Rotor of a turbomachine

1. A rotor of a turbomachine comprising:

a main rotor body; and

a plurality of rotor blades, each rotor blade having:

a blade root, wherein each rotor blade is fastened by its blade root to the main rotor body;

a blade body; and

at least one coupling element segment in the region of a blade body, wherein a width of the coupling element segment of each rotor blade is defined in circumferential direction by edges extending substantially in axial direction,

wherein viewed from radially outside, the at least one coupling element segment, of every rotor blade is contoured such that at a first side to which a coupling element segment of a first directly adjacent rotor blade is connected considered in circumferential direction and

adjacent to a flow inlet side a flow inlet edge of the blade body of the respective rotor blade a radially outer edge of the coupling element segment, which radially outer edge extends substantially in axial direction, projects outwardly in circumferential direction beyond a radially inner edge of the respective coupling element segment, the radially inner edge extends substantially in axial direction,

whereas, at the first side facing away from the flow outlet side from a flow outlet edge of the blade body of the respective rotor blade, the radially inner edge extending substantially in axial direction projecting outwardly in circumferential direction beyond the radially outer edge extending substantially in axial direction, and

the coupling element segment of each rotor blade is contoured such that a second side located opposite the first side, to which second side the coupling element segment of a second directly adjacent rotor blade is connected considered in circumferential direction, adjacent on the flow outlet side to the flow outlet edge of the blade body of the rotor blade,

the radially outer edge of the respective coupling element segment extends substantially in axial direction and projects outwardly in circumferential direction beyond the radially inner edge of the respective coupling element segment, the radially inner edge extends substantially in axial direction,

whereas, at the second side facing away on the flow inlet side from the flow inlet edge of the blade body of the respective rotor blade, the radially inner edge extending substantially in axial direction projects outwardly in circumferential direction beyond the radially outer edge extending substantially in the axial direction, and

wherein the radially inner edge of the respective coupling element segment extends substantially in the axial direction, respectively, delimits two surfaces which are separated from one another by a straight separating line, configured as a surface which is concealed considered from radially outside and a surface which is visible considered from radially outside,

wherein, at the first side and at the second side of each coupling element segment, the separating lines which, at the first side and at the second side, separate the surface which is concealed from radially outside from the surface which is visible from radially outside are formed without an inflection point,

wherein, at the first side and at the second side of the respective coupling element segment viewed along the separating lines, the surface that is concealed from radially outside is inclined relative to the radial direction by a first angle and the surface which is visible from radially outside is inclined relative to the radial direction by a second angle.

2. The rotor according to claim 1 , wherein

at the first side and at the second side, the radially outer edge of the respective coupling element segment, the radially outer edge extends substantially in axial direction, and

wherein, at the first side, the surface which is concealed from radially outside is positioned on the flow inlet side and the surface which is visible from radially outside is positioned on the flow outlet side, and

wherein, at the second side, the surface which is concealed from radially outside is positioned on the flow outlet side and the surface which is visible from radially outside is positioned on the flow inlet side.

3. The rotor according to claim 1 , wherein, at the first side and at the second side of each respective coupling element segment, the first angle and second angle are identical with respect to degree and have different mathematical signs.

4. The rotor according to claim 1 , wherein, at the first side and at the second side of each respective coupling element segment, the first angle and the second angle differ in degree and have different mathematical signs.

5. The rotor according to claim 1 , wherein, at the first side and at the second side of each respective coupling element segment, the surfaces concealed from radially outside and the surfaces visible from radially outside are identically dimensioned and have a surface ratio of 1:1.

6. The rotor according to claim 4 , wherein, at the first side and at the second side of each respective coupling element segment, the surfaces concealed from radially outside and the surfaces visible from radially outside have different dimensions.

7. The rotor according to claim 6 , wherein, at the first side and at the second side, the surfaces concealed from radially outside and the surfaces visible from radially outside have a surface ratio of at least 1:5 and up to 5:1.

8. The rotor according to claim 7 , wherein, at the first side and at the second side of the respective coupling element segment, the surfaces concealed from radially outside and the surfaces visible from radially outside are each two-dimensionally contoured, plane surfaces.

9. The rotor according to claim 7 , wherein, at the first side and at the second side, the surfaces concealed from radially outside and the surfaces visible from radially outside are each three-dimensionally contoured, spatially curved surfaces.

10. The rotor according to one of claim 9 , wherein at least at one of the first side and at the second side of the respective coupling element segment considered from radially outside, the radially outer edge extending substantially in axial direction and the radially inner edge extending substantially in axial direction have a same radial length at a point where the inner and outer sides cross.

11. The rotor according to claim 10 , wherein, at the first side and at the second side, this axial position is positioned in the middle between edges of the coupling element segment on the flow inlet side and edges of the coupling element segment on the flow outlet side.

12. The rotor according to claim 10 , wherein, at the first side and at the second side, this axial position is positioned one of closer to edges of the coupling element segment on the flow inlet side and closer to edges of the coupling element segment on the flow outlet side.

13. The rotor according to claim 1 , wherein each rotor blade has a coupling element segment constructed as outer shroud segment radially outwardly in the area of the blade body.

14. The rotor according to one of claim 1 , wherein every rotor blade has in the area of the blade body thereof a coupling element segment constructed as inner coupling element segment.

15. The rotor according to claim 7 , wherein, at the first side and at the second side, the surfaces concealed from radially outside and the surfaces visible from radially outside have a surface ratio of 1:3 and up to 3:1.