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JP6877962B2 - Manufacturing method of steam turbine partition plate, steam turbine and steam turbine partition plate - Google Patents
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JP6877962B2 - Manufacturing method of steam turbine partition plate, steam turbine and steam turbine partition plate - Google Patents

Manufacturing method of steam turbine partition plate, steam turbine and steam turbine partition plate Download PDF

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JP6877962B2
JP6877962B2 JP2016223358A JP2016223358A JP6877962B2 JP 6877962 B2 JP6877962 B2 JP 6877962B2 JP 2016223358 A JP2016223358 A JP 2016223358A JP 2016223358 A JP2016223358 A JP 2016223358A JP 6877962 B2 JP6877962 B2 JP 6877962B2
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inner ring
flow direction
steam
steam turbine
partition plate
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JP2018080629A (en
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憲一 村上
憲一 村上
光由 土屋
光由 土屋
誠 溝脇
誠 溝脇
太郎 村岡
太郎 村岡
一男 相良
一男 相良
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Mitsubishi Power Ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/10Geothermal energy

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Description

本発明は、蒸気タービン仕切板、蒸気タービン及び蒸気タービン仕切板の製造方法に関するものである。 The present invention relates to a steam turbine partition plate, a steam turbine, and a method for manufacturing a steam turbine partition plate.

蒸気タービンは、蒸気が通過する内部通路において、静翼と動翼が交互に複数段設置される。動翼は、ロータ軸と一体であり、蒸気圧力を受けて、ロータ軸を回転させる。動翼と動翼の間には、ノズルの役割を果たす静翼が設置された仕切板が設置される。仕切板は、静翼が設置された部分以外は、隔壁となっており、各動翼間の気密性が保たれる。図4及び図5に示すように、仕切板51は、車室に固定されるリング状の板状部材である外輪52と、ロータ軸側に設置されるリング状の板状部材である内輪54と、外輪52の内周端部と内輪54の外周端部の間に設置される静翼53などを備える。 In the steam turbine, stationary blades and moving blades are alternately installed in a plurality of stages in an internal passage through which steam passes. The rotor blades are integral with the rotor shaft and receive steam pressure to rotate the rotor shaft. A partition plate with a stationary blade that acts as a nozzle is installed between the moving blades. The partition plate is a partition plate except for the part where the stationary blades are installed, and the airtightness between the moving blades is maintained. As shown in FIGS. 4 and 5, the partition plate 51 includes an outer ring 52 which is a ring-shaped plate-shaped member fixed to the passenger compartment and an inner ring 54 which is a ring-shaped plate-shaped member installed on the rotor shaft side. A stationary blade 53 or the like installed between the inner peripheral end of the outer ring 52 and the outer peripheral end of the inner ring 54 is provided.

下記の特許文献1では、内輪と静翼、及び、外輪と静翼が互いに嵌合して仕切板を構成し、溶接工程と焼鈍工程を省くという技術が開示されている。下記の特許文献2では、静翼を溶接せずに嵌合させて組み付けた場合、上下二分割した内輪又は外輪の接合面付近で、静翼にかかる荷重が他の部分に比べて大きくなるという端部効果を抑制する技術が開示されている。下記の特許文献3では、360°の内輪を構成する上下二分割の分割内輪同士を連結して、内輪の倒れを防止する技術が開示されている。 Patent Document 1 below discloses a technique in which an inner ring and a stationary blade, and an outer ring and a stationary blade are fitted to each other to form a partition plate, and a welding step and an annealing step are omitted. According to Patent Document 2 below, when the stationary blades are fitted and assembled without welding, the load applied to the stationary blades becomes larger in the vicinity of the joint surface of the inner ring or the outer ring divided into upper and lower parts as compared with other parts. A technique for suppressing the edge effect is disclosed. Patent Document 3 below discloses a technique for preventing the inner ring from collapsing by connecting the upper and lower divided inner rings constituting the 360 ° inner ring.

