HYDROTURBINE RUNNER BLADE LOCAL EXTENSION TO AVOID CAVITATION EROSION

Abstract

The invention concerns a hydraulic turbine comprising a runner crown or a hub (1), possibly a band (2), and blades (3) fixed to said crown or hub, or between said band and said crown, and to be actuated in rotation around an axis of rotation, each blade comprising: a leading edge (8) and a trailing edge (10), at least one local extension (20) having a first contact surface fixed to the trailing edge of the blade (2), a second contact surface fixed to either said band (6) or said crown (4) and two lateral sides (24.sub.1, 24.sub.2) joining at a ridge line (22).

Claims

1-16: (canceled)

17. A hydraulic turbine comprising: a runner crown; a runner band; a plurality of blades fixed between the runner crown and the runner band, the blades rotating around an axis of rotation in operation of the hydraulic turbine in water; each of the blades comprising: a leading edge and a trailing edge; at least one local extension having a first contact surface fixed to the trailing edge of the blade, a second contact surface fixed to either the runner band or the runner crown, and two lateral sides joining at a ridge line; and wherein the local extension is deformable with respect to the blade, the runner band, or the runner crown.

18. The hydraulic turbine according to claim 17, wherein each blade comprises two of the local extensions each fixed to the trailing edge of the blade, one of the local extensions fixed to the runner band and the other of the local extensions fixed to the runner crown.

19. The hydraulic turbine according to claim 17, wherein the lateral sides comprise a shape that follows water flow lines along the blade when the hydraulic turbine is operated in water.

20. The hydraulic turbine according to claim 17, wherein the local extension is a 3D printed component.

21. The hydraulic turbine according to claim 17, wherein the local extension is formed from one or a combination of: epoxy resin material, a composite or plastic material, glass fibers or carbon fibers, or carbon fibers mixed with an epoxy resin material.

22. The hydraulic turbine according to claim 17, wherein the local extension comprises a shell and an internal part.

23. The hydraulic turbine according to claim 22, wherein the shell comprises a stratified composite material and the internal part comprises a resin material.

24. The hydraulic turbine according to claim 17, wherein the hydraulic turbine is one of: a Francis turbine, a Kaplan turbine, a diagonal flow type turbine, or a pump-turbine.

25. A method for improving the performance of a hydraulic turbine, wherein the hydraulic turbine includes: a runner crown; a runner band; a plurality of blades fixed between the runner crown and the runner band, each of the blades including a leading edge and a trailing edge; the method comprising fixing at least one local extension to the trailing edge of the blade via a first contact surface and to either the runner crown or the runner band via a second contact surface, the local extension having two lateral sides joining at a ridge line and being deformable with respect to the blade, the runner band, or the runner crown.

26. The method according to claim 25, comprising fixing two of the local extensions to the trailing edge of each blade, wherein one local extension is fixed to the runner band and the other local extension is fixed to the runner crown.

27. The method according to claim 25, comprising providing the lateral sides with a shape that follows water flow lines along the blade when the hydraulic turbine is operated in water.

28. The method according to claim 25, comprising forming the local extension as a 3D printed component.

29. The method according to claim 25, comprising forming the local extension from one or a combination of: epoxy resin material, a composite or plastic material, glass fibers or carbon fibers, or carbon fibers mixed with an epoxy resin material.

30. The method according to claim 25, comprising forming the local extension with a shell and an internal part.

31. The method according to claim 30, wherein the shell is formed from a stratified composite material and the internal part is formed from a resin material.

32. The method according to claim 25, wherein the hydraulic turbine is one of: a Francis turbine, a Kaplan turbine, a diagonal flow type turbine, or a pump-turbine.

Description

BRIEF DESCRIPTION OF THE FIGURES

[0026] FIG. 1 shows a known hydroelectric turbine runner,

[0027] FIGS. 2A-2E are different views of blades and of erosion zones of each blade and/or of the crown or the band;

[0028] FIG. 3 shows an embodiment of a blade local extension according to the invention;

[0029] FIGS. 4A-4B are different views of an embodiment of a local extension blade according to the invention;

[0030] FIGS. 5A-5B are different views of another embodiment of a local extension blade according to the invention;

[0031] FIG. 6 shows a perspective view of the blade of FIGS. 5A and 5B;

[0032] FIGS. 7A-7B are different views of another embodiment of a local extension blade according to the invention;

[0033] FIGS. 8 and 9 are views of examples of asymmetrical local extensions according to the invention;

[0034] FIG. 10 is an example of fluid numerical simulation of von Karman vortices.

