STEAM TURBINE STATOR VANE, STEAM TURBINE, AND PRODUCTION METHOD FOR STEAM TURBINE STATOR VANE
20220228510 · 2022-07-21
Assignee
Inventors
- Ryo Takata (Tokyo, JP)
- Yasuhiro Sasao (Yokohama-shi, JP)
- Naoto Tochitani (Yokohama-shi, JP)
- Soichiro TABATA (Yokohama-shi, JP)
Cpc classification
F05D2240/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/31
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/608
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/602
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01D25/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A steam turbine stator vane includes a vane body portion which has a vane surface including a pressure surface and a suction surface, a moisture removal channel disposed in the vane body portion, at least one slit opening to the vane surface to communicate with the moisture removal channel and extending along a height direction from a base end portion toward a tip end portion of the vane body portion, and at least one groove portion disposed in the vane surface and extending from the base end portion along the height direction, at least a part of the at least one groove portion overlapping the at least one slit along the height direction.
Claims
1. A steam turbine stator vane, comprising: a vane body portion which has a vane surface including a pressure surface and a suction surface; a moisture removal channel disposed in the vane body portion; at least one slit opening between a center of the pressure surface and a trailing edge in a direction orthogonal to a height direction from a base end portion toward a tip end portion of the vane body portion to communicate with the moisture removal channel, and extending along the height direction; and at least one groove portion disposed between the center of the pressure surface and the trailing edge in the direction orthogonal to the height direction and extending from the base end portion along the height direction, at least a part of the at least one groove portion overlapping the at least one slit along the height direction.
2. The steam turbine stator vane according to claim 1, wherein the at least one groove portion is configured to be inclined to a side of the trailing edge from the tip end portion toward the base end portion.
3. The steam turbine stator vane according to claim 1, wherein the at least one slit includes a plurality of slits disposed separately from each other in the height direction.
4. The steam turbine stator vane according to claim 3, wherein the steam turbine stator vane further includes a recess which is disposed in the vane surface and to which the plurality of slits open.
5. The steam turbine stator vane according to claim 1, wherein the at least one slit is disposed between the at least one groove portion and a leading edge.
6. The steam turbine stator vane according to claim 1, wherein the at least one slit is disposed between the at least one groove portion and the trailing edge.
7. The steam turbine stator vane according to claim 1, wherein the vane body portion includes a curved plate encompassing the moisture removal channel and configured such that a difference between a maximum value and a minimum value of a thickness of the curved plate falls within 40% of an average value of the thickness.
8. The steam turbine stator vane according to claim 7, wherein the curved plate includes a pressure surface-side curved plate which has a surface including at least a part of the pressure surface, and a suction surface-side curved plate which has a surface including at least a part of the suction surface, and wherein one of the at least one slit or the at least one groove portion is configured to include a joint where one end portion of the pressure surface-side curved plate and one end portion of the suction surface-side curved plate are joined by welding.
9. The steam turbine stator vane according to claim 8, wherein the vane body portion further includes a trailing edge portion disposed between the joint and the trailing edge, the trailing edge portion having a trailing edge-side pressure surface connected to the trailing edge and a trailing edge-side wall surface extending from a front end portion on the trailing edge-side pressure surface along a direction intersecting with the trailing edge-side pressure surface, and wherein the at least one groove portion includes the joint, and a part of the at least one groove portion is defined by the trailing edge-side wall surface.
10. The steam turbine stator vane according to claim 8, wherein the vane body portion further includes a trailing edge portion disposed between the joint and the trailing edge, the trailing edge portion having a trailing edge-side pressure surface connected to the trailing edge and a trailing edge-side wall surface extending from a front end portion on the trailing edge-side pressure surface along a direction intersecting with the trailing edge-side pressure surface, and wherein the at least one slit includes the joint, and a part of the at least one slit is defined by the trailing edge-side wall surface.
11. The steam turbine stator vane according to claim 8, wherein the suction surface-side curved plate includes an extension portion extending from the trailing edge toward a leading edge, the extension portion having a surface including at least a part of the pressure surface, wherein the one end portion of the suction surface-side curved plate includes a front end portion of the extension portion located on a side of the leading edge, and wherein the at least one groove portion includes the joint, and a part of the at least one groove portion is defined by an end surface at the front end portion of the extension portion.
