Vortex generating device

1. A vortex generating device comprising:

a body having a leading edge and a trailing edge, a streamwise direction (l) extending from the leading edge to the trailing edge, the body further exhibiting a spanwise extent extending along a spanwise direction (s);

the body, in profile cross sections taken across the spanwise direction, exhibiting an airfoil-shaped geometry, each airfoil-shaped profile cross section having a camber line extending from the leading edge to the trailing edge, at least two of the camber lines exhibiting different camber angles, such that the body exhibits at least two different flow deflection angles along the spanwise extent;

a first surface extending between the leading edge and the trailing edge and having airfoil-shaped profile lines on a first side of the respective camber lines and a second surface extending between the leading edge and the trailing edge, and having airfoil-shaped profiles on an opposite second side of the respective camber lines, and the first and second surface joining each other at the leading edge and at the trailing edge;

wherein the trailing edge extends from a first spanwise end to a second spanwise end, and the trailing edge, when seen from a downstream viewpoint, includes a first section which is convexly shaped on a side of the first surface and is concavely shaped on a side of the second surface, and includes a second section which is concavely shaped on a side of the first surface and is convexly shaped on a side of the second surface;

an imaginary trailing edge diagonal extending straight from the first spanwise end of the trailing edge to the second spanwise end of the trailing edge, wherein when seen from the downstream viewpoint, the trailing edge crosses the imaginary trailing edge diagonal exactly once at one diagonal crossing point; and

wherein the trailing edge, when seen from the downstream viewpoint, comprises:

at least two trailing edge segments which abut each other at a nonzero angle, and wherein the nonzero angle between each of the at least two trailing segments is an obtuse angle.

2. The vortex generating device according to claim 1 , wherein the trailing edge, when seen from the downstream viewpoint, comprises:

exactly one first section which extends from the first spanwise end and wherein the trailing edge is convexly shaped on a side of the first surface and is concavely shaped on a side of the second surface; and

exactly one second section which extends from the second spanwise end and wherein the trailing edge is concavely shaped on the side of the first surface and is convexly shaped on the side of the second surface.

3. The vortex generating device according to claim 1 , wherein the trailing edge, when seen from the downstream viewpoint, is symmetric to the diagonal crossing point.

4. The vortex generating device according to claim 1 , wherein the trailing edge is shaped such that at least one imaginary trailing edge mean line exists which, when seen from the downstream viewpoint, is parallel to the leading edge and equidistant from the first spanwise end of the trailing edge and the second spanwise end of the trailing edge, and wherein in a course of the trailing edge extending along a spanwise extent and starting from the diagonal crossing point to any of the first and second spanwise ends of the trailing edge, a distance (h) of the trailing edge from the imaginary trailing edge mean line, when seen from the downstream viewpoint, monotonically increases.

5. The vortex generating device according to claim 1 , wherein the trailing edge is shaped such that an imaginary trailing edge mean line exists which, when seen from the downstream viewpoint, is equidistant from the first spanwise end of the trailing edge and the second spanwise end of the trailing edge, and wherein the trailing edge at the spanwise ends, or any tangent to the trailing edge at the spanwise ends, respectively, extends parallel to the imaginary trailing edge mean line.

6. The vortex generating device according to claim 5 , wherein the imaginary trailing edge mean line, when seen from the downstream viewpoint, extends parallel to the leading edge.

7. The vortex generating device according to claim 1 , wherein the trailing edge, when seen from the downstream viewpoint, comprises:

at least one curved trailing edge segment.

8. The vortex generating device according to claim 1 , wherein the at least two trailing edge segments, when seen from the downstream viewpoint, comprises:

a first straight trailing edge segment extending from the first spanwise end of the trailing edge to an inner end of the first straight trailing edge segment, a second straight trailing edge segment extending from the second spanwise end of the trailing edge to an inner end of the second straight trailing edge segment, and a third straight trailing edge segment which abuts the first and the second straight trailing edge segments at their inner ends and crosses the imaginary trailing edge diagonal.

9. The vortex generating device according to claim 1 , wherein the trailing edge, when seen from the downstream viewpoint, extends in a curved manner between the first spanwise end and the second spanwise end of the trailing edge.

10. The vortex generating device according to claim 1 , wherein a smallest angle (a) enclosed by any two trailing edge segments, or any tangents of trailing edge segments, respectively, when seen from the downstream viewpoint, is larger than 90°.

11. The vortex generating device according to claim 1 , configured as a fuel discharge device, comprising:

at least one fuel supply plenum is inside the body; and

at least one fuel discharge opening is at the trailing edge, whereby the fuel discharge opening is in fluid communication with a fuel supply plenum.

12. The vortex generating device according to claim 1 , wherein the obtuse angle between the each of the at least two trailing segments is at least 93 degrees or larger.

13. A sequential combustion system, comprising:

an upstream combustion stage; and

a downstream combustion stage, wherein the downstream combustion stage is in fluid communication with the upstream combustion stage and configured to receive combustion gases from the upstream combustion stage, wherein at least one vortex generating device according to claim 1 is provided upstream the downstream combustion stage as a fuel discharge device.

14. A gas turbine engine, comprising:

a sequential combustion system according to claim 13 .