DETAILED DISCLOSURE OF EMBODIMENTS

[0035] A first example of a blade local extension 20 according to the invention will be explained in connection with FIGS. 3 and 4A, 4B.

[0036] This local extension has a first contact surface with the blade, delimited by a first line of contact 18.sub.1 with the blade 2, close to its trailing edge 10 and a second contact surface with the runner band 6, and possibly with the band fillet (not shown of this figure), delimited by second line of contact 18.sub.2. Both lines form together a contour or an outline of the local extension.

[0037] Instead of a squared shaped trailing edge whose thickness e (see FIG. 3) is of some milimeters, the local extension has a sharp trailing edge or trailing line 22 in order to avoid or reduce Von Karman vortices that are involved in the cavitation erosion; examples of this erosion are given on FIGS. 2A-2E. The profile of the local extension according to the invention ends with this sharp trailing edge or line 22 having a thickness equal to 0 or comprised between 0 and 2 mm.

[0038] The local extension has two lateral sides 24.sub.1, 24.sub.2, joining at a ridge line 22. These two lateral sides 24.sub.1, 24.sub.2, have a shape which follows the flow lines 28, 29. Each of said lateral sides 24.sub.1, 24.sub.2, extends between a portion of the first line of contact 18.sub.1, a portion of said second line of contact 18.sub.2 and said trailing edge 22. The shape of the local extension, in particular said lateral sides and said ridge line, can be tested or measured and/or calculated in order to avoid or reduce Von Karman vortices.

[0039] Von Karman vortices are generated by a fluid flowing along a profile having a trailing edge. When the fluid leaves said trailing edge, it turns into a wake that organizes itself into a series of vortices. These vortices are organized symmetrically along the profile axis. FIG. 10 is an example of fluid numerical simulation of von Karman vortices 121, 122, 123 etc generated by a flow of fluid around a trailing edge 100 of a piece of material 120.

[0040] In the present application to hydraulic turbines, the inventors have evidenced that the amplitude of the von Karman vortices is linked to the thickness of the trailing edge 10 of the blade and that these vortices are reduced if the thickness of the trailing edge is reduced. Ultimately, if said thickness is smoothly reduced to 0, smoothly enough to avoid flow separation, no vortices appears.

[0041] To test a local blade extension according to the invention an experimental setup can be implemented and computer simulations (Computational fluid dynamics, CFD) can be performed as disclosed for example in P. Ausoni et al. in “Karman vortex shedding in the wake of a 2D hydrofoil: measurement and numerical simulation”, IAHR Int. Meeting of WG on Cavitation and Dynamic Problems in Hydraulic Machinery and Systems, Barcelona, 28-30 Jun. 2006; in particular, flow induced vibrations can be measured with help of an accelerometer and a laser vibrometer. It is thus possible to ensure that the von Karman phenomenon is reduced or has disappeared thanks to a local extension according to the invention. The shape of a local extension according to the invention can be adapted according to the above mentioned tests and simulations in order to reach the desired degree of reduction of von Karman phenomenon.

[0042] In the example of FIGS. 3 and 4A, 4B, but also in the following other examples of a local extension according to the invention, there is a continuity between the hydraulic profile of the blade 2 and that of the local extension: there is no perturbation of a flow 28, 29 flowing along the blade and then along the local extension. As can be understood from FIGS. 3 and 4B, water flows 28 and 29 can flow along the lateral sides 2a, 2b of the blade 2 and then along the lateral sides of the local extension 20 according to the invention without any perturbation.

[0043] The ridge line 22, from its top 22s.sub.1 (against the blade 2) to its bottom 22s.sub.2 (against the band 6) is curved. In some embodiments it has, starting from its top 22s.sub.1, a concave shape and then, a convex shape which terminates at the bottom 22s.sub.2. Alternatively, in this or in other embodiments, it can have, starting from its top 22s.sub.1, a convex shape and then, a concave shape which terminates at the bottom 22s.sub.2. As other possibility, it can have a concave shape from its top 22 s.sub.1 to its bottom 22s.sub.2.

[0044] FIG. 4A is a cross-sectional view of the local extension, along a plane P (see FIG. 3) roughly perpendicular to the surface of the band 6 and parallel to plane defined by the axis Y, Z; FIG. 4B is a cross-sectional view of the local extension, along a plane P′ (see FIG. 3) roughly perpendicular to the surface of the blade, perpendicular to plane P and parallel to plane defined by the axis X, Z. On these figures, reference 22a, resp. 22b, is the intersection of ridge 22 with the corresponding cut plane P, resp. P′.