12. A steam turbine, comprising: the steam turbine stator vane according to claim 1; an annular member for supporting the steam turbine stator vane; and a cavity disposed in the annular member and configured to receive a liquid from each of the moisture removal channel and the at least one groove portion in the vane body portion.
13. A production method for a steam turbine stator vane, the method comprising: a slit forming step of forming at least one slit that opens between a center of the pressure surface and a trailing edge in a direction orthogonal to a height direction from a base end portion toward a tip end portion of the vane body portion, which has the vane surface including a pressure surface and a suction surface, to communicate with a moisture removal channel disposed in the vane body portion, and extends along the height direction; and a groove portion forming step of forming at least one groove portion extending from the base end portion along the height direction between the center of the pressure surface and the trailing edge in the direction orthogonal to the height direction, at least a part of the at least one groove portion overlapping the at least one slit along the height direction.
Description
BRIEF DESCRIPTION OF DRAWINGS
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DETAILED DESCRIPTION
[0052] Some embodiments of the present invention will be described below with reference to the accompanying drawings. It is intended, however, that unless particularly identified, dimensions, materials, shapes, relative positions and the like of components described or shown in the drawings as the embodiments shall be interpreted as illustrative only and not intended to limit the scope of the present invention.
[0053] For instance, an expression of relative or absolute arrangement such as“in a direction”, “along a direction”, “parallel”, “orthogonal”, “centered”, “concentric” and “coaxial” shall not be construed as indicating only the arrangement in a strict literal sense, but also includes a state where the arrangement is relatively displaced by a tolerance, or by an angle or a distance whereby it is possible to achieve the same function.
[0054] For instance, an expression of an equal state such as “same”, “equal”, and “uniform” shall not be construed as indicating only the state in which the feature is strictly equal, but also includes a state in which there is a tolerance or a difference that can still achieve the same function.
[0055] Further, for instance, an expression of a shape such as a rectangular shape or a tubular shape shall not be construed as only the geometrically strict shape, but also includes a shape with unevenness or chamfered corners within the range in which the same effect can be achieved.
[0056] On the other hand, the expressions “comprising”, “including” or “having” one constitutional element is not an exclusive expression that excludes the presence of other constitutional elements.
[0057] The same configurations are indicated by the same reference characters and may not be described again in detail.
[0058]
[0059] As shown in
[0060] The annular member 13 defines an inner space 15 with the rotor 11. The annular member 13 and the stator vane 3 remain still without being linked to rotations of the rotor 11 and the rotor blade 12. The stator vane 3 extends along the radial direction (a direction orthogonal to the axis LA of the steam turbine 1) so as to traverse the inner space 15 from the annular member 13 toward the rotor 11. The rotor blade 12 extends along the radial direction so as to traverse the inner space 15 from the rotor 11 toward the annular member 13.
[0061] As shown in
[0062] In the illustrated embodiment, as shown in
[0063] The steam introduced to the inner space 15 mainly flows along the axial direction (a direction in which the axis LA of the steam turbine 1 extends). Hereinafter, upstream of the steam flow direction may simply be referred to as “upstream”, and downstream of the steam flow direction may simply be referred to as “downstream”.
[0064] With the steam flowing through the inner space 15 along the axial direction being a working fluid, the steam turbine 1 is configured to convert energy of the working fluid into rotational energy of the rotor 11. In the illustrated embodiment, provided that the combination of a vane row of the stator vanes 3 and a blade row of the rotor blades 12 is one stage, the steam turbine 1 includes a plurality of stages. The stator vanes 3 of each stage are disposed at predetermined intervals along the circumferential direction. The rotor blades 12 of each stage are disposed at predetermined intervals along the circumferential direction of the rotor 11. The stator vanes 3 of each stage rectify steam when the steam passes between the stator vanes 3 of each stage, and upon reception of the steam rectified by the stator vanes 3, the rotor blades 12 of each stage convert a force received from the steam into a rotational force to rotate the rotor 11. By the rotation of the rotor 11, a generator (not shown) mechanically connected to the rotor 11 is driven.
