JP6126483B2 - Axial water turbine runner blades, axial water turbine runners and axial water turbines - Google Patents

Description

  Embodiments of the present invention relate to an axial flow turbine runner blade, an axial flow turbine runner, and an axial flow turbine.

  Axial flow turbines include Kaplan turbines and valve turbines. For example, in a Kaplan water turbine, water that has flowed into the casing from the upper pond passes through a stay vane and flows into a guide vane having an opening / closing function for adjusting the flow rate. The water flowing out from the guide vane flows into the runner, and rotates the runner around the rotation axis of the water turbine. As a result, power is generated in the generator connected to the runner via the rotation main shaft. Water flowing out of the runner is discharged to the lower pond through the suction pipe.

  The runner includes a runner boss that is rotatable around a rotation axis of the water turbine, and a plurality of runner blades that are arranged at predetermined intervals in the circumferential direction. Of these, each runner blade is rotatable about the blade rotation axis with respect to the runner boss. Thus, the angle of the runner blades is adjusted according to the flow rate of water flowing into the runner to improve the power generation efficiency.

  Here, FIG. 9 shows the runner blade as viewed from the direction of the blade rotation axis. An inner gap is formed between the runner boss and the runner blade 100. By forming this inner gap, the runner blade 100 can be smoothly rotated about the blade rotation axis. A runner collar 101 that supports the runner blade 100 is provided in the runner boss, and the runner collar 101 is connected to the runner blade rotation drive unit via a runner spindle.

  By the way, there is a problem that cavitation 102 is likely to occur in the leakage flow of water passing through the inner gap. That is, since the pressure in the region on the blade negative pressure surface 103 side of the runner blade 100 is lower than the pressure in the region on the blade positive pressure surface 104 side of the runner blade 100, the pressure on the blade positive pressure surface 104 side of the runner blade 100 from the runner inlet. A part of the water flow (main flow) flowing in the downstream direction through the region flows through the inner gap to the region on the blade negative pressure surface 103 side and leaks. As a result, cavitation 102 can occur when the leakage flow reaches the region on the blade suction surface 103 side where the pressure is low. In particular, the cavitation 102 is likely to occur when the leakage flow through the inner gap upstream of the runner collar 101 flows around the runner collar 101 in the region on the blade negative pressure surface 103 side. The generated cavitation 102 propagates downstream, and cavitation erosion may occur in a portion of the blade suction surface 103 of the runner blade 100 on the downstream side of the runner collar 101.

  An axial water turbine runner for suppressing the occurrence of such cavitation is known from Patent Documents 1 to 6, for example. In the axial-flow turbine runner shown in these documents, a protruding portion that protrudes from the runner blade toward the runner boss is provided in the inner gap. Accordingly, the water in the region on the blade pressure surface side of the runner blade is prevented from flowing through the inner gap to the region on the blade suction surface side and leaking.

US Pat. No. 5,954,474 US Pat. No. 6,254,339 US Pat. No. 6,533,536 US Pat. No. 5,947,679 US Pat. No. 6,164,907 US Pat. No. 6,402,477

  However, in the axial-flow water turbine shown in Patent Documents 1 to 6, the above-described protrusion is in contact with the runner boss. Thus, when the runner blades are rotated, the rotation of the runner blades can be difficult due to the friction generated between the protrusion and the runner boss.

  The present invention has been made in consideration of such points, and an axial flow turbine runner blade, an axial flow turbine runner, and an axial flow turbine capable of suppressing the occurrence of cavitation and smoothly rotating the runner blade. The purpose is to provide.

  The axial-flow water turbine runner blade according to the embodiment is rotatable with respect to a runner boss connected to the rotation main shaft. The axial-flow turbine runner blade is disposed on the runner boss through a gap, and has a blade body having a blade pressure surface and a blade suction surface, a stem extending from the runner boss to the blade body, and supporting the blade body. A projecting portion provided on the runner boss side on the blade suction surface and projecting from the blade suction surface. The blade body is arranged between the upstream region, the downstream region, and the upstream region and the downstream region when viewed from the direction of the rotation axis of the runner blade, and the blade body and the stem are connected to each other. And a region. The protrusion extends from the upstream region of the blade body to the connection region on the blade suction surface of the blade body.

  The axial water turbine runner according to the embodiment includes a runner boss and the above-described axial water turbine runner blades.

  The axial water turbine according to the embodiment includes the above-described axial water turbine runner.

