NZ627914B - Hydraulic turbine - Google Patents

Abstract

hydraulic turbine 1 comprises a turbine body 2 having a runner configured to be rotated by water flowing therein during hydraulic turbine operation, and a guide vane 5 configured to adjust a flow rate of the water flowing into the runner 8. A running water surface is provided in the turbine body, with the running water surface defining a channel for water, and a coating layer provided on the running water surface. The coating layer is formed by hydrophilic paint. with the running water surface defining a channel for water, and a coating layer provided on the running water surface. The coating layer is formed by hydrophilic paint.

Description

HYDRAULIC TURBINE CROSS REFERENCE TO RELATED APPLICATIONS This application is based upon and claims the benefit of priority from Japanese Patent Application Nos. 70681, 35828 and 2014-137072, filed on August 20, 2013, February 26, 2014 and July 2, 2014, respectively, the entire contents of which are incorporated herein by reference.

FIELD The Embodiments relates to a hydraulic turbine. A pipe is also disclosed.

BACKGROUND In general, hydraulic turbines such as a Francis turbine, a Kaplan turbine or a Bulb e serving as an axial flow turbine or the like are known. Further, as a hydraulic turbine capable of conducting both power generation and pumped storage, a Francis pump hydraulic turbine is known. Here, the s pump hydraulic turbine (hereinafter simply referred to as Francis turbine) will be described by way of example.

[0004] In the Francis turbine, water flows from an upper reservoir into a spiral , and the water flowing into the casing flows into a runner through stay vanes and guide vanes.

The guide vanes are configured to be rotated to change an opening degree, thereby enabling ment of a flow rate of the water g into the runner. The runner is rotated around a hydraulic turbine rotating axis by the water flowing thereinto.

Thereby, power is generated at a generator connected to the runner via a main shaft. The water flowing out of the runner is discharged to a lower reservoir through a draft tube.

In this way, the water from the upper reservoir is discharged to the lower reservoir through the casing, the stay vanes, the guide vanes, the , and the draft tube. In the meantime, the water flows along a running water surface of a channel which is defined by the running water surface of, for instance, the casing. Thereby, a friction loss occurs at a flow of the water along the running water surface. The friction loss is different depending on a flow velocity and a Reynolds number.

In general, the higher the flow velocity, the greater the on loss, whereas the smaller the Reynolds number, the greater the friction loss.

In the Francis turbine, various losses in addition to the friction loss can occur. For example, a secondary flow loss caused by ion of a flow that does not follow a main flow, a separation loss caused by generation of separation from a flow, and a vortex loss caused by a swirl flow generated from a runner outlet in a draft tube are exemplified.

[0007] The secondary flow loss and the separation loss or the like can be reduced by optimizing a shape of each part. r, even in the case of optimizing the shape of each part, the friction loss occurs at a flow of water along a running water surface of each part. For this reason, there is a limitation in reducing the losses of the Francis turbine as a whole by reducing the secondary flow loss and the separation loss or the like. [0007a] It is an object of the invention to at least provide the public with a useful choice.

In one aspect of the invention there is provided a hydraulic turbine comprising: a turbine body having a runner ured to be rotated [Followed by page 2a] by water flowing therein during hydraulic turbine operation, and a guide vane configured to adjust a flow rate of the water flowing into the ; a running water surface provided in the turbine body, the g water e defining a channel for water; and a coating layer provided on the running water surface, the coating layer being formed by hydrophilic paint. [0007c] In a further aspect of the invention there is provided a hydraulic turbine comprising: a casing into which water flows; a runner having a crown, a band, and a ity of runner blades provided between the crown and the band, the runner being configured to be rotated by the water flowing therein from the casing; and an upper cover provided outside the crown of the runner, the upper cover being configured to form a back pressure chamber between the crown and the upper cover, wherein a back pressure chamber coating layer having hydrophilicity is provided on a surface of the crown which is located in the back pressure r. [0007d] In a further aspect of the invention there is provided a lic turbine comprising: a casing into which water flows; a runner having a crown, a band, and a plurality of runner blades ed between the crown and the band, the runner being configured to be rotated by the water flowing therein from the casing; and a lower cover provided outside the band of the , the lower cover being configured to form a lateral pressure chamber between the band and the lower cover, wherein a lateral pressure chamber coating layer having [Followed by page 2b] hydrophilicity is provided on a e of the band which is located in the l pressure chamber.

BRIEF DESCRIPTION OF THE DRAWINGS is a view illustrating an overall configuration of a hydraulic turbine in a first embodiment; is a cross-sectional view illustrating a coating layer provided on a running water surface of the hydraulic turbine of and is a view viewed in a direction of [followed by page 3] [Followed by page 3] arrow P of ; FIGS. 3A to 3C are views illustrating a method of forming the g layer illustrated in FIGS. 2A and 2B; is a view illustrating a function of dimples of the coating layer of FIGS. 2A and 2B; is a view illustrating a cover non-coating region formed on an upper cover and a lower cover in a second embodiment; is a longitudinal section view illustrating a runner in a third embodiment; is a cross-sectional view taken along line A-A which illustrates a runner blade of the runner of is a view illustrating a modification of is a cross-sectional view illustrating a coating layer in a fourth embodiment; is a cross-sectional view illustrating an overall configuration of a hydraulic turbine in a fifth embodiment; is a partially ed cross-sectional view of A is a cross-sectional view illustrating a coating layer in the hydraulic turbine of , and B is a view viewed in a direction of arrow P of A; FIGS. 13A to 13C are views illustrating a method of g the g layer illustrated in FIGS. 12A and 12B; is a view illustrating a function of dimples of the coating layer illustrated in FIGS. 12A and 12B; is a schematic view illustrating a pipe in a sixth embodiment; and is a cross-sectional view rating a coating layer provided on a running water surface of the pipe of FIG.

DETAILED PTION Unless the context y requires otherwise, throughout the description and the claims, the words “comprise”, “comprising”, and the like are to be construed in an inclusive [Followed by page 3a] sense as opposed to an exclusive or exhaustive sense; that is to say, in the sense of "including, but not d to". [0009a] A hydraulic turbine according to an embodiment includes a turbine body, a running water surface provided in the turbine [followed by page 4] [Followed by page 4] body, the running water surface defining a l for water, and a g layer provided on the running water surface, the coating layer being formed by water-repellent paint or hydrophilic paint.

A hydraulic turbine according to an embodiment es a casing into which water flows, and a runner rotated by the water flowing therein from the casing. The runner es a crown, a band, and a plurality of runner blades provided between the crown and the band. An upper cover is provided outside the crown of the runner and forms a back pressure chamber between the crown and the upper cover. A back pressure chamber coating layer having hydrophilicity is provided on a surface of the crown which is d in the back re chamber.

A hydraulic turbine according to an embodiment includes a casing into which water flows, and a runner rotated by the water flowing therein from the casing. The runner includes a crown, a band, and a plurality of runner blades provided between the crown and the band. A lower cover is provided outside the band of the runner and forms a lateral pressure chamber between the band and the lower cover. A lateral pressure chamber coating layer having hydrophilicity is ed in a surface of the band which is located in the lateral pressure chamber.

A pipe according to an embodiment is a pipe connected to a hydraulic turbine. The pipe includes a pipe body, a running water surface that is provided in the pipe body and defines a channel for water, and a coating layer that is ed on the running water surface and has hydrophilicity.

