. The method according to claim 1 ,

wherein the adjustment pin and/or the central section is locked in its circumferential position in the stator stage.

9. The method according to claim 1 ,

wherein the deformable part of the adjustment pin is deformed by peening.

10. A stator stage of a gas turbine engine, comprising

at least one vane segment and at least a central section, wherein the vane segment comprises at least one wall segment and a gap, wherein the at least one wall segment restricts the gap in at least one direction, wherein the central section comprises at least one circumferential slot and an axial through hole passing in a direction basically perpendicular to a circumferential direction of the slot through the slot,

an adjustment pin, wherein the adjustment pin is inserted into the through hole, wherein the adjustment pin comprises two end sections and a middle portion extending between the end sections and having at least one action device,

wherein the at least one wall segment of the vane segment is inserted in the slot of the central section so that the gap is circumferentially aligned with the through hole of the central section,

wherein the adjustment pin is arranged in its circumferential direction so that the central section is correctly positioned in the stator stage through interaction of the at least one wall segment with the at least one action device of the adjustment pin,

wherein a deformable part of the adjustment pin is deformed so that the now deformed part establishes a force fit with at least one segment of a corresponding structure of the central section and thereby

wherein the adjustment pin and thus the central section are locked in a fixed position in the stator stage.

11. The stator stage according to claim 10 ,

wherein the deformable part is embodied as a protrusion of at least one end section and extends in an axial direction of the adjustment pin and at least partially along a circumference of the at least one end section.

12. The stator stage according to claim 10 , further comprising:

a drive slot extending basically perpendicular to the axial direction of the adjustment pin and/or wherein the drive slot divides the deformable part in two sectors.

13. The stator stage according to claim 12 ,

wherein the drive slot is embodied as a hex head slot or wherein the drive slot is embodied as a cross head slot.

14. The stator stage according to claim 12 , further comprising:

a first and a second end section, wherein the drive slot is arranged in the first end section and the deformable part is arranged at the second end section.