FIG. 1 is a diagram illustrating a configuration of an axial-flow water turbine according to the first embodiment. FIG. 2 is a diagram showing runner blades in the axial-flow turbine of FIG. FIG. 3 is a view of the runner blade of FIG. 2 as viewed from the direction of the blade rotation axis. FIG. 4 is a view corresponding to a cross section taken along line AA of FIG. FIG. 5 is a view corresponding to a cross section taken along line B-B in FIG. 2. FIG. 6 is a diagram showing an outline of pressure distribution in a region on the blade suction surface side when a runner blade without fins is viewed from the direction of the blade rotation axis. FIG. 7 is a view showing a modification of the runner blade of FIG. FIG. 8 is a view showing another modification of the runner blade of FIG. FIG. 9 is a view of a conventional runner blade as viewed from the direction of the blade rotation axis.

  An axial flow turbine runner blade, an axial flow turbine runner, and an axial flow turbine according to an embodiment of the present invention will be described with reference to the drawings.

  First, the axial flow turbine will be described. Here, a Kaplan turbine will be described as an example of an axial flow turbine.

  As shown in FIG. 1, a Kaplan turbine 1 is provided with a casing 2 into which water flows from an upper pond (not shown), and is rotatable with respect to the casing 2, and flows from the casing 2 through a stay vane 3 and a guide vane 4. An axial-flow turbine runner (hereinafter simply referred to as “runner”) 10 that is rotationally driven by water is provided.

  The stay vane 3 is for forming a flow path from the casing 2 to the runner 10, and is disposed on the inner peripheral side from the casing 2. The guide vane 4 is for adjusting the flow rate of water flowing into the runner 10, and is arranged on the inner peripheral side from the stay vane 3. By changing the opening of the guide vane 4, the amount of water flowing from the casing 2 into the runner 10 is adjusted to change the amount of power generation.

  The runner 10 is disposed on the inner peripheral side and below the guide vane 4. The main flow direction of the flowing water flowing in from the casing 2 is directed substantially in the radial direction in the stay vane 3 and the guide vane 4, but in the runner 10 is directed in the direction of the water turbine rotation axis X (vertical direction). The runner 10 is surrounded by a discharge ring 7 provided on the outer peripheral side thereof.

  A generator 8 is connected to the runner 10 via a rotary main shaft 6. When the runner 10 is rotationally driven by the inflowing water, the generator 8 generates power.

  A suction pipe 9 is provided on the downstream side of the runner 10. The suction pipe 9 is connected to a lower pond (not shown), and water in which the runner 10 is driven to rotate is discharged to the lower pond.

  Next, the runner 10 according to the present embodiment will be described.

  As shown in FIGS. 1 and 2, the runner 10 includes a runner boss 11 that is rotatable about a turbine rotation axis X and a plurality of axial water turbines that are rotatable about a blade rotation axis Y with respect to the runner boss 11. Runner blades (hereinafter simply referred to as runner blades) 20. Among these, the runner blades 20 are arranged at predetermined intervals in the circumferential direction, and the angle of the runner blades 20 is adjusted according to the flow rate of water flowing into the runner 10 by rotating each runner blade 20. Improvement of power generation efficiency has been attempted. The runner boss 11 is connected to the rotary main shaft 6 described above, and the rotation of the runner boss 11 is transmitted to the generator 8 via the rotary main shaft 6.

  Next, the runner blade 20 according to the present embodiment will be described.

  As shown in FIGS. 2 to 4, the runner blade 20 includes a blade body 21 including a blade positive pressure surface 22 and a blade negative pressure surface 23, and a runner that extends from the inside of the runner boss 11 to the blade body 21 and supports the blade body 21. And a collar 24 (stem). Among these, the blade body 21 is provided on the outer peripheral side of the runner boss 11 and on the inner peripheral side of the discharge ring 7. That is, the blade body 21 is disposed between the runner boss 11 and the discharge ring 7.

  As shown in FIG. 2, the blade body 21 is disposed on the outer peripheral surface of the runner boss 11 via an inner gap 40. In other words, the inner gap 40 is formed between the blade body 21 and the runner boss 11. Further, an outer gap 41 is formed between the blade body 21 and the spherical surface portion 7 a of the discharge ring 7. Thus, the runner blade 20 can be smoothly rotated with respect to the runner boss 11.