Hereafter, a hydraulic turbine in embodiments will be described with nce to the drawings. Here, a Francis turbine will be described as an example of the hydraulic turbine.

(First embodiment) First, a hydraulic turbine in a first embodiment will be described using FIGS. 1 to 4.

As illustrated in a Francis turbine 1 is equipped with a turbine body 2 and a running water surface 20 (see ) provided in the turbine body 2.

The turbine body 2 has a spiral casing 3 into which water flows from an upper reservoir 201 (see ) h a hydraulic iron pipe 200 during hydraulic turbine operation, a plurality of stay vanes 4, a plurality of guide vanes 5, and a runner 8. Among them, the stay vanes 4 guide the water flowing into the casing 3 to the guide vanes 5 and the runner 8, and are disposed at a given interval in a circumferential direction. A channel 21 in which the water flows is formed n the stay vanes 4. The guide vanes 5 guide the inflow water to the runner 8, and are disposed at a given interval in a circumferential direction. The channel 21 in which the water flows is formed between the guide vanes 5.

Upper and lower covers 6 and 7, which are opposite to each other, are provided at upper and lower sides of the guide vanes 5, respectively. The upper cover 6 and the lower cover 7 bly support the guide vanes 5. The guide vanes 5 are rotated to change an opening angle, and thereby a flow rate of the water flowing into the runner 8 is adapted to be adjustable.

In this way, a capacity of power generation of a tor motor 3O 11 to be described below is adapted to be adjustable.

The runner 8 is configured to be rotatable around an axis X of on with respect to the casing 3, and is rotatably driven by the water flowing from the casing 3 during the hydraulic turbine operation. Further, the runner 8 has a plurality of runner blades 9 ed at a given interval in a circumferential direction, and the channel 21 in which the water flows is formed between the runner blades 9.

The generator motor 11 is connected to the runner 8 via a main shaft 10. The generator motor 11 tes power based on rotation of the runner 8 during the hydraulic turbine operation, and is configured to rotatably drive the runner 8 during pump ion g pumped storage operation). A draft tube 12 for restoring a pressure of the water flow flowing out of the runner 8, as a part of the turbine body 2, is ed at a downstream side of the runner 8 during the hydraulic turbine operation. The draft tube 12 is connected to a lower reservoir 202 (see ), and the water rotatably driving the runner 8 is d to be discharged to the lower reservoir 202.

[0020] The running water e 20 (see ) is provided for each of the casing 3, the stay vanes 4, the guide vanes 5, the upper cover 6, the lower cover 7, the runner 8, and the draft tube 12 of the aforementioned e body 2. Each running water surface 20 is adapted to define the channel 21 for the running water such that the water flows in the channel 21.

As illustrated in , the running water surface 20 is provided with a coating layer 30 formed by repellent paint.

The coating layer 30 can be formed on the running water surface 20 by coating the water—repellent paint. The water—repellent paint is not particularly limited as long as it has water repellency. For example, paint containing fluorine resin or silicon resin, or ship's bottom paint can be used. Further, 3O the water—repellent paint preferably has a contact angle of, for instance, 75 degrees or more, and more preferably 90 degrees or more, (wherein the contact angle is an angle formed between a surface of the coating layer 30 which is a solid surface and a tangent line to an edge of the water being in contact with the solid surface).

The coating layer 30 is ably provided with a plurality of (or multiple) dimples 31 that are open to the channel 21. The dimples 31 are formed in the coating layer 30 in a concave shape like a small pit. Each dimple 31 preferably has a depth that is not less than 0.05 times and not more than 0.15 times a diameter of an inscribed circle of the dimple 31 when a planar shape of the dimple 31 is a polygonal shape, or a diameter of the dimple 31 when a planar shape of the dimple 31 is a circular shape. Here, as the depth of the dimple 31 is set to not less than 0.05 times the diameter, the dimple 31 can be formed with high ion. As the depth of the dimple 31 is set to not more than 0.15 times the diameter, an increase in friction loss caused by the presence itself of the dimple 31 can be suppressed. On the other hand, the planer shape of the dimple 31 is not particularly limited, but it is ably, for instance, a circular shape as illustrated in or a hexagonal shape. For example, if the diameter of the inscribed circle of the polygonal dimple 31 or the diameter (Dd illustrated in ) of the circular dimple 31 is 1 mm, the depth (Hd illustrated in ) of the dimple 31 is preferably not less than 50 pm and not more than 150 pm. A depth of the coating layer 30 is not particularly d if the dimples 31 can be formed, if the running water surface 20 is not exposed to the bottoms of the dimples 31, and if the material of the coating layer 30 can be left behind.

Further, an interval between the dimples 31 adjacent to each other is preferably not less than 0.8 times and not more 3O than 0.12 times the er of the inscribed circle of the dimple 31 when the planar shape of the dimple 31 is the polygonal shape, or the diameter of the dimple 31 when the planar shape of the dimple 31 is the circular shape. Thereby, an effect of reducing viscosity resistance of the water flow according to the dimples 31 can be effectively ed, which is experimentally confirmed by the inventors. For example, if the diameter of the inscribed circle of the polygonal dimple 31 or the er (Dd illustrated in ) of the circular dimple 31 is 1 mm, the interval (G illustrated in ) between the dimples 31 is ably not less than 0.8 mm and not more than 1.2 mm.

As illustrated in FIGS. 3A to 3C, the coating layer 30 can be formed using, for example, a mold 40 having bulges 41 corresponding to the dimples 31 of the coating layer 30. In this case, as illustrated in , the repellent paint is applied to the g water surface 20 in a film shape at a given ess first, and a paint film 30a is formed.

Subsequently, as illustrated in , the mold 40 is pressed against the paint film 30a of the water—repellent paint. In this case, the mold 40 is pressed such that the paint film 30a remains between the bulges 41 of the mold 40 and the running water surface 20. Next, in the state in which the mold 40 is pressed, the paint film 30a is dried and cured. After the paint film 30a is cured, the mold 40 is removed as illustrated in 3C. In this way, the coating layer 30 can be obtained in the present embodiment. The method of forming the coating layer is not limited to the aforementioned method. For example, after the paint film of the water—repellent paint is cured, the mold 40 may be placed on the cured paint film, and the water—repellent paint may be applied to the surroundings of the bulges 41 of the mold 40, and be cured. Thereby, the coating layer 30 can also be ed in the present embodiment.

Such a coating layer 30 is provided on each of the 3O running water surfaces 20 of the casing 3, the stay vane 4, the guide vane 5, the upper cover 6, the lower cover 7, the runner 8, and the draft tube 12. In other words, without other restraints, the coating layer is preferably provided on the running water surface 20 of each member of the Francis turbine 1.

Next, an ion of the t embodiment configured in this way will be described.

When the hydraulic turbine operation is conducted in the Francis turbine according to the present embodiment, as illustrated in water flows from the upper reservoir 201 (see ) into the casing 3 through the hydraulic iron pipe 200. The water flowing into the casing 3 flows from the casing 3 into the runner 8 through the stay vanes 4 and the guide vanes 5. The runner 8 is rotatably driven by the water flowing into the runner 8. Thereby, the generator motor 11 connected to the runner 8 via the main shaft 10 is driven to produce electric power. The water g into the runner 8 is discharged from the runner 8 through the draft tube 12 to the lower reservoir 202. During which the hydraulic turbine operation is ted, the guide vanes 5 are rotated. Thereby, the opening degree of the guide vanes 5 is adjusted, and the capacity of power generation of the generator motor 11 is adjusted.