特許第4131739号公報Japanese Patent No. 4131739 特許第4072177号公報Japanese Patent No. 4072177 特開2004−176548号公報Japanese Unexamined Patent Publication No. 2004-176548

図4に示すように、従来、内輪54と静翼53の間、外輪52と静翼53の間には、溶接がリング状に全周方向にわたって施されていたため、溶接工程と焼鈍工程に多くの作業時間を要していた。溶接部分は、例えば図4中の符号Mで示されている部分である。また、火力発電に用いられる蒸気タービンでは、嵌め合わせによる溶接作業の軽減や省略が行われるものがある。例えば、図5に示すように、外輪52と内輪54との間で静翼53を嵌め込み、これを移動しないように固定するため、押え板61を用いる場合がある。押え板61は、内輪54側にボルト65によって固定され、内輪54側から静翼53側へ径方向に突出した形状を有する。押え板61の突出部62は、静翼53に形成された凹部64と係止して、静翼53の周方向の移動が拘束される。 As shown in FIG. 4, conventionally, welding is performed between the inner ring 54 and the stationary blade 53 and between the outer ring 52 and the stationary blade 53 in a ring shape over the entire circumference, so that it is often used in the welding process and the annealing process. It took a lot of work time. The welded portion is, for example, a portion indicated by reference numeral M in FIG. Further, in some steam turbines used for thermal power generation, welding work is reduced or omitted by fitting. For example, as shown in FIG. 5, a holding plate 61 may be used to fit the stationary blade 53 between the outer ring 52 and the inner ring 54 and fix it so as not to move. The pressing plate 61 is fixed to the inner ring 54 side by a bolt 65, and has a shape protruding in the radial direction from the inner ring 54 side to the stationary blade 53 side. The protruding portion 62 of the pressing plate 61 is locked with the recess 64 formed in the stationary blade 53, and the movement of the stationary blade 53 in the circumferential direction is restricted.

図5に示すように、仕切板51では、内輪54の厚さ、すなわち、蒸気流れ方向の長さLが、静翼53の翼53bの蒸気流れ方向の長さLに比べて長い。これにより、仕切板51の内輪54の剛性を高めて、蒸気圧力による変形を抑制することができる。例えば、静翼53の翼53bの蒸気流れ方向の長さLに対して、内輪54の蒸気流れ方向の長さLは、長くなっている。静翼53は、下流側の動翼5に対して蒸気を効果的に噴射させるため、静翼53の翼53bは、静翼53の蒸気流れ方向の長さLのうち上流側部分よりも略中央付近から下流側端部にかけて設けられる。 As shown in FIG. 5, in the partition plate 51, the thickness of the inner ring 54, that is, the length L 6 in the steam flow direction is longer than the length L 5 in the steam flow direction of the blade 53b of the stationary blade 53. As a result, the rigidity of the inner ring 54 of the partition plate 51 can be increased, and deformation due to steam pressure can be suppressed. For example, to the steam flow direction of the length L 5 of the wing 53b of the stationary blade 53, the steam flow direction length L 6 of the inner ring 54 is longer. Stationary blade 53, in order to effectively inject steam against blades 5 of the downstream side, the wing 53b of the stationary blade 53, of the upstream portion of the vapor stream direction of the length L 4 of the stationary blade 53 It is provided from approximately the center to the downstream end.

また一方では、図5に示すように、内輪54と接合される静翼53の接合部分であるインナーシュラウド53aにおいて、押え板61を、仕切板51の上流側に設置する際には、静翼53の蒸気流れ方向の上流側において、押え板61の突出部62と係止できる凹部64を形成しておく必要がある。そのため、静翼53は、翼53bとインナーシュラウド53aの間には蒸気流れ方向の下流側へと後退する段差部が設けられて、翼53bは外周側(図5の紙面下方側)にあるインナーシュラウド53aが蒸気流れの上流側へ突出した形状を有する。 On the other hand, as shown in FIG. 5, in the inner shroud 53a which is a joint portion of the stationary blade 53 to be joined to the inner ring 54, when the holding plate 61 is installed on the upstream side of the partition plate 51, the stationary blade is installed. On the upstream side of the 53 in the steam flow direction, it is necessary to form a recess 64 that can be locked with the protruding portion 62 of the holding plate 61. Therefore, the stationary blade 53 is provided with a stepped portion between the blade 53b and the inner shroud 53a that recedes to the downstream side in the steam flow direction, and the blade 53b is an inner on the outer peripheral side (lower side of the paper surface in FIG. 5). The shroud 53a has a shape protruding to the upstream side of the steam flow.