  The blade pressure surface 22 (or blade pressure surface) of the blade body 21 is a surface that receives the pressure of the main flow that has flowed into the runner 10, and in the region 50 on the blade pressure surface 22 side, the pressure of running water is high. . The blade negative pressure surface 23 is a surface located on the opposite side of the blade positive pressure surface 22, and in the region 51 on the blade negative pressure surface 23 side, the pressure of running water is low.

  As shown in FIG. 4, the runner collar 24 is connected to a runner blade rotation drive unit (for example, servo motor) 25 via a runner spindle 26. Thus, by driving the runner blade rotation drive unit 25, the blade body 21 is rotated through the runner spindle 26 and the runner collar 24, and the angle of the blade body 21 is adjusted. Yes.

  The runner collar 24 is a disc-shaped collar body portion 24 a disposed inside the runner boss 11, a collar connection portion 24 b provided on the outer peripheral side of the runner boss 11, and connecting the collar body portion 24 a and the blade body 21; have. Of these, the collar connecting portion 24b is formed in a conical shape so as to connect the collar body portion 24a and the blade body 21 in a smooth shape. The strength of the runner blade 20 is improved by forming the collar connecting portion 24b in a conical shape.

  As shown in FIG. 3, the blade main body 21 is viewed from the upstream region 21 a disposed on the upstream side, the downstream region 21 b disposed on the downstream side, and the direction of the blade rotation axis Y of the runner blade 20. And a connecting region 21c that is disposed between the upstream region 21a and the downstream region 21b and to which the blade body 21 and the collar connecting portion 24b of the runner collar 24 are connected. More specifically, the connection region 21c can be said to be a region where the end edge 21d of the blade body 21 on the runner boss 11 side is connected to the collar connection portion 24b.

  As shown in FIGS. 3 and 4, fins 30 (protruding portions) are provided on the runner boss 11 side on the blade negative pressure surface 23 of the blade body 21. More specifically, the fin 30 is disposed at the end of the runner blade 20 on the runner boss 11 side, protrudes from the blade negative pressure surface 23, and extends along the outer peripheral surface of the runner boss 11. In this manner, the fin 30 guides the leakage flow of water that has passed through the inner gap 40 in a direction away from the blade negative pressure surface 23 of the blade body 21. The cross section of the fin 30 along the main flow direction (the cross section viewed from the direction perpendicular to the paper surface of FIG. 2) can guide the leakage flow through the inner gap 40 in a direction away from the blade negative pressure surface 23 of the blade body 21. If there is, there is no particular limitation.

  As shown in FIG. 3, the fin 30 extends from the upstream region 21 a of the blade body 21 to the downstream region 21 b through the connection region 21 c on the blade negative pressure surface 23 of the blade body 21. In the present embodiment, the fin 30 does not extend over the entire length of the blade body 21 of the runner blade 20, and the upstream end 30 a of the fin 30 is downstream of the upstream end 21 e of the blade body 21. And the downstream end 30b of the fin 30 is positioned upstream of the downstream end 21f of the blade body 21.

  It is preferable that the surface of the fin 30 on the runner boss 11 side is disposed closer to the runner boss 11 than the end edge 21 d of the blade body 21 on the runner boss 11 side. More specifically, as shown in FIGS. 4 and 5, the distance L <b> 1 (see FIG. 4) between the runner boss 11 side surface of the fin 30 and the outer peripheral surface of the runner boss 11 is the runner boss 11 of the blade body 21. It is preferable that the distance L0 is smaller than the distance L0 (see FIG. 5) between the edge 21d on the side and the outer peripheral surface of the runner boss 11.

  Next, the operation of the present embodiment having such a configuration will be described.

  When driving in the Kaplan turbine 1 according to the present embodiment, water flows from the upper pond (not shown) into the casing 2 (see FIG. 1). The water flowing into the casing 2 flows into the runner 10 from the casing 2 through the stay vanes 3 and the guide vanes 4. The runner 10 is rotationally driven by the water flowing into the runner 10. As a result, the generator 8 connected to the runner 10 is driven to generate power. The water flowing into the runner 10 is discharged from the runner 10 through the suction pipe 9 to a lower pond (not shown).