During pump operation, the generator motor 11 rotatably drives the runner 8, thereby g up the water in the draft tube 12. The water pumped up into the runner 8 flows into the casing 3 h the guide vanes 5 and the stay vanes 4, and is discharged from the casing 3 through the hydraulic iron pipe 200 to the upper reservoir 201. The guide vanes 5 and stay vanes 4 guide the water flowing out of the runner 8 to the casing 3. In this case, the opening degree of the guide vanes 5 is variable to have a proper pumpage depending on a pump head.

During the hydraulic turbine operation and the pump operation, a flow of the water along the running water surface 20 is formed inside the channel 21 defined by the running water surface 20 of the casing 3, the running water surfaces 20 of the stay vanes 4, the running water surfaces 20 of the guide vanes , the running water surface 20 of the upper cover 6, the running water surface 20 of the lower cover 7, the running water surface 20 of the runner 8, and the running water surface of the draft tube 12. The running water surface 20 is provided with the g layer 30 (see ) formed by the water—repellent paint. Thereby, the water flowing near the g layer 30 can flow to be repelled from the coating layer , and the viscosity resistance of the water flow near the g layer 30 can be reduced. For this reason, the friction loss of the main flow against the running water e 20 can be reduced.

Further, as described above, the coating layer 30 is provided with the a plurality of dimples 31. While entering or leaving the dimples 31, part of the water is affected by a flow in a water flow direction, and flows to circulate in the s 31 as rated in In this case, the water in the dimples 31 can flow to be repelled from walls of the dimples 31 formed by the water—repellent paint, and smoothly circulate in the s 31. For this reason, the water flow circulating in the dimples 31 exerts the same function as a roller used in a common conveyer or the like, still more reduces the viscosity resistance of the flow of the water flowing above the dimples 31, and allows the main flow to flow smoothly on the running water surface 20.

Incidentally, in head energy Ph of the water flowing into the Francis turbine 1, assuming that a y of the water be p, 3O a flow rate be Q, a head be H, and gravitational acceleration be g, the head energy Ph is expressed as follows.

Ph = p x g x Q X H Assuming the friction loss of the water occurring on the running water surface 20 be Lf, Lf of the head energy Ph is used as friction energy. Further, if the loss caused by the shape of the hydraulic turbine, such as the secondary flow loss, the separation loss, or the vortex loss described above, is defined as Ls, energy Pt that can be used to rotate the runner 8 is as follows.

Pt = Ph - Lf - Ls However, as described above, as the running water surface 20 is provided with the coating layer 30 formed by the water-repellent paint, the viscosity resistance of the water flow near the coating layer 30 can be reduced. For this reason, it is le to reduce the friction loss Lf, and increase the energy Pt that can be used to rotate the runner 8.

According to the present embodiment, the running water surface 20 is provided with the coating layer 30 formed by the repellent paint. Thereby, it is possible to reduce the viscosity resistance of the water flow in the vicinity of the g layer 30, and to reduce the friction loss of the water flow flowing in the channel 21 defined by the running water surfaces 20. For this reason, it is possible to make good use of energy of the water flowing into the casing 3 to improve efficiency of the hydraulic e.

Further, according to the t embodiment, the coating layer 30 is provided with the a plurality of dimples 31.

Thereby, it is possible to more reduce the viscosity resistance of the water flow in the vicinity of the coating layer 30, and to more reduce the friction loss of the water flow. 3O (Second embodiment) Next, a lic e in a second embodiment will be described using In the second embodiment illustrated in a main difference is that a non—coating region is provided for an upper cover and a lower cover, and other configurations are imately identical to those of the first embodiment illustrated in FIGS. 1 to 4. In the same parts as in the first embodiment rated in FIGS. 1 to 4 are given the same symbols, and detailed description thereof will be omitted.

As illustrated in a running water surface 20 of an upper cover 6 has a coating region 50 in which a coating layer is provided, and a cover non—coating region 51 in which no coating layer 30 is provided. In the cover non—coating region 51 of these regions, the running water surface 20 of the upper cover 6 is exposed. When viewed in a direction taken along a onal axis Y (see of a guide vane 5 (in the state of , the cover non—coating region 51 is formed to include (or cover) a rotation region of the guide vane 5. In the present ment, the cover non—coating region 51 is formed around the rotational axis of the guide vane 5 in a circular shape.

Preferably, a radius of the cover non-coating region 51 is approximately equal to the maximum rotation radius of the guide vane 5 or is greater than the maximum rotation radius.

In this way, when viewed in the ion taken along the rotational axis, the rotation region of the guide vane 5 is adapted to avoid overlapping the coating region 50.

Like the upper cover 6, the lower cover 7 also has a coating region 50 and a cover non-coating region 51. When viewed in the direction taken along the rotational axis of the guide vane 5, the cover non—coating region 51 is formed to include the rotation region of the guide vane 5. 3O Thus, according to the present embodiment, the cover ating region 51 of the upper cover 6 and the cover non—coating region 51 of the lower cover 7 are formed to include the rotation region of the guide vane 5 when viewed in the direction taken along the rotational axis of the guide vane 5.

Thereby, it is possible to prevent the rotating guide vane 5 from coming into contact with the coating layer 30, and to thus prevent the coating layer 30 from being separated. Further, in the cover non—coating region 51, since the coating layer 30 does not intervene between the guide vane 5 and the upper cover 6 and between the guide vane 5 and the lower cover 7, a gap between the guide vane 5 and the upper cover 6 and a gap between the guide vane 5 and the lower cover 7 can be ted from being reduced. Thereby, it is possible to prevent sand or foreign substances such as dust from being put in these gaps, and to thus t the coating layer 30 from being scratched or separated. For this reason, the coating layer 30 is prevented from being damaged, and the coating layer 30 is prolonged in service life, so that it is possible to enjoy an effect of reducing the friction loss based on the coating layer 30 for a long time.

[0041] (Third ment) Next, a hydraulic turbine in a third embodiment will be described using FIGS. 6 and 7.

In the third embodiment illustrated in FIGS. 6 and 7, a main difference is that a non—coating region is provided for each runner blade of a runner, and other urations are imately identical to those of the first ment illustrated in FIGS. 1 to 4. In FIGS. 6 and 7, the same parts as in the first embodiment illustrated in FIGS. 1 to 4 are given the same symbols, and detailed description thereof will be omitted.

As illustrated in FIGS. 6 and 7, a running water surface of each runner blade 9 of a runner 8 has a pressure surface (driving face) 9a and a suction surface 9b. r, the running water surface 20 of the runner blade 9 has a coating region 50 for which a coating layer 30 is provided, and an upstream non-coating region 52 in which the coating layer 30 is not provided. The am non-coating region 52 is formed at an upstream end (an inlet-side end or a guide vane—side end) of each of the pressure and suction surfaces 9a and 9b of the runner blade 9 during hydraulic turbine operation.

The upstream non-coating region 52 has a length that follows a main flow direction and is indicated in by Li, and is formed to extend from a crown 8a toward a band 8b.

When an outlet diameter (a diameter of a draft ide end) of the runner 8 during the hydraulic turbine operation is defined as De, the length Li of the upstream non—coating region 52 in the main flow direction is preferably given as follows.