[0065] As shown in
[0066]
[0067] As shown in
[0068] As shown in
[0069] The stator vane 3 is disposed in a region 15A of the inner space 15 where a wet steam flow flows. In a certain embodiment, the region 15A is a region that satisfies a condition where the wetness of the steam flow is not less than 5% during the operation of the steam turbine 1. The vane body portion 4 is disposed such that the leading edge 43 is located upstream and the trailing edge 44 is located downstream in the steam flow direction. The pressure surface 45 is disposed to intersect with the steam flow direction so as to receive steam. Moisture in the wet steam flow adheres to the vane surface 47 (the pressure surface 45 and the suction surface 46) as water droplets (liquid).
[0070] As shown in
[0071] As shown in
[0072] As shown in
[0073] As shown in
[0074] The liquid W adhering between the leading edge 43 and the slit 7 in the vane surface 47 is sucked to the moisture removal channel 5 via the slit 7 by a differential pressure between the moisture removal channel 5 and the section 15B of the region 15A facing the vane surface 47. The liquid W sucked to the moisture removal channel 5 is sucked to the cavity 24 via the first communication hole 131 by a differential pressure between the moisture removal channel 5 and the cavity 24.
[0075] The liquid W adhering between the leading edge 43 and the groove portion 8 in the vane surface 47 is pushed by the flow of the steam flowing through the region 15A and enters the groove portion 8. The liquid W entering the groove portion 8 is sucked to the cavity 24 via the second communication hole 132 by a differential pressure between the groove portion 8 and the cavity 24.
[0076] The liquid W stored in the cavity 24 is discharged to the exhaust hood 17 via the third communication hole 133 by a differential pressure between the cavity 24 and the exhaust hood 17. In some other embodiments, the liquid W may be discharged to the outside of the steam turbine 1, or it may be configured such that the liquid W is sucked by a suction device (not shown) such as a suction pump.
[0077] In the embodiment shown in
[0078] In the embodiment shown in
[0079] In some other embodiments, each of the slit 7 and the groove portion 8 may be disposed between the leading edge 43 and the center of the pressure surface 45 or in the suction surface 46. However, since liquid (water film flow) is collected on the side of the trailing edge 44 in the pressure surface 45, each of the slit 7 and the groove portion 8 is preferably disposed in the pressure surface 45 relative to the suction surface 46 and is preferably disposed near the trailing edge 44 in the pressure surface 45. Further, the groove portion 8 may be disposed between the slit 7 and the trailing edge 44.
[0080]
[0081] As shown in
[0082]
[0083] As described above, for example, as shown in
[0084] In the illustrated embodiment, as shown in
[0085] With the above configuration, the stator vane 3 includes the slit 7 and the groove portion 8 disposed in the vane surface 47 which is the surface of the stator vane 3, and the slit 7 and the groove portion 8 overlap at least partially along the height direction. Thus, it is possible to remove the liquid W collected in the vane surface 47 by a section (upstream drainage section) of the slit 7 and the groove portion 8 disposed upstream (the side of the leading edge 43) of the vane surface 47. Further, it is possible to remove the liquid W collected downstream of the above-described upstream drainage section in the vane surface 47, by a section (downstream drainage section) of the slit 7 and the groove portion 8 disposed downstream (the side of the trailing edge 44) of the vane surface 47. That is, the stator vane 3 can remove the liquid W adhering to the vane surface 47, by the groove portion 8 and the slit 7 having higher removal efficiency of the liquid W than the groove portion 8. Thus, it is possible to improve the removal efficiency of the liquid W adhering to the vane surface 47.