  The water that has flowed into the runner 10 flows in a direction (main flow direction) along the blade body 21 of the runner blade 20 (see FIGS. 1 and 2). Here, since the pressure in the region 51 on the blade negative pressure surface 23 side of the blade main body 21 is lower than the pressure in the region 50 on the blade positive pressure surface 22 side of the blade main body 21, from the runner 10 to the blade positive pressure surface 22 side. A part of the water flow (main flow) flowing in the downstream direction through the region 50 of this is leaked from the inner gap 40 formed between the runner boss 11 and the blade body 21, and is a region on the blade negative pressure surface 23 side. It flows to 51 and leaks (refer arrow P of Drawing 3 and 4). Accordingly, when the fin 30 described above is not provided, the leakage flow through the inner gap 40 is directed to the blade negative pressure surface 23 where the pressure is low, and cavitation may occur in the vicinity of the blade negative pressure surface 23. . In particular, as shown in FIG. 6, when the fin 30 is not provided, in the region 51 on the blade negative pressure surface 23 side, the region in the vicinity of the collar connecting portion 24 b of the runner collar 24 tends to have a low pressure. is there. For this reason, when the leakage flow that has passed through the inner gap 40 reaches a region in the vicinity of the collar connecting portion 24b, there is a high possibility that cavitation will occur.

  On the other hand, in the present embodiment, fins 30 that protrude from the blade negative pressure surface 23 are provided on the runner boss 11 side of the blade negative pressure surface 23 of the blade main body 21. The fin 30 guides the leakage flow through the inner gap 40 in a direction away from the blade suction surface 23 (see arrow Q in FIGS. 3 and 4), and suppresses the leakage flow toward the blade suction surface 23. Is done. As a result, the occurrence of cavitation in the vicinity of the blade suction surface 23 can be suppressed.

  As described above, according to the present embodiment, the fin 30 protruding from the blade negative pressure surface 23 is provided on the side of the runner boss 11 on the blade negative pressure surface 23 of the blade main body 21. As a result, the water leakage flow through the inner gap 40 formed between the blade body 21 and the runner boss 11 is kept away from the blade suction surface 23 from the region 50 on the blade pressure surface 22 side of the blade body 21. You can guide in the direction. For this reason, it is possible to suppress the leakage flow that has passed through the inner gap 40 from moving toward the blade suction surface 23, and to suppress the occurrence of cavitation in the vicinity of the blade suction surface 23. Further, since the inner gap 40 is formed between the blade body 21 and the runner boss 11, the runner blade 20 can be smoothly rotated with respect to the runner boss 11. As a result, the runner blade 20, the runner 10, and the Kaplan turbine 1 that can suppress the occurrence of cavitation and can smoothly rotate the runner blade 20 can be obtained.

  Further, according to the present embodiment, the fin 30 extends from the upstream region 21a of the blade body 21 to the downstream region 21b through the connection region. Thereby, it is possible to further suppress the leakage flow through the inner gap 40 from moving toward the region around the collar connecting portion 24b of the runner collar 24 in the region 51 on the blade suction surface 23 side of the blade body 21. . For this reason, it is possible to further suppress the occurrence of cavitation in the vicinity of the blade suction surface 23.

  Moreover, in this Embodiment, when the surface by the side of the runner boss 11 of the fin 30 is arrange | positioned from the edge 21d by the side of the runner boss 11 of the blade | wing main body 21 at the runner boss 11 side, the distance of the fin 30 and the runner boss 11 The pressure of the leakage flow that flows between the fin 30 and the runner boss 11 can be increased. Thereby, the pressure in the exit area | region of the fin 30 can be raised, and it can suppress that cavitation generate | occur | produces.

  In the above-described embodiment, the example in which the fin 30 extends from the upstream region 21a of the blade body 21 to the downstream region 21b through the connection region 21c has been described. However, the present invention is not limited to this. For example, as shown in FIG. 7, the fin 30 extends from the upstream region 21a of the blade body 21 to the connection region 21c and terminates at the connection region 21c. Also good. That is, the upstream end 30a of the fin 30 may be disposed in the upstream region 21a, and the downstream end 30b of the fin 30 may be disposed in the connection region 21c. Even in this case, it is possible to suppress the leakage flow that has passed through the inner gap 40 from going to the region around the runner collar 24 in the region 51 on the blade negative pressure surface 23 side of the blade body 21. Further, since the downstream end 30b of the fin 30 is disposed in the connection region 21c, the length in the main flow direction of the fin 30 can be shortened, and the friction loss in the region 51 on the blade negative pressure surface 23 side can be suppressed. .