このように、この静翼53は、翼53bが、蒸気流れ方向の中央付近から下流側のみに長さLで形成されるのに対して、静翼53のインナーシュラウド53aが、内輪54との接合にあたっての接合長さは、内輪54の蒸気流れ方向の長さLと同じになっている。すなわと、インナーシュラウド53aが、蒸気流れ方向の上流端側から下流端側の全てにわたって長さLで形成される。そのため、このような静翼53を削り出し加工によって製作する場合、図5の破線によるハッチング部分(長さLと長さLの差に相当する部分)で示すように、翼53bよりも蒸気流れ方向の上流側の部分を削り除去する加工をする必要があるため、余分な削り代を設けることになる。そのため、無駄な材料費や作業工数が発生するという問題がある。 Thus, the stationary blade 53, blade 53b has with respect to the vicinity of the center of the steam flow direction being formed in a length L 5 only on the downstream side, the inner shroud 53a of the stationary blade 53, an inner ring 54 bonding lengths of when bonding is the same as the vapor flow direction length L 6 of the inner ring 54. That is, the inner shroud 53a is formed with a length L 6 from the upstream end side to the downstream end side in the steam flow direction. Therefore, when such a stationary blade 53 is manufactured by machining, it is more than the blade 53b as shown by the hatched portion (the portion corresponding to the difference between the length L 6 and the length L 5) by the broken line in FIG. Since it is necessary to perform processing to remove the portion on the upstream side in the steam flow direction, an extra cutting allowance is provided. Therefore, there is a problem that wasteful material costs and work man-hours are generated.

また、地熱発電に用いられる蒸気タービンでは、地熱蒸気が蒸気タービンに供給され、蒸気タービンは、地熱蒸気によって駆動される。このとき、地熱蒸気に含まれるスケールSが、上流側に設置された押え板61やボルト65で形成される小さな段差溝を起点にその周辺に蓄積されることがあり、静翼53が閉塞したり腐食したりする要因の一つになるおそれがある。 Further, in a steam turbine used for geothermal power generation, geothermal steam is supplied to the steam turbine, and the steam turbine is driven by geothermal steam. At this time, the scale S contained in the geothermal steam may be accumulated around a small step groove formed by the holding plate 61 and the bolt 65 installed on the upstream side, and the stationary blade 53 is blocked. It may be one of the factors that cause or corrode.

本発明は、このような事情に鑑みてなされたものであって、内輪と静翼を溶接せずに接合するとき、静翼を削り出し加工によって製作する場合において、余分な削り代を低減することが可能な蒸気タービン仕切板、蒸気タービン及び蒸気タービン仕切板の製造方法を提供することを目的とする。 The present invention has been made in view of such circumstances, and reduces an extra cutting allowance when the inner ring and the stationary blade are joined without welding and the stationary blade is manufactured by cutting. It is an object of the present invention to provide a steam turbine partition plate, a steam turbine, and a method for manufacturing a steam turbine partition plate, which are possible.