[0086] Further, since one of the above-described upstream drainage section or the above-described downstream drainage section is the groove portion 8 that does not communicate with the moisture removal channel 5, the stator vane 3 can reduce the amount of the drive steam leaking to the moisture removal channel 5 through the slit, as compared with the configuration, where the two slits (the slit 7, the second slit 70) overlapping each other along the height direction are disposed in the vane surface 47, as in the stator vane 30 according to the comparative example. Further, unlike the configuration, where the two slits overlapping each other along the height direction are disposed in the vane surface 47, as in the stator vane 30 according to the comparative example, the stator vane 3 is free from the risk that the liquid W flows back from the moisture removal channel 5 via the slit 7, and thus the slit width need not be increased to improve a suction pressure of the slit 7. By suppressing the suction pressure of the slit 7, it is possible to further reduce the amount of the drive steam leaking to the moisture removal channel 5 through the slit 7. Thus, the stator vane 3 can reduce the amount of the drive steam leaking to the moisture removal channel 5 through the slit 7, making it possible to prevent the decrease in performance of the steam turbine 1.
[0087] In some embodiments, for example, as shown in
[0088]
[0089] In some embodiments, for example, as shown in
[0090] With the above configuration, since the plurality of slits 7B are disposed separately from each other in the height direction, as compared with a case where the single slit 7A extends along the height direction, it is possible to improve strength of the stator vane 3 in the vicinity of the slit 7. Improving the strength of the stator vane 3 in the vicinity of the slit 7, it is possible to reduce the thickness of the stator vane 3, and thus to reduce a production cost of the stator vane 3.
[0091] In some embodiments, for example, as shown in
[0092] In the embodiment shown in
[0093] With the above configuration, since the plurality of slits 7B disposed separately from each other open to the recess 9 disposed in the vane surface 47, the liquid W adhering to the vane surface 47 is pushed by the flow of the steam flowing through the region 15A, enters the recess 9, and is stored in the recess 9. Thus, the stator vane 3 including the recess 9 can prevent the liquid W adhering to the vane surface 47 from flowing downstream of the slits 7B in the vane surface 47 through the slits 7B. Thus, the stator vane 3 including the recess 9 can improve removal efficiency of the liquid W adhering to the vane surface 47.
[0094] In some embodiments, as shown in
[0095]
[0096] In some embodiments, as shown in
[0097] In some embodiments, as shown in
[0098] In some embodiments, as shown in
[0099] In some embodiments, the vane body portion 4 including the curved plate 6 described above is a sheet-metal part where the shape of the vane body portion 4 is formed by performing sheet-metal processing on at least one sheet metal. In this case, it is possible to form the vane body portion 4 including the curved plate 6 by performing sheet-metal processing (such as cutting, bending, and welding) on one or a plurality of sheet metals (such as metal plate materials each formed into a thin flat shape by rolling or the like). Thus, it is possible to reduce the material cost and a processing cost of the vane body portion 4. Thus, with the above configuration, since it is possible to reduce the material cost and the processing cost of the vane body portion 4, it is possible to reduce the production cost of the stator vane 3.
[0100] In some embodiments, as shown in
[0101] In the illustrated embodiment, as shown in
[0102] With the above configuration, one of the slit 7 or the groove portion 8 includes the joint WP where the one end portion 622 of the pressure surface-side curved plate 62 and the one end portion 632 of the suction surface-side curved plate 63 are joined by welding. That is, the shape of one of the slit 7 or the groove portion 8 is formed, when the curved plate 6 is formed by welding the one end portion 622 of the pressure surface-side curved plate 62 and the one end portion 632 of the suction surface-side curved plate 63. With the above configuration, since additional processing such as cutting is not needed to form one of the slit 7 or the groove portion 8, it is possible to reduce the processing cost, and thus to reduce the production cost of the stator vane 3. Further, with the above configuration, since one of the slit 7 or the groove portion 8 can be formed without processing such as cutting, it is possible to prevent a decrease in strength in the vicinity of one of the slit 7 or the groove portion 8.