  In the present embodiment described above, as shown in FIG. 8, the cross section along the main flow direction of the fin 30 (the cross section viewed from the direction perpendicular to the plane of FIG. 8) has an airfoil shape, The 30 runner boss 11 side surface may be a fin positive pressure surface (projecting portion positive pressure surface) 31, and the discharge ring 7 side surface may be a fin negative pressure surface (projecting portion negative pressure surface) 32. Thereby, the pressure of the leakage flow flowing between the surface of the fin 30 on the runner boss 11 side and the outer peripheral surface of the runner boss 11 can be increased. For this reason, the pressure in the exit area | region of the fin 30 can be raised, and it can suppress that cavitation generate | occur | produces.

  As mentioned above, although embodiment of this invention has been described in detail, the axial-flow turbine runner blade, the axial-flow turbine runner, and the axial-flow turbine according to the present invention are not limited to the above-described embodiments. Various modifications can be made without departing from the spirit of the invention. In the above-described embodiment, the example in which the axial flow turbine runner blade, the axial flow turbine runner, and the axial flow turbine according to the present invention are applied to the Kaplan turbine is described. However, the present invention is not limited to this, and other than the Kaplan turbine. The axial-flow turbine runner blade, the axial-flow turbine runner, and the axial-flow turbine according to the present invention can also be applied to the other turbine.

1 Kaplan turbine 6 Rotating main shaft 10 Runner 11 Runner boss 20 Runner blade 21 Blade body 21a Upstream region 21b Downstream region 21c Connection region 21d Edge 22 Blade positive pressure surface 23 Blade negative pressure surface 24 Runner collar 30 Fin 30a Upstream end 30b Downstream Side end 31 Fin positive pressure surface 32 Fin negative pressure surface 40 Inner gap

Claims (7)

In the axial-flow water turbine runner blade that is rotatable with respect to the runner boss connected to the rotation main shaft,
A blade body disposed on the runner boss via a gap, and having a blade pressure surface and a blade suction surface;
A stem that extends from the inside of the runner boss to the blade body and supports the blade body;
Provided on the side of the runner boss on the blade suction surface of the blade body, and a protrusion protruding from the blade suction surface,
The blade body is disposed between the upstream region, the downstream region, and the upstream region and the downstream region when viewed from the direction of the rotation axis of the axial flow turbine runner blade, And a connecting region to which the stem is connected,
The protrusion extends from the upstream region of the blade body to the connection region on the blade suction surface of the blade body,
The surface on the side of the Ran'nabosu of protrusions, the more the edge of the side of the Ran'nabosu the blade body, the axis running water wheel runner blades characterized in that it is arranged on the side of the Ran'nabosu. The cross section along the main flow direction of the protrusion has an airfoil shape,
Said side surface of said Ran'nabosu protrusions becomes protrusions pressure side, the side opposite to the side of the Ran'nabosu of the projecting portion, to claim 1, characterized in that has a projecting portion suction surface The axial-flow turbine runner blade described. In the axial-flow water turbine runner blade that is rotatable with respect to the runner boss connected to the rotation main shaft,
A blade body disposed on the runner boss via a gap, and having a blade pressure surface and a blade suction surface;
A stem that extends from the inside of the runner boss to the blade body and supports the blade body;
Provided on the side of the runner boss on the blade suction surface of the blade body, and a protrusion protruding from the blade suction surface,
The blade body is disposed between the upstream region, the downstream region, and the upstream region and the downstream region when viewed from the direction of the rotation axis of the axial flow turbine runner blade, And a connecting region to which the stem is connected,
The protrusion extends from the upstream region of the blade body to the connection region on the blade suction surface of the blade body,
The cross section along the main flow direction of the protrusion has an airfoil shape,
Said side surface of said Ran'nabosu protrusions becomes protrusions positive pressure surface, the opposite surface to the side of the Ran'nabosu of the projecting portion, the shaft running water wheel you characterized in that has a projecting portion suction surface Lanna feathers. The protrusions in the blade suction surface of the blade body, either from the upstream region of the blade body through said connecting region of claims 1 to 3, characterized in that it extends the downstream region axis running water wheel runner blade according to one paragraph or. The axial flow turbine runner blade according to any one of claims 1 to 3 , wherein a downstream end portion of the projecting portion is disposed in the connection region of the blade body. The runner boss,
An axial-flow turbine runner comprising the axial-flow turbine runner blade according to any one of claims 1 to 5.   An axial-flow turbine provided with the axial-flow turbine runner according to claim 6.

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