上記課題を解決するために、本発明の蒸気タービン仕切板、蒸気タービン及び蒸気タービン仕切板の製造方法は以下の手段を採用する。
すなわち、本発明に係る蒸気タービン仕切板は、車室に固定された板状部材であり、周方向に配置されてリング状の外輪を構成する複数の外輪部材と、ロータ軸側に設置された板状部材であり、周方向に配置されてリング状の内輪を構成する複数の内輪部材と、前記外輪の内周端部と、前記内輪の外周端部の間に支持され、翼が形成された静翼部材と、前記内輪部材における蒸気流れ方向の下流側の面に設置され、前記内輪部材から前記静翼部材側へ突出した突出部を有する複数の押え板と、前記静翼部材における前記蒸気流れ方向の下流側の面において凹状に形成され、前記突出部と係止する凹部とを備え、前記静翼部材に形成された前記内輪部材と接合する接合部は、前記蒸気流れ方向の長さが、前記内輪部材の前記蒸気流れ方向の長さよりも短いことを特徴とする。
In order to solve the above problems, the following means are adopted in the method for manufacturing the steam turbine partition plate, the steam turbine and the steam turbine partition plate of the present invention.
That is, the steam turbine partition plate according to the present invention is a plate-shaped member fixed to the passenger compartment, and is installed on the rotor shaft side with a plurality of outer ring members arranged in the circumferential direction to form a ring-shaped outer ring. A wing is formed by being supported between a plurality of inner ring members which are plate-shaped members and are arranged in the circumferential direction to form a ring-shaped inner ring, an inner peripheral end portion of the outer ring, and an outer peripheral end portion of the inner ring. A plurality of holding plates installed on a surface of the inner ring member on the downstream side in the steam flow direction and having protrusions protruding from the inner ring member toward the stationary wing member, and the stationary wing member. The joint portion formed in a concave shape on the surface on the downstream side in the steam flow direction, provided with the protrusion and the recess for locking, and joined with the inner ring member formed on the stationary blade member is the length in the steam flow direction. The inner ring member is shorter than the length in the steam flow direction.

この構成によれば、内輪部材における蒸気流れ方向の下流側の面には、内輪部材から静翼部材へ突出した突出部が設置されており、押え板の突出部は、静翼部材における蒸気流れ方向の下流側の面に形成された凹状の凹部と係止する。これにより、突出部が凹部と係止して、静翼部材の周方向の移動が拘束される。また、静翼部材には、内輪部材と接合する接合部が形成されており、静翼部材における接合部は、蒸気流れ方向の長さが、内輪部材の蒸気流れ方向の長さよりも短い。そして、内輪部材及び静翼部材は、蒸気流れ方向の下流側の蒸気流れ方向に交わる径方向の面において、突出部と凹部によって互いに係止されていることから、静翼部材における接合部の蒸気流れ方向の上流側端部は、内輪部材の蒸気流れ方向の上流側端部よりも下流側に位置する。したがって、内輪部材及び静翼部材が、蒸気流れ方向の上流側の面において互いに係止される場合に比べて、静翼部材における接合部の長さを短くすることができる。その結果、翼を含む静翼部材を形成する際に、蒸気流れ方向の接合部の長さと静翼部材の長さの差により生じる余分な削り代を低減できる。また、突出部と凹部が、蒸気流れ方向の下流側に位置することから、蒸気流れ方向の上流側に位置する場合に比べて、押え板やボルトで形成される小さな段差溝を起点にしたスケールが付着しにくい。 According to this configuration, a protrusion protruding from the inner ring member to the stationary blade member is installed on the surface of the inner ring member on the downstream side in the steam flow direction, and the protruding portion of the holding plate is the steam flow in the stationary blade member. It locks with a concave recess formed on the surface on the downstream side in the direction. As a result, the protruding portion is locked with the concave portion, and the movement of the stationary blade member in the circumferential direction is restricted. Further, the stationary blade member is formed with a joint portion to be joined to the inner ring member, and the length of the joint portion in the stationary blade member in the steam flow direction is shorter than the length of the inner ring member in the steam flow direction. Since the inner ring member and the stationary blade member are locked to each other by the protruding portion and the concave portion on the radial surface intersecting the steam flow direction on the downstream side in the steam flow direction, the steam at the joint portion in the stationary blade member. The upstream end in the flow direction is located downstream of the upstream end in the steam flow direction of the inner ring member. Therefore, the length of the joint portion in the stationary blade member can be shortened as compared with the case where the inner ring member and the stationary blade member are locked to each other on the surface on the upstream side in the steam flow direction. As a result, when forming the stationary blade member including the blade, it is possible to reduce the extra cutting allowance caused by the difference between the length of the joint portion in the steam flow direction and the length of the stationary blade member. In addition, since the protrusions and recesses are located on the downstream side in the steam flow direction, the scale starts from a small step groove formed by a holding plate or a bolt as compared with the case where the protrusion and the recess are located on the upstream side in the steam flow direction. Is hard to adhere.