Li/De s 0.8 The length Li defined in the expression above becomes a region in which flow separation 55 may generally occur during the hydraulic turbine operation. This prevents the coating layer from being provided in the region in which the flow separation 55 may occur.

In other words, when a water flow direction of the water g into the runner 8 during the hydraulic turbine operation is not matched with the runner blade 9, flow separation 55 can occur at the pressure e 9a or the n surface 9b at an upstream end of the runner blade 9 as illustrated in However, as described above, the am non—coating region 52 is formed on the pressure surface 9a and the suction surface 9b at the upstream end of the runner blade 9. This can prevent the coating layer 30 from being provided in the region in which the flow tion 55 can occur during the hydraulic turbine operation.

Further, as illustrated in FIGS. 6 and 7, the running water 3O surface 20 of the runner blade 9 further includes a downstream ating region 53 in which the coating layer 30 is not provided. The downstream non—coating region 53 is formed at a downstream end (an outlet-side end or a draft tube-side end) of the suction surface 9b of the runner blade 9 during the lic turbine operation.

The downstream ating region 53 has a length that follows the main flow direction and is indicated in by Lo, and is formed to extend from the crown 8a toward the band 8b.

When the outlet diameter (the diameter of the draft tube—side end) of the runner 8 during the hydraulic turbine operation is d as De, the length Lo of the downstream non—coating region 53 in the main flow direction is preferably given as follows.

Lo/De s 0.8 The length Lo d in the expression above becomes a region in which cavitation 56 can generally occur during the hydraulic turbine operation. This prevents the coating layer 30 from being provided in the region in which the cavitation 56 can occun In other words, when a flow rate of the water flowing into the runner 8 is more than a design point (or when output is high), the cavitation 56 can occur in the ty of the suction surface 9b at a downstream end of the runner blade 9 as illustrated in However, as described above, downstream non—coating region 53 is formed on the suction surface 9b at the downstream end of the runner blade 9. This can prevent the coating layer 30 from being provided in the region in which the tion 56 can occur during the hydraulic turbine ion.

Thus, according to the present embodiment, the upstream non—coating region 52 is formed at the upstream end of each of the pressure and suction surfaces 9a and 9b of the 3O runner blade 9 during the hydraulic turbine operation. This can prevent the g layer 30 from being provided in the region in which the flow separation 55 can occur. Further, the downstream non-coating region 53 is formed at the downstream end of the suction surface 9b of the runner blade 9 during the hydraulic turbine operation. This can prevent the coating layer from being provided in the region in which the cavitation 56 can occur. For this reason, the coating layer 30 is prevented from being damaged by the flow separation 55 and/or the cavitation 56, and the coating layer 30 is prolonged in service life, so that it is le to enjoy the effect of reducing the friction loss based on the coating layer 30 for a long time.

In the aforementioned present embodiment, as illustrated in the downstream non—coating region 53 may be formed also at a downstream end (an outlet-side end or a draft tube—side end) of the re surface 9a of the runner blade 9.

In other words, the downstream non—coating region 53 may be formed on both the pressure surface 9a and the suction surface 9b at the downstream end of the runner blade 9 during the hydraulic turbine operation.

[0051] Since the water flows from the draft tube 12 toward the casing 3 during the pump operation in a direction opposite to that during the hydraulic e operation, when the water flow direction of the water flowing into the runner 8 is not matched with the shape of the runner blade 9, the flow separation 55 can occur on the pressure surface 9a or the suction surface 9b at the draft tube—side end (the side end during the pump operation or the downstream end during the hydraulic turbine operation) of the runner blade 9. However, as described above, when the ream non-coating region 53 is formed at the draft ide ends of the pressure and suction surfaces 9a and 9b of the runner blade 9 during the hydraulic turbine operation, it is possible to prevent the coating layer 30 from being provided in the region in which the flow separation 55 may occur. 3O Thereby, even in the case of conducting the pump operation of the Francis turbine 1, it is possible to prevent the coating layer from being damaged. In other words, when the pump ion of the Francis turbine 1 is led, the downstream non—coating region 53 is preferably formed on both the pressure surface 9a and the suction surface 9b at the downstream end of the runner blade 9 during the hydraulic e operation.

(Fourth embodiment) Next, a hydraulic turbine in a fourth embodiment will be described using In the fourth embodiment illustrated in a main difference is that a coating layer is formed by hydrophilic paint, and other configurations are approximately identical to those of the first embodiment illustrated in FIGS. 1 to 4. In the same parts as in the first embodiment illustrated in FIGS. 1 to 4 are given the same symbols, and detailed description thereof will be omitted.

As illustrated in a running water surface 20 is provided with a coating layer 60 formed by hydrophilic paint.

The coating layer 60 can be formed on the running water surface 20 by coating the hydrophilic paint. The hilic paint is not particularly limited as long as it has hydrophilicity.

For example, paint containing a material having a hydrophilic group (-OH) may be properly used. Further, a t angle of the hydrophilic paint is preferably equal to or less than, for instance, 40 degrees.

Similarly to the coating layer 30 and the dimples 31 illustrated in FIGS. 2A and 28, the g layer 60 is ably provided with a plurality of (or multiple) s 61 open to the channel 21. Each dimple 61 preferably has a depth that is not less than 0.05 times and not more than 0.15 times a diameter of an inscribed circle of the dimple 61 when a planar shape of 3O the dimple 61 is a nal shape, or a diameter of the dimple 61 when a planar shape of the dimple 61 is a ar shape.

On the other hand, the planar shape of the dimple 61 is not particularly limited, but it is preferably a circular shape or a hexagonal shape. For example, if a diameter of an inscribed circle of the polygonal dimple 61 or a diameter (for example, Dd illustrated in of the circular dimple 61 is 1 mm, the depth (for example, Hd illustrated in of the dimple 61 is preferably not less than 50 pm and not more than 150 pm.

Further, an interval n the dimples 61 adjacent to each other is preferably not less than 0.8 times and not more than 0.12 times the diameter of the inscribed circle of the dimple 61 when the planar shape of the dimple 61 is the polygonal shape, or the diameter of the dimple 61 when the planar shape of the dimple 61 is the ar shape. Thereby, an effect of reducing viscosity resistance of the water flow according to the s 61 can be effectively produced, which is experimentally confirmed by the inventors. For example, if the diameter of the inscribed circle of the polygonal dimple 61 or the diameter (Dd illustrated in of the circular dimple 61 is 1 mm, the interval (G illustrated in between the dimples 61 is preferably not less than 0.8 mm and not more than 1.2 mm.

Further, the coating layer 60 illustrated in can be formed to be r to the coating layer 30 rated in , and is preferably formed on the running water surface 20 provided for each member, such as the casing 3.

During the hydraulic turbine operation and the pump ion, a flow of the water along the running water surface is formed inside the channel 21 defined by the g water surface 20 of the casing 3 etc. The g water surface 20 is provided with the coating layer 60 formed by the hydrophilic paint. Thereby, a thin water adhesion layer 62 is formed on a 3O surface 60a of the coating layer 60 in such a manner that water is adhered. The water adhesion layer 62 is interposed between the main flow and the coating layer 60. Further, the water forming the water adhesion layer 62 is not at a standstill with respect to the coating layer 60, but it has an extremely low flow velocity. With the above configuration, it is possible to reduce the viscosity resistance of the water flow in the proximity of the coating layer 60 and to reduce the friction loss of the main flow against the running water surface 20.