[0103] In some embodiments, as shown in
[0104] In the embodiment shown in
[0105] In the embodiment shown in
[0106] In the embodiment shown in
[0107] In the embodiment shown in
[0108] With the above configuration, the at least one groove portion 8 includes the joint WP, and a part of the groove portion 8 is defined by the trailing edge-side wall surface 644. That is, the shape of the groove portion 8 is formed as a part of the trailing edge-side wall surface 644 of the trailing edge portion 64, when the curved plate 6 is formed by welding. Since a part of the above-described groove portion 8 is defined by the trailing edge-side wall surface 644 extending along the direction intersecting with the trailing edge-side pressure surface 642, it is possible to effectively prevent the liquid W adhering to the vane surface 47 from flowing toward the trailing edge-side pressure surface 642 from the trailing edge-side wall surface 644.
[0109] In some embodiments, as shown in
[0110] In the embodiment shown in
[0111] The shape of the slit 7 is defined by the end surface 623 at the one end portion 622 of the pressure surface-side curved plate 62, the trailing edge-side wall surface 644, and the joint WP joining a section between the end surface 623 and the trailing edge-side wall surface 644. The groove portion 8 is disposed in the trailing edge-side pressure surface 642 of the thick portion 64A (trailing edge portion 64) located between the slit 7 and the trailing edge 44, and has a U-shaped cross-sectional shape. By thus disposing the groove portion 8 in the trailing edge portion 64 located between the slit 7 and the trailing edge 44, as compared with a case where the groove portion 8 is disposed in the pressure surface-side curved plate 62 located between the slit 7 and the leading edge 43, it is possible to improve removal efficiency of the liquid adhering to the vane surface 47. Further, the process of forming the groove portion 8 in the trailing edge portion 64 can be performed more easily than the process of forming the groove portion 8 in the pressure surface-side curved plate 62. Furthermore, with the configuration where the groove portion 8 is not disposed in the pressure surface-side curved plate 62, it is possible to reduce the thickness of the pressure surface-side curved plate 62 (curved plate 6).
[0112] Moreover, setting the joint WP on the trailing edge-side wall surface 644 to a section 644A spaced apart from the front end portion 643 toward the side of the suction surface 46, it is possible to form the above-described recess 9 by a section 644B of the trailing edge-side wall surface 644 between the above-described section 644A and the front end portion 643, and the surface 621 of the pressure surface-side curved plate 62. That is, the shape of the recess 9 is formed as a part of the trailing edge-side wall surface 644 of the trailing edge portion 64, when the curved plate 6 is formed by welding.
[0113] With the above configuration, the at least one slit 7 includes the joint WP, and a part of the slit 7 is defined by the trailing edge-side wall surface 644. That is, the shape of the slit 7 is formed as a part of the trailing edge-side wall surface 644 of the trailing edge portion 64, when the curved plate 6 is formed by welding. Since a part of the above-described slit 7 is defined by the trailing edge-side wall surface 644 extending along the direction intersecting with the trailing edge-side pressure surface 642, the liquid W adhering to the vane surface 47 is removed from the vane surface 47 by the slit 7 in the trailing edge-side wall surface 644. Thus, with the above configuration, it is possible to effectively prevent the liquid W adhering to the vane surface 47 from flowing toward the trailing edge-side pressure surface 642 from the trailing edge-side wall surface 644.
[0114] In some embodiments, as shown in
[0115] In the embodiment shown in
[0116] With the above configuration, the at least one groove portion 8 includes the joint WP and a part of the groove portion 8 is defined by the end surface 653 at the front end portion 652 of the extension portion 65. That is, the shape of the groove portion 8 is formed as a part of the end surface 653 at the front end portion 652 of the extension portion 65, when the curved plate 6 is formed by welding the one end portion 622 of the pressure surface-side curved plate 62 and the front end portion 652. Since a part of the above-described groove portion 8 is defined by the end surface 653 at the front end portion 652 of the extension portion 65 located on the side of the leading edge 43, it is possible to effectively prevent the liquid W adhering to the end surface 653 from flowing toward the surface 651 (pressure surface) of the extension portion 65.