上記発明において、前記内輪部材の前記蒸気流れ方向の長さは、前記接合部の前記蒸気流れ方向の長さの1.5倍から2.5倍でもよい。 In the above invention, the length of the inner ring member in the steam flow direction may be 1.5 to 2.5 times the length of the joint portion in the steam flow direction.

上記発明において、前記突出部は、前記内輪の周方向に沿って、前記内輪部材に複数設置され、前記複数の押え板が設置される位置にそれぞれ対応して、複数の溝部が、前記内輪部材に形成され、複数の前記突出部が設置される位置にそれぞれ対応して、複数の前記凹部が、前記静翼部材に形成されてもよい。 In the above invention, a plurality of the projecting portions are installed on the inner ring member along the circumferential direction of the inner ring, and a plurality of groove portions correspond to the positions where the plurality of pressing plates are installed. The plurality of recesses may be formed in the stationary wing member corresponding to the positions where the plurality of protrusions are installed.

この構成によれば、押え板の突出部と接合部の凹部が、前記内輪の周方向に沿って複数設置されることから、内輪部材と静翼部材が確実に固定され、静翼部材の周方向の移動が更に拘束される。 According to this configuration, since a plurality of recesses of the protrusion and the joint of the presser plate are installed along the circumferential direction of the inner ring, the inner ring member and the stationary blade member are securely fixed, and the circumference of the stationary blade member is peripherally fixed. Directional movement is further constrained.

上記発明において、前記静翼部材は、前記翼の内周側で前記蒸気流れ方向の上流側に関し、前記接合部の端面と前記内輪の内周端面の間に段差部が設けられて、前記内輪の前記内周端面が、前記蒸気流れ方向の上流側へ突出した形状を有してもよい。 In the above invention, the stationary blade member is provided with a step portion between the end surface of the joint portion and the inner peripheral end surface of the inner ring with respect to the upstream side in the steam flow direction on the inner peripheral side of the blade, and the inner ring is provided. The inner peripheral end surface of the above may have a shape protruding toward the upstream side in the steam flow direction.

本発明に係る蒸気タービンは、ロータ軸と、前記ロータ軸に設置された動翼と、前記動翼に隣接して設置された、請求項1から4のいずれか1項に記載の蒸気タービン仕切板とを備える。 The steam turbine partition according to any one of claims 1 to 4, wherein the steam turbine according to the present invention includes a rotor shaft, a moving blade installed on the rotor shaft, and a steam turbine partition installed adjacent to the moving blade. It is equipped with a board.

上記発明において、前記蒸気タービン仕切板は、衝動段に設置されることが望ましい。 In the above invention, it is desirable that the steam turbine partition plate is installed in the impulse stage.

上記発明において、蒸気タービンは、地熱蒸気が供給され、前記地熱蒸気の少なくとも一部を含む蒸気によって駆動されてもよい。 In the above invention, the steam turbine may be supplied with geothermal steam and may be driven by steam containing at least a part of the geothermal steam.