Further, the coating layer 60 is provided with the a plurality of dimples 61. In this case, the water in the dimples 61 is adapted to be adhered to walls of the dimples 61 formed by the hydrophilic paint, and thus a flow velocity of the water in the dimples 61 is extremely reduced. Thereby, an effect of increasing a thickness of the water adhesion layer 62 described above is obtained in a region in which the dimples 61 are provided within the running water surface 20. For this reason, the viscosity resistance of the water flow flowing above the dimples 61 can be more reduced, and the main flow can smoothly flow on the running water surface 20.

[0060] Thus, according to the t embodiment, the running water surface 20 is ed with the g layer 60 formed by the hilic paint. Thereby, it is possible to form the adhesion layer 62 of the water having an ely low flow ty on the surface 60a of the coating layer 60, and to reduce the friction loss of the water flow flowing in the l 21 defined by the running water surface 20. For this reason, it is possible to improve the efficiency of the hydraulic turbine by making good use of energy of the water flowing into the casing 3.

Further, according to the present embodiment, the coating layer 60 is provided with the a plurality of dimples 61.

Thereby, it is possible to more reduce the viscosity resistance of 3O the water flow in the proximity of the coating layer 60, and to more reduce the friction loss of the water flow.

(Fifth embodiment) Next, a hydraulic turbine in a fifth embodiment will be described using FIGS. 10 to 14.

In the fifth embodiment illustrated in FIGS. 10 to 14, a main difference is that a back pressure chamber coating layer having hydrophilicity is provided on a surface of a crown which is located in a back pressure chamber, and a l pressure chamber coating layer having hydrophilicity is provided on a surface of a band which is located in a lateral pressure chamber, and other configurations are approximately identical to those of the first embodiment illustrated in FIGS. 1 to 4. In FIGS. 10 to 14, the same parts as in the first embodiment illustrated in FIGS. 1 to 4 are given the same symbols, and detailed description thereof will be omitted.

Here, as an e of the hydraulic turbine, a Francis turbine will be described by way of example.

As rated in , a Francis turbine 101 is equipped with a spiral casing 103 into which water flows from an upper reservoir 201 (see ) through a hydraulic iron pipe 200, a plurality of stay vanes 104, a ity of guide vanes 105, and a runner 106. Among them, the stay vanes 104 are to guide the water flowing into the casing 103 to the guide vanes 105 and the runner 106, and are disposed at a given interval in a circumferential direction.

[0066] The guide vanes 105 are to guide the inflow water to the runner 106, and are disposed at a given interval in a circumferential direction. Further, each guide vane 105 is rotatably provided, and is configured to allow a flow rate of the 3O water flowing into the runner 106 to be adjusted by rotation and the resultant ion in opening . Thereby, a capacity of power generation of a generator 111 to be described below can be adjusted.

The runner 106 is configured to be ble around a rotational axis X relative to the casing 103, and is rotatably driven by the water flowing therein from the casing 103.

Further, as illustrated in , the runner 106 has a crown 107, a band 108, and a ity of runner blades 109 provided between the crown 107 and the band 108. Among them, the runner blades 109 are disposed at a given interval in a circumferential ion.

As illustrated in , the generator 111 is connected to the runner 106 via a main shaft 110. The generator 111 is configured to generate power by rotation of the runner 106. A draft tube 112 for restoring a pressure of the water flow flowing out of the runner 106 is provided at a downstream side of the runner 106. The draft tube 112 is connected to a lower reservoir 202. The water rotatably g the runner 106 is adapted to be rged to the lower reservoir 202.

As illustrated in , a back pressure chamber 113 is formed outside (an upper side in ) the crown 107 of the runner 106. To be more specific, an upper cover 114 is provided outside the crown 107, and the aforementioned back re chamber 113 is formed between the crown 107 and the upper cover 114. On the other hand, a lateral pressure chamber 115 is formed outside (a right side in or a radial outer side) the band 108 of the runner 106. More particularly, a lower cover 116 is provided outside the band 108, and the aforementioned lateral pressure chamber 115 is formed between the band 108 and the lower cover 116.

Part of the water flowing through the guide vanes 105 3O flows into the back pressure and lateral pressure chambers 113 and 115 as a e flow. In other words, a back pressure chamber-side gap portion 117 is provided at a radial outer side (upstream side) of the crown 107. Water flows into the back pressure chamber 113 through the back pressure chamber—side gap portion 117. When a h-hole 118 is provided in the crown 107 of the runner 106 as illustrated in , the running water in the back pressure chamber 113 flows into the draft tube 112 through the h—hole 118. Further, a back pressure chamber-side seal portion (intermediate seal portion) 119 is provided at a radial inner side of the back pressure chamber 113 (more ularly, between the back pressure chamber 113 and the through-hole 118). The back pressure chamber-side seal portion 119 is formed such that it is difficult for water to flow due to a narrowest gap between the crown 107 that is a rotation—side portion and the upper cover 114 that is a standstill-side. Thereby, an inflow rate of the water from guide vanes 105 toward the back pressure chamber 113 is suppressed.

The back pressure chamber—side seal portion 119 can be formed by a labyrinth seal.

On the other hand, a lateral re chamber—side gap portion 120 is provided at a radial outer side eam side) of the band 108. Water flows into the lateral pressure r 115 through the lateral pressure chamber-side gap portion 120.

The running water in the lateral pressure chamber 115 flows into the draft tube 112 h a downstream gap portion 121 provided at a radial inner side (downstream side) of the band 108. Further, a lateral pressure chamber—side seal portion 122 is provided at a radial inner side of the lateral pressure chamber 115 (more particularly, between the lateral re chamber 115 and the ream gap portion 121). The lateral pressure chamber—side seal portion 122 is formed such that it is difficult for water to flow due to a narrowest gap between the band 108 that is a rotation—side portion and the lower cover 116 that is a standstill-side. Thereby, an inflow rate of the water from guide vanes 105 toward the lateral pressure chamber 115 is suppressed. The lateral pressure chamber-side seal portion 122 can be formed by a nth seal.

As bed above, since the back pressure chamber 113 and the lateral pressure chamber 115 form a relatively narrow channel, a disk friction loss can occur while the water flows into the back pressure chanwber 113 and the lateral pressure chamber 115 and the runner 106 is rotated.

GeneraHy,sfince the channeksin the back pressure and lateral pressure chambers 113 and 115 are relatively , velocity gradients of the water flows passing through the back pressure and lateral pressure chan1bers 113 aruj 115 can be complicated from the rotation—side portions (the crown 107 and the band 108) U3the fiandsHH—Qde porfions(the uppercover 114 and the lower cover 116). Thereby, the y resistance can be increased, and the disk friction loss may be sed. Since disk friction acts in a direction so as to block energy with which the runner 106 rotates, it is difficult to improve the efficiency of the hydraulic turbine when the disk fflcfionlossisincreased.

As a countern1easure to reduce the disk filcfion loss,it can be taken into t to reduce an outer dian1eter of the runner106. 'Hfisis based(N1thefactthatthecfiskfflcfionloss is in proportion to the fifth power of a rotating disk radius.

However, in the case of reducing the outer diameter of the runner 106, the hydrauHc tuflflne is rnade sxnaHen so that output of the lic turbine is reduced, and it is difficult to obtaHidesWed perfinTnance.