[0117] As shown in
[0118] With the above configuration, since the steam turbine 1 includes the cavity 24 disposed in the annular member 13 and configured to receive the liquid from each of the moisture removal channel 5 and the at least one groove portion 8 in the vane body portion 4, it is possible to store, in the cavity 24, the liquid W removed from the vane surface 47 by the slit 7 and the groove portion 8. Storing, in the cavity 24, the liquid W removed from the vane surface 47 by the slit 7 and the groove portion 8, it is possible to prevent that the liquid W accumulates in the slit 7 and the moisture removal channel 5 in the vane body portion 4, and removal efficiency of the liquid W adhering to the vane surface 47 by the slit 7 and the groove portion 8 is decreased. Thus, the above-described steam turbine 1 can effectively remove the liquid W adhering to the vane surface 47 by the slit 7 and the groove portion 8.
[0119]
[0120] As shown in
[0121] The slit forming step S102 includes forming the at least one slit 7 (7A, 7B) that opens to the vane surface 47 of the vane body portion 4, which has the vane surface 47 including the pressure surface 45 and the suction surface 46, to communicate with the moisture removal channel 5 disposed in the vane body portion 4, and extends along the height direction from the base end portion 41 toward the tip end portion 42 of the vane body portion 4.
[0122] The groove portion forming step S103 includes forming the at least one groove portion 8 which extends from the base end portion 41 along the height direction in the vane surface 47 and at least a part of which overlaps the at least one slit 7 along the height direction.
[0123] Each of the slit 7 and the groove portion 8 may be formed by cutting, or the shape of each of the slit 7 and the groove portion 8 may be formed when the curved plate 6 is formed as described above.
[0124] With the above method, the production method 100 for the steam turbine stator vane includes the slit forming step S102 of forming the at least one slit 7, and the groove portion forming step S103 of forming the at least one groove portion 8. The stator vane 3 produced by the production method 100 for the steam turbine stator vane includes the slit 7 and the groove portion 8 disposed in the vane surface 47 which is the surface of the stator vane 3, and the slit 7 and the groove portion 8 overlap at least partially along the height direction. Thus, the stator vane 3 produced by the production method 100 for the steam turbine stator vane can improve removal efficiency of the liquid W adhering to the vane surface 47 and can prevent the decrease in performance of the steam turbine 1.
[0125] The present invention is not limited to the above-described embodiments, and also includes an embodiment obtained by modifying the above-described embodiments and an embodiment obtained by combining these embodiments as appropriate.
REFERENCE SIGNS LIST
[0126] 1 Steam turbine [0127] 3 Stator vane [0128] 30 Stator vane according to comparative example [0129] 4 Vane body portion [0130] 41 Base end portion [0131] 42 Tip end portion [0132] 43 Leading edge [0133] 44 Trailing edge [0134] 45 Pressure surface [0135] 46 Suction surface [0136] 47 Vane surface [0137] 5 Moisture removal channel [0138] 51 Base end-side opening portion [0139] 52 Tip end-side opening portion [0140] 53 Trailing edge-side end portion [0141] 6 Curved plate [0142] 61 Inner surface [0143] 62 Pressure surface-side curved plate [0144] 63 Suction surface-side curved plate [0145] 64 Trailing edge portion [0146] 64A Thick portion [0147] 65 Extension portion [0148] 7, 7A, 7B Slit [0149] 70 Second slit [0150] 71 Inlet opening [0151] 72 Outlet opening [0152] 8 Groove portion [0153] 81 Opening end portion [0154] 9 Recess [0155] 91 Opening end portion [0156] 11 Rotor [0157] 12 Rotor blade [0158] 12A Last-stage rotor blade [0159] 13 Annular member [0160] 131 First communication hole [0161] 132 Second communication hole [0162] 133 Third communication hole [0163] 14 Bearing [0164] 15 Inner space [0165] 15A Region [0166] 15B Section [0167] 16 Casing [0168] 17 Exhaust hood [0169] 18 Steam inlet [0170] 19 Steam outlet [0171] 20 Steam introduction line [0172] 21 Steam generation device [0173] 22 Exhaust hood inlet [0174] 23 Diaphragm [0175] 24 Cavity [0176] 100 Production method for stator vane [0177] LA Axis [0178] S101 Curved plate forming step [0179] S102 Slit forming step [0180] S103 Groove portion forming step [0181] T Thickness [0182] TH Throat section [0183] W Liquid [0184] WP Joint