本発明に係る蒸気タービン仕切板の製造方法は、車室に固定された板状部材であり、周方向に配置されてリング状の外輪を構成する複数の外輪部材と、ロータ軸側に設置された板状部材であり、周方向に配置されてリング状の内輪を構成する複数の内輪部材と、前記外輪の内周端部と、前記内輪の外周端部の間に支持され、翼が形成された静翼部材とを備え、前記静翼部材に形成された前記内輪部材と接合する接合部は、蒸気流れ方向の長さが、前記内輪部材の前記蒸気流れ方向の長さよりも短いことを特徴とする蒸気タービン仕切板の製造方法であって、前記内輪部材から前記静翼部材側へ突出した突出部を有する複数の押え板を、前記内輪部材における前記蒸気流れ方向の下流側の面に形成された溝に設置するステップと、前記静翼部材における前記蒸気流れ方向の下流側の面において凹状に形成された凹部に対して、前記突出部を係止させるステップとを備える。 The method for manufacturing a steam turbine partition plate according to the present invention is a plate-shaped member fixed to the passenger compartment, and is installed on a rotor shaft side with a plurality of outer ring members arranged in the circumferential direction to form a ring-shaped outer ring. A wing is formed by being supported between a plurality of inner ring members which are plate-shaped members and are arranged in the circumferential direction to form a ring-shaped inner ring, an inner peripheral end portion of the outer ring, and an outer peripheral end portion of the inner ring. The joint portion provided with the stationary blade member and joined with the inner ring member formed on the stationary blade member has a length in the steam flow direction shorter than the length in the steam flow direction of the inner ring member. A method for manufacturing a steam turbine partition plate, which is characterized in that a plurality of holding plates having protrusions protruding from the inner ring member toward the stationary blade member are provided on a surface of the inner ring member on the downstream side in the steam flow direction. It includes a step of installing in the formed groove and a step of locking the protruding portion with respect to the concave portion formed in a concave shape on the surface of the stationary blade member on the downstream side in the steam flow direction.

本発明によれば、内輪と静翼を溶接せずに接合するとき、静翼を削り出し加工によって製作する場合において、余分な削り代を低減することができる。 According to the present invention, when the inner ring and the stationary blade are joined without being welded, an extra cutting allowance can be reduced when the stationary blade is manufactured by cutting.

本発明の一実施形態に係る蒸気タービンの仕切板、動翼及びロータ軸を示す縦断面図である。It is a vertical sectional view which shows the partition plate, the moving blade and the rotor shaft of the steam turbine which concerns on one Embodiment of this invention. 本発明の一実施形態に係る蒸気タービンの仕切板部を示す斜視図である。It is a perspective view which shows the partition plate part of the steam turbine which concerns on one Embodiment of this invention. 本発明の一実施形態に係る蒸気タービンの押え板を示す斜視図である。It is a perspective view which shows the holding plate of the steam turbine which concerns on one Embodiment of this invention. 従来の蒸気タービンの仕切板の一例を示す縦断面図である。It is a vertical cross-sectional view which shows an example of the partition plate of the conventional steam turbine. 従来の蒸気タービンの仕切板の他の例を示す縦断面図である。It is a vertical sectional view which shows another example of the partition plate of the conventional steam turbine.

以下に、本発明に係る実施形態について、図面を参照して説明する。
本発明の一実施形態に係る蒸気タービンは、図1に示すように、蒸気が通過する内部通路10において、ロータ軸6の軸方向へ静翼(静翼部材)3と動翼5が交互に複数段設置される。各動翼5は、ロータ軸6と一体であり、蒸気の流れと圧力を受けて、ロータ軸6を回転させる。動翼5と動翼5の間には、複数枚の翼3bが配置された静翼3が設置された蒸気タービン仕切板1が設置される。複数ある各蒸気タービン仕切板1は、複数の静翼3が設置された部分以外は、隔壁となっており、動翼5間の気密性が保たれる。
なお、本実施形態に適用される蒸気は、水蒸気、地熱蒸気を少なくとも一部に含む蒸気であるが、有機ランキンサイクル(ORC)発電システムにおける低沸点媒体の媒体蒸気等でもよい。
Hereinafter, embodiments according to the present invention will be described with reference to the drawings.
In the steam turbine according to the embodiment of the present invention, as shown in FIG. 1, the stationary blades (static blade members) 3 and the moving blades 5 alternate in the axial direction of the rotor shaft 6 in the internal passage 10 through which steam passes. It is installed in multiple stages. Each rotor blade 5 is integrated with the rotor shaft 6 and receives the flow and pressure of steam to rotate the rotor shaft 6. A steam turbine partition plate 1 on which a stationary blade 3 on which a plurality of blades 3b are arranged is installed is installed between the moving blades 5 and the moving blades 5. Each of the plurality of steam turbine partition plates 1 is a partition wall except for a portion where a plurality of stationary blades 3 are installed, and airtightness between the moving blades 5 is maintained.
The steam applied to this embodiment is steam containing at least a part of steam and geothermal steam, but may be medium steam of a low boiling medium in an organic Rankine cycle (ORC) power generation system.