[0075] Furthen as another counternieasure,it can be taken Hmo t u)rnake adequate a channelarea ofthe back pressure r 113 or the lateral pressure chamber 115. This is based on the fact that the disk lloss can be reduced by decreashugthe channelarea ofthe back pressure chan1ber 113 or the lateral pressure chamber 115. However, if the channel area is too small, the friction loss of the back pressure or lateral pressure chan1ber 113 or 115 per se is Hureased, and itis difficult to make the channel area adequate.

[0076] Thus, in the present embodiment, to reduce the disk friction loss, g layers 130 and 131 having hydrophilicity are provided on the running water surface ce by which the channel of the running water is defined) of the back pressure chamber 113 and the running water e of the lateral pressure chamber 115.

To be more specific, as illustrated in FIGS. 11, 12A, and 128, the back pressure chamber g layer 130 having hydrophilicity is provided on a e (outer surface) 107a of the crown 107 which is located in the back pressure chamber 113. The back re chamber coating layer 130 may also be ed on a surface (inner surface) 114a of the aforementioned upper cover 114 which is located in the back pressure chamber 113. Here, the e 107a of the crown 107 which is located in the back pressure chamber 113 and the surface 114a of the upper cover 114 which is located in the back pressure chamber 113 constitute the running water surface of the back pressure chamber 113. The back pressure chamber coating layer 130 is preferably disposed at a radial outer side (upstream side) ve to the aforementioned back pressure chamber—side seal portion 119. That is, the back pressure chamber coating layer 130 is not preferably formed on the back pressure chamber—side seal n 119.

Further, the lateral pressure chamber coating layer 131 having hydrophilicity is provided on a surface (outer surface) 108a of the band 108 which is located in the lateral pressure chamber 115. The lateral pressure chamber coating layer 131 may also be ed on a surface (inner surface) 116a of the 3O lower cover 116 which is located in the lateral pressure chamber 115. Here, the surface 108a of the band 108 which is located in the lateral pressure chamber 115 and the surface 116a of the lower cover 116 which is located in the lateral pressure chamber 115 constitute the running water surface of the lateral pressure chamber 115. The lateral pressure chamber coating layer 131 is preferably disposed at a radial outer side (upstream side) relative to the aforementioned lateral pressure chamber—side seal portion 122. That is, the lateral pressure chamber coating layer 131 is not ably formed on the lateral pressure chamber-side seal portion 122.

In the present embodiment, the aforementioned back pressure and l pressure chamber coating layers 130 and 131 are formed by hydrophilic paint. Such hydrophilic paint is not particularly d as long as it has hydrophilicity. For example, paint containing a material having a hydrophilic group (—OH), such as a hydrophilic fluorine material or hydrophilic ship’s bottom paint, can be properly used. Further, the hydrophilic paint preferably has a contact angle of, for instance, 40 degrees or less (wherein the contact angle is an angle formed between a surface of the coating layer 130 or 131 which is a solid surface and a tangent line to an edge of water being in contact with the solid surface).

The back pressure chamber coating layer 130 is preferably provided with a plurality of back pressure chamber dimples es) 132 open to the back re chamber 113.

The back pressure chamber dimples 132 are formed in a part of the back pressure chamber coating layer 130 which is nt to the crown 107 and in a part of the back pressure chamber coating layer 130 which is adjacent to the upper cover 114.

Similarly, the lateral pressure chamber coating layer 131 is preferably provided with a plurality of lateral pressure chamber dimples es) 133 open to the l pressure chamber 115.

The lateral pressure chamber dimples 133 are formed in a part of the lateral re chamber coating layer 131 which is adjacent to the band 108 and in a part of the lateral pressure chamber coating layer 131 which is adjacent to the lower cover 116.

The dimples 132 and 133 are formed in the corresponding coating layers 130 and 131 in a concave shape like a small pit. Each of the dimples 132 and 133 preferably has a depth that is not less than 0.05 times and not more than 0.15 times a diameter of an inscribed circle of each of the dimples 132 and 133 when the planner shapes of the dimples 132 and 133 have a polygonal shape, or a er of each of the dimples 132 and 133 when the planner shapes of the dimples 132 and 133 have a circular shape. Here, as the depth of each of the dimples 132 and 133 is set to not less than 0.05 times the er, the dimples 132 and 133 can be formed with high precision. As the depth of each of the dimples 132 and 133 is set to not more than 0.15 times the er, an increase in friction loss caused by the presence itself of the dimples 132 and 133 can be ssed. On the other hand, the planer shape of the dimples 132 and 133 is not particularly limited, but it is preferably, for instance, a circular shape or a hexagonal shape. For example, if the diameter of the inscribed circle of each of the polygonal dimples 132 and 133 or the diameter (Dd illustrated in A) of each of the circular dimples 132 and 133 is 1 mm, the depth (Hd illustrated in 12A) of each of the dimples 132 and 133 is preferably not less than 50 um and not more than 150 pm. A depth of each of the coating layers 130 and 131 is not particularly limited if the dimples 132 and 133 can be formed, if the running water surfaces (the surfaces 107a and 114a located in the back pressure chamber and the es 108a and 116a located in the lateral pressure chamber) are not exposed to the s of the dimples 132 and 133, and if the materials of the coating layers 130 and 131 can be left . 3O r, an interval between the dimples 132 adjacent to each other and an interval between the dimples 133 adjacent to each other are preferably not less than 0.8 times and not more than 0.12 times the diameter of the inscribed circle of each of the dimples 132 and 133 when the planner shapes of the dimples 132 and 133 have the polygonal shape, or the diameter of each of the dimples 132 and 133 when the planner shapes of the dimples 132 and 133 have the circular shape. Thereby, an effect of reducing viscosity resistance of the water flow according to the dimples 132 and 133 can be effectively produced, which is experimentally confirmed by the inventors.

For example, if the diameter of the inscribed circle of each of the polygonal dimples 132 and 133 or the diameter (Dd illustrated in A) of each of the ar dimples 132 and 133 is 1 mm, the al (G illustrated in A) between the dimples 132 and the interval (G illustrated in A) between the dimples 133 are preferably not less than 0.8 mm and not more than 1.2 mm.

These coating layers 130 and 131 can be formed using, for instance, a mold 140 having bulges 141 corresponding to the dimples 132 and 133 of the coating layers 130 and 131 as illustrated in FIGS. 13A to 13C. In this case, as illustrated in A, hydrophilic paint is applied to the running water surface in a film shape at a given thickness first, and a paint film 134 is formed. Subsequently, as illustrated in 8, the mold 140 is pressed t the paint film 134 of the hydrophilic paint. In this case, the mold 140 is pressed such that the paint film 134 remains between the bulges 141 of the mold 140 and the running water surface. Next, in the state in which the mold 140 is pressed, the paint film 134 is dried and cured. After the paint film 134 is cured, the mold 140 is removed as illustrated in C. Thereby, it is possible to obtain the coating layers 130 and 131 in the present ment. Further, a method of forming the coating layers 130 and 131 is not limited to the aforementioned method. For e, after the paint film of the hydrophilic paint is cured, the mold 140 is placed on the cured paint film, and the hilic paint is applied to the ndings of the bulges 141 of the mold 140, and cured. Thereby, it is also possible to obtain the coating layers 130 and 131 in the present embodiment.