[0045] FIG. 5A is a cross-sectional view of another local extension, also along a plane P (see FIG. 6) roughly perpendicular to the surface of the band 6 and parallel to plane defined by the axis Y, Z, FIG. 5B being a cross-sectional view of the local extension, along a plane P′ (see FIG. 6) roughly perpendicular to the surface of the blade 2, perpendicular to plane P and parallel to plane defined by the axis X, Z. On these figures, 22a, 22b is the intersection of the ridge with the corresponding cut plane P, P′.

[0046] On each of FIGS. 4A-5B the local extension 20: [0047] has two lateral sides 24.sub.1, 24.sub.2, joining at a ridge line 22; they have a shape which follows the flow lines 28, 29; [0048] has a first contact surface with the blade 2, delimited by a first line of contact 18.sub.1 with the blade, close to its trailing edge 10 and a second contact surface with the runner band, delimited by second line of contact 18.sub.2. Both lines form together a contour or an outline of the local extension.

[0049] FIG. 6 is a perspective view of the local extension 20 (which has cross-sectional views along planes P and P′ illustrated on FIGS. 5A and 5B) after it has been fixed against blade 2 and against a blade to band (or blade to crown) fillet 7 and a band 6 (or a crown).

[0050] FIGS. 7A and 7B are a variant of the embodiment of FIGS. 4A and 4B; the reference numbers on these FIGS. 7A and 7B which are identical to those of FIGS. 4A and 4B designate identical or similar technical elements: a local extension 20 according to the invention can comprise, or can be covered by, an outside shell 26, for example in a stratified composite material, and an internal part 27 which is for example in resin, for example epoxy resin, and which can be fixed to the blade and the band by gluing. Such an outside shell can also be applied to a local extension according to other embodiments (as illustrated on FIGS. 5A and 5B or on FIGS. 6, 8 and 9).

[0051] The local extension illustrated on the FIGS. 3-7B have shapes which are symmetric with respect to a plane S perpendicular to both planes P and P′ (see FIG. 3).

[0052] Alternatively, a local extension 20 according to the invention can also have an asymmetrical shape, as illustrated on FIG. 8 (which is a cross-sectional view along a cut plane P having the same orientation as on FIG. 3).

[0053] Another example of asymmetrical local extension 20 according to the invention is shown on FIG. 9, this extension being located on a blade 2 which has a contour 2.sub.1 and is itself is asymmetrical with respect to a plane S.sub.1.

[0054] A local extension according to the invention is fixed with respect to both the blade and the blade to band (or blade to crown) fillet and/or the band (or the crown). A deformation of the local extension is possible with respect to the blade or the runner band, preferably without applying a significant load to the band and/or to the blade.

[0055] For a runner of 6 m diameter, the local extension 20 has for example the following dimensions: [0056] a width w (measured along axis z, see FIGS. 4A and 5A) between 10 mm (most distant plane from band/crown of device) and 20 cm; [0057] a depth d (measured along axis x, see FIGS. 4B and 5B) between 10 cm and 20 cm; [0058] a height h (measured along axis y, see FIGS. 4A and 5A) between 10 cm and 15 cm.

[0059] For runners with larger or smaller or larger diameters, these ranges can be adapted in a homothetic way.

[0060] A local extension 20 according to the invention can be made in resin, for example epoxy resin or in a composite or plastic material; other possible materials are glass fibers or carbon fibers mixed with an epoxy resin. All these materials allow a deformation of this local extension with respect to both the band and the blade; they also avoid any welding of the local extension on the band or crown and the blade. On FIGS. 3-5B the local extension is represented joined to the blade and the band; however, preferably it is first fabricated and then fixed to the blade 2 and the band 6, for example by gluing. Although no view represents only the local extension without the blade and the band, this application should be understood as covering the local extension before it is assembled with the blade and the band.

[0061] A local extension according to the invention can be pre-shaped to have all the attributes normally achieved after securing it against the blade and the runner band.

[0062] It can be fabricated based on 3D printing technologies or additive techniques. It can then be assembled with the blade and the band and/or the band fillet.

[0063] The above description can be applied to a blade local extension 20 in contact with a crown.

[0064] One or more local extension(s) 20 as described above can be fixed, for example by gluing, to a blade and the crown (or the hub) or the band of an existing turbine runner, for example of the type disclosed above in connection with FIG. 1. This improves the performances of said turbine runner by reducing or eliminating the von Karman vortices and the resulting erosion described above in connection with FIGS. 2A-2E.