蒸気タービン仕切板1は、車室7に固定されるリング状の板状部材である外輪2と、ロータ軸6側に設置されるリング状の板状部材である内輪4と、外輪2の内周端部と内輪4の外周端部の間に設置される静翼3などを備える。本実施形態に係る蒸気タービン仕切板1は、例えば蒸気タービンの衝動段に設置される。 The steam turbine partition plate 1 includes an outer ring 2 which is a ring-shaped plate-shaped member fixed to the passenger compartment 7, an inner ring 4 which is a ring-shaped plate-shaped member installed on the rotor shaft 6 side, and an inner ring 2. A stationary blade 3 or the like installed between the peripheral end portion and the outer peripheral end portion of the inner ring 4 is provided. The steam turbine partition plate 1 according to the present embodiment is installed, for example, in the impulse stage of the steam turbine.

蒸気タービン仕切板1は、内輪4の内周側にロータ軸6が組み込まれる。そのため、蒸気タービン仕切板1は、組立や分解点検時の作業性を考慮して、本実施形態では上下2分割の半リング(180度リング)形状とされており、外輪2及び内輪4それぞれが2分割されている。 In the steam turbine partition plate 1, the rotor shaft 6 is incorporated on the inner peripheral side of the inner ring 4. Therefore, in consideration of workability during assembly and overhaul, the steam turbine partition plate 1 has a half ring (180 degree ring) shape divided into upper and lower parts in the present embodiment, and the outer ring 2 and the inner ring 4 are each formed. It is divided into two parts.

以下では、図2に示すように、蒸気タービン仕切板1が分割された、蒸気タービン仕切板1を構成する周方向180°分の半リング状の部材を仕切板部1Aという。また、外輪2が分割された、外輪2を構成する周方向180°分の半リング状の部材を分割外輪2A(又は外輪部材)といい、内輪4が分割された、内輪4を構成する周方向180°分の半リング状の部材を分割内輪4A(又は内輪部材)という。 In the following, as shown in FIG. 2, a semi-ring-shaped member having a circumferential direction of 180 °, which constitutes the steam turbine partition plate 1 in which the steam turbine partition plate 1 is divided, is referred to as a partition plate portion 1A. Further, a semi-ring-shaped member having a circumferential direction of 180 ° constituting the outer ring 2 in which the outer ring 2 is divided is referred to as a divided outer ring 2A (or an outer ring member), and the circumference forming the inner ring 4 in which the inner ring 4 is divided is referred to. A semi-ring-shaped member having a direction of 180 ° is called a split inner ring 4A (or inner ring member).

蒸気タービン仕切板1を組み立てる際には、一方の分割外輪2Aの内周端部の溝部2aに静翼3のアウターシュラウド3cを配置する。また、一方の分割内輪4Aの外周端部の凸状の突起部4aに静翼3のインナーシュラウド(接合部)3aを配置する。そして、順次に複数の静翼3を配置していき、一方の仕切板部1Aとする。同様にして、他方の分割外輪2Aの内周端部と他方の分割内輪4Aの外周端部に静翼3を順次配置して、他方の仕切板部1Aとする。 When assembling the steam turbine partition plate 1, the outer shroud 3c of the stationary blade 3 is arranged in the groove 2a at the inner peripheral end of one of the divided outer rings 2A. Further, the inner shroud (joint portion) 3a of the stationary blade 3 is arranged on the convex protrusion 4a at the outer peripheral end of one of the divided inner rings 4A. Then, a plurality of stationary blades 3 are sequentially arranged to form one partition plate portion 1A. Similarly, the stationary blades 3 are sequentially arranged at the inner peripheral end portion of the other split outer ring 2A and the outer peripheral end portion of the other split inner ring 4A to form the other partition plate portion 1A.