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

When a hydraulic turbine operation is conducted in the Francis turbine 101 according to the present embodiment, as illustrated in , water flows from the upper reservoir 201 (see ) into the casing 103 through the hydraulic iron pipe 200. The water flowing into the casing 103 flows from the casing 103 into the runner 106 through the stay vanes 104 and the guide vanes 105. Due to the water flowing into the runner 106, the runner 106 is rotatably driven. y, the generator 111 connected to the runner 106 via the main shaft 110 is driven to generate power. The water flowing into the runner 106 is discharged from the runner 106 to the lower reservoir 202 through the draft tube 112. In the meantime, the guide vanes 105 are rotated. Thereby, the opening degree of the guide vanes 105 is adjusted, and the capacity of power generation of the tor 111 is adjusted.

[0086] While the hydraulic turbine is operated, part of the water passing through the guide vanes 105 flows into the back pressure chamber 113. In other words, the water flow flowing into the back re chamber 113 through the back pressure chamber—side gap portion 117 ed at the radial outer side of the crown 107 is formed. Thereby, as illustrated in , the water is adapted to be adhered to a surface 135 of the back pressure chamber coating layer 130, so that a thin water adhesion layer 136 is formed. The water adhesion layer 136 is osed between the main flow formed by the running water located at the center side of the back pressure chamber 113 and the back pressure chamber coating layer 130. Further, the water forming the water adhesion layer 136 is not at a standstill with t to the back pressure chamber coating layer 130, but it has an extremely slow flow velocity. With the aforementioned configuration, it is possible to reduce the viscosity ance of the water flow in the proximity of the back pressure chamber coating layer 130, and to reduce the friction loss of the running water in the back pressure chamber 113 against the running water surfaces (the surfaces 107a and 114a located in the back pressure chamber).

Further, while the lic turbine is operated, part of the water passing through the guide vanes 105 flows into the lateral pressure r 115. In other words, a flow of the water flowing into the lateral pressure chamber 115 through the lateral pressure chamber-side gap portion 120 ed at the radial outer side of the band 108 is formed. Even in this case, since a water adhesion layer 136 is formed similarly to the back re chamber 113, it is possible to reduce the ity resistance of the water flow in the proximity of the lateral pressure chamber g layer 131, and to reduce the friction loss of the running water in the lateral pressure chamber 115 against the running water surfaces (the surfaces 108a and 116a located in the back pressure chamber).

[0088] The back pressure chamber coating layer 130 is provided with the a plurality of back pressure chamber dimples 132, and the lateral pressure chamber coating layer 131 is provided with the a plurality of lateral pressure chamber s 133.

Thereby, the water in the dimples 132 and 133 is adapted to be adhered to walls of the dimples 132 and 133 formed by the hydrophilic paint, and a flow velocity of the water in the dimples 132 and 133 is extremely reduced. Thereby, an effect of increasing a thickness of the aforementioned water adhesion 3O layer 136 in regions of the running water surfaces in which the dimples 132 and 133 are ed is obtained. For this , it is le to more reduce the viscosity resistance of the water flow flowing above the dimples 132 and 133, and cause the running water to smoothly flow on the running water surfaces.

According to the present embodiment, as described above, the back pressure chamber coating layer 130 formed by the hydrophilic paint is provided on the surface 107a of the crown 107 which is located in the back pressure chamber 113.

Further, the lateral pressure chamber coating layer 131 formed by the hydrophilic paint is provided on the surface 108a of the band 108 which is located in the lateral pressure chamber 115.

Thereby, the adhesion layer 136 of the water having an extremely low flow velocity can be formed on the surfaces of the coating layers 130 and 131, and the friction loss of the water flow flowing in the back pressure chamber 113 and lateral pressure chamber 115 can be reduced. For this reason, it is possible to reduce the disk friction loss caused by the rotation of the runner 106. Further, in this case, since the outer diameter of the runner 106 is not restricted, the outer diameter of the runner 106 can be decided depending on desired output of the Francis turbine 101. In on, the disk friction loss can be reduced regardless of the channel area and shape of the back pressure chamber 113 or the lateral pressure chamber 115.

Further, according to the present embodiment, as described above, the back pressure chamber coating layer 130 is provided on the surface 107a of the crown 107 which is d in the back pressure chamber 113 among the running water surface of the back pressure r 113. For this reason, it is possible to effectively reduce the viscosity resistance of the water flow in the crown—side’s region of the back pressure chamber 113 which can be vely increased in 3O velocity gradient and is located at the crown 107. se, the lateral re chamber g layer 131 is provided on the surface 108a of the band 108 which is d in the lateral pressure chamber 115 among the running water surface of the lateral pressure chamber 115. For this reason, it is possible to effectively reduce the viscosity ance of the water flow in the band—side’s region of the lateral pressure chamber 115 which can be relatively sed in velocity gradient and is located at the band 108.

Further, according to the present ment, the back pressure chamber coating layer 130 is disposed at a radial outer side relative to the back pressure chamber—side seal portion 119, and the lateral pressure chamber coating layer 131 is disposed at a radial outer side ve to the lateral pressure chamber—side seal n 122. Thereby, it is possible to prevent the back pressure r coating layer 130 from being formed at the back pressure chamber—side seal portion 119, and to prevent the lateral pressure chamber coating layer 131 from being formed at the lateral re r-side seal portion 122. For this reason, it is possible to prevent that an inflow rate of the water into the back pressure r 113 is increased on the ground that the friction loss of the water flow is reduced at the back pressure chamber-side seal portion 119 for suppressing the inflow rate of the water from the guide vanes 105 to the back pressure chamber 113. Similarly, it is possible to prevent that an inflow rate of the water into the lateral pressure chamber 115 is increased on the ground that the friction loss of the water flow is reduced at the lateral pressure chamber-side seal portion 122 for suppressing the inflow rate of the water from the guide vanes 105 to the lateral pressure chamber 115.

Further, according to the present embodiment, the back pressure chamber coating layer 130 is also ed on the surface 114a of the upper cover 114 which is located in the 3O back pressure chamber 113, and the l pressure chamber coating layer 131 is provided on the surface 116a of the lower cover 116 which is located in the lateral pressure chamber 115.

Thereby, it is possible to more reduce the friction loss of the water flow flowing in the back pressure chamber 113 and the lateral pressure chamber 115. Thus, it is possible to more reduce the disk friction loss caused by the rotation of the runner 106.

In on, ing to the present embodiment, the back pressure chamber coating layer 130 is provided with the a plurality of back pressure r dimples 132, and the lateral pressure chamber coating layer 131 is provided with the a ity of lateral pressure chamber dimples 133. Thereby, it is possible to still more reduce the ity resistance of the water flow in the proximity of the coating layers 130 and 131, and to more reduce the friction loss of the water flow.

Thus, ing to the present embodiment, it is possible to reduce the disk on loss to improve the efficiency of the hydraulic turbine.

[0095] For example, in the aforementioned embodiment, the example in which the lic turbine according to the t invention is applied to the Francis turbine has been described.

However, without being limited thereto, the present invention can also be applied to other hydraulic turbines except the Francis turbine. Further, the Francis turbine in the above embodiment may have a pump operation function of suctioning up the water of the lower reservoir 202 to pump up it to the upper reservoir 201.

[0096] Further, in the above ment, the example in which the back pressure chamber coating layer 130 is provided on the running water surface of the back pressure chamber 113, and the lateral pressure chamber coating layer 131 is provided on 3O the running water surface of the lateral pressure chamber 115 has been described. However, without being limited thereto, any one of the back pressure chamber coating layer 130 and the lateral pressure chamber coating layer 131 may be provided, and the other may not be provided. Even in this case, it is possible to reduce the disk friction loss caused by the rotation of the runner 106.

In addition, in the above embodiment, the example in which the coating layers 130 and 131 are formed by the hydrophilic paint has been described. r, without being d thereto, if the base material such as the crown 107 or the band 108 of the runner 106, the upper cover 114, or the lower cover 116 or the like is formed of aluminum, the coating layers 130 and 131 may be formed by, for instance, boehmite treatment. In this case, an aluminum hydrated oxide film may be formed on a running water surface ce) of the base material, and the coating layers 130 and 131 can have hydrophilic.

(Sixth embodiment) Next, a pipe in a sixth embodiment will be described using FIGS. 15 and 16.

In the sixth embodiment illustrated in FIGS. 15 and 16, a main difference is that a coating layer formed by hydrophilic paint is ed on a running water e of the pipe, and other configurations are approximately identical to those of the first embodiment illustrated in FIGS. 1 to 4. In FIGS. 15 and 16, the same parts as in the first embodiment rated in FIGS. 1 to 4 are given the same symbols, and ed description thereof will be omitted.

In the present embodiment, reference will be made to a Francis turbine 1 given as an example of a hydraulic turbine, and to a hydraulic iron pipe 200 that is given as an example of 3O the pipe and guides water from an upper reservoir 201 to a casing 3 (see FIGS. 1 and 10) of the Francis turbine 1.

As illustrated in , the hydraulic iron pipe (pipe) 200 in the present embodiment is configured to be connected to the casing 3 of the Francis turbine 1, and to guide the water from the upper reservoir 201 to the casing 3 of the Francis turbine 1 during hydraulic e operation. The water flowing out of the Francis turbine 1 is adapted to be guided to a lower reservoir 202.

As rated in , the hydraulic iron pipe 200 is equipped with a pipe body 210 and a running water surface 212 that is provided for the pipe body 210 and defines a channel 211 for water. Among them, the running water surface 212 is provided with a coating layer 213 formed by hydrophiiic paint, and the g layer 213 is provided with a plurality of (or multiple) dimples 214 open to the channel 211. The coating layer 213 and the s 214 may be equally formed with the same configuration as the coating layer 60 and the dimples 61 described in the aforementioned fourth embodiment or the g layers 130 and 131 and the dimples 132 and 133 described in the aforementioned fifth embodiment. Further, if the pipe body 210 is formed of aluminum, the coating layer 213 can be formed by, for instance, boehmite treatment.

Thus, according to the present embodiment, the coating layer 213 formed by the hydrophiiic paint is provided on the running water surface 212. Thereby, an adhesion layer 62 (see of the water having an extremely low flow velocity can be formed on a surface of the coating layer 213, and a friction loss of a water flow flowing in the channel 211 defined by the running water e 212 can be reduced. For this reason, it is possible to prevent energy of the water flowing into the casing 3 of the Francis turbine 1 from being dissipated, and to make good use of the energy of the water to e efficiency 3O of the hydraulic turbine.

Further, according to the present embodiment, the g layer 213 is provided with the a plurality of dimples 214.

Thereby, it is possible to more reduce viscosity resistance of the water flow in the proximity of the g layer 213 and to more reduce the friction loss of the water flow.

In the entioned present ment, the e in which the pipe is the hydraulic iron pipe 200 connected to the Francis turbine 1 has been described. r, the pipe connected to the hydraulic e is not limited to the hydraulic iron pipe 200 connected to the Francis e 1, and thus the present invention may be applied to an arbitrary pipe connected to an arbitrary hydraulic turbine.

According to the aforementioned embodiment, it is possible to reduce the friction loss to make good use of the energy of the water.

While certain embodiments of the present invention have been described, these embodiments have been presented by way of example only, and are not intended to limit the scope of the inventions. Indeed, the novel embodiments may be embodied in a variety of other forms; rmore, various omissions, substitutions and changes in the form of the embodiments described herein may be made without departing from the spirit of the inventions. The accompanying claims and their equivalents are intended to cover such forms or modifications as would fall within the scope and spirit of the inventions. Further, it will be understood that these embodiments can be at least partially combined properly without departing from the gist of the present invention.

Furthermore, in the above embodiments, the e in which the hydraulic turbine according to the present ion is applied to the Francis turbine has been described. However, 3O without being limited thereto, the present invention may be applied to other hydraulic turbines except the Francis turbine.

Claims (11)

1. A lic e comprising: a turbine body having a runner configured to be rotated by water flowing therein during hydraulic turbine ion, and a guide vane configured to adjust a flow rate of the water flowing into the runner; a running water surface provided in the turbine body, the running water surface defining a channel for water; and a coating layer provided on the running water surface, the coating layer being formed by hydrophilic paint.

2. The hydraulic turbine according to claim 1, wherein the coating layer includes a plurality of dimples open to the channel.

3. The hydraulic turbine according to claim 1 or 2, wherein: the turbine body has upper and lower covers opposite to each other, the guide vane is ed between the upper cover and the lower cover, the guide vane being rotatably supported by the upper and lower covers; the running water e provided for the upper cover and the running water surface provided for the lower cover each have a tive cover ating region in which the coating layer is not provided; and the cover non-coating region is formed to include rotation region of the guide vane when viewed in a direction taken along a rotational axis of the guide vane.

4. The hydraulic turbine according to any one of claims 1 to 3, wherein: the runner of the turbine body includes a plurality of runner blades; the running water surface provided for each runner blade has an upstream non-coating region in which the coating layer is not provided; and the upstream non-coating region is formed at upstream ends of pressure and n surfaces of the running water surface of each runner blade during hydraulic turbine operation.

5. The lic turbine according to claim 4, n, when an outlet diameter of the runner during the hydraulic turbine operation is defined as De, a length (Li) of the am non-coating region in a main flow direction is given as s: Li/De £ 0.8.

6. The hydraulic turbine according to any one of claims 1 to 5, n: the runner of the turbine body includes a plurality of runner ; the running water surface provided for each runner blade has a downstream non-coating region in which the coating layer is not provided; and the downstream non-coating region is formed at a downstream end of a suction surface of the running water surface of each runner blade during the hydraulic turbine operation.

7. The hydraulic turbine according to claim 6, wherein, when an outlet diameter of the runner during the hydraulic turbine operation is d as De, a length (Lo) of the downstream non-coating region in a main flow direction is given as follows: Lo/De £ 0.8.

8. The hydraulic turbine according to claim 2, wherein the dimples have a depth that is not less than 0.05 times and not more than 0.15 times a diameter of an inscribed circle of each dimple when the planar shape of each dimple is a polygonal shape, or a diameter of each dimple when the planar shape of each dimple is a circular shape.

9. The hydraulic turbine according to claim 2, wherein an interval between the dimples adjacent to each other has not less than 0.8 times and not more than 1.2 times a diameter of an inscribed circle of each dimple when the planar shape of each dimple is a polygonal shape, or a er of each dimple when the planar shape of each dimple is a circular shape.

10. The hydraulic turbine according to claim 2, wherein the dimple has a depth of not less than 50 mm and not more than 150 mm.

11. The hydraulic turbine according to claim 1, substantially as herein described with reference to any one of the embodiments shown in the accompanying