その後、一方の仕切板部1Aの分割外輪2Aの外周端部を車室7の内壁面に固定した後、ロータ軸6を分割内輪4Aの内周端部に配置する。そして、他方の仕切板部1Aの分割内輪4Aの内周端部がロータ軸6に対応するようにして、他方の仕切板部1Aを配置して、他方の仕切板部1Aの分割外輪の外周端部を車室7の内壁に固定する。つまり、二つの分割外輪2A、及び、二つの分割内輪4Aは、静翼3を挟持した状態で、蒸気タービン仕切板1が組み立てられることになる。 After that, the outer peripheral end of the split outer ring 2A of one of the partition plate portions 1A is fixed to the inner wall surface of the vehicle interior 7, and then the rotor shaft 6 is arranged at the inner peripheral end of the split inner ring 4A. Then, the other partition plate portion 1A is arranged so that the inner peripheral end portion of the divided inner ring 4A of the other partition plate portion 1A corresponds to the rotor shaft 6, and the outer circumference of the divided outer ring of the other partition plate portion 1A is arranged. The end is fixed to the inner wall of the passenger compartment 7. That is, the steam turbine partition plate 1 is assembled with the two split outer rings 2A and the two split inner rings 4A sandwiching the stationary blade 3.

図2では、蒸気タービン仕切板1の下側半分の部分である仕切板部1Aのみが示されており、この下側半分の仕切板部1Aには、上側半分の部分である仕切板部(図示せず。)が配置される。 In FIG. 2, only the partition plate portion 1A, which is the lower half portion of the steam turbine partition plate 1, is shown, and the partition plate portion 1A, which is the lower half portion, is the partition plate portion (the upper half portion). (Not shown) is placed.

図2に示すように、分割外輪2Aの内周端部には、その中心部に沿って溝部2aが形成されている。つまり、分割外輪2Aの内周端部にはその周面に沿って、径方向外側に延びる凹状の溝部2aが形成されている。一方、分割内輪4Aの外周端部には、その中心部に沿って突起部4aが形成されている。つまり、分割内輪4Aの外周端部にはその周面に沿って、径方向外側に延びる凸状の突起部4aが形成されている。なお、図示はしないが、上側半分の仕切板部も同様にして、分割外輪2Aの内周端部には溝部が形成され、分割内輪の外周端部には突起部が形成されている。そして、下側半分の仕切板部1Aと上側半分の仕切板部とを連結した際には、分割外輪2Aの溝部2a同士が連続し、分割内輪4Aの突起部4a同士が連続することになる。 As shown in FIG. 2, a groove portion 2a is formed at the inner peripheral end portion of the divided outer ring 2A along the central portion thereof. That is, a concave groove portion 2a extending radially outward is formed at the inner peripheral end portion of the divided outer ring 2A along the peripheral surface thereof. On the other hand, a protrusion 4a is formed along the central portion of the outer peripheral end of the divided inner ring 4A. That is, a convex protrusion 4a extending radially outward is formed at the outer peripheral end of the divided inner ring 4A along the peripheral surface thereof. Although not shown, the partition plate portion of the upper half is similarly formed with a groove portion at the inner peripheral end portion of the split outer ring 2A and a protrusion portion at the outer peripheral end portion of the split inner ring. When the lower half partition plate portion 1A and the upper half partition plate portion are connected, the groove portions 2a of the split outer ring 2A are continuous, and the protrusions 4a of the split inner ring 4A are continuous. ..

分割外輪2Aと分割内輪4Aとの間には、静翼3が配置される。つまり、複数の静翼3が周方向に沿って配列されることになる。静翼3は、インナーシュラウド3a、翼3b、及びアウターシュラウド3cを有しており、翼3bはインナーシュラウド3a及びアウターシュラウド3cに挟持された状態となっている。蒸気流れが生じたとき、隣り合う二枚の翼3bの間に形成される隙間が、動翼5へ向かい蒸気を噴出すノズルとしての機能を果たす。 A stationary blade 3 is arranged between the split outer ring 2A and the split inner ring 4A. That is, a plurality of stationary blades 3 are arranged along the circumferential direction. The stationary wing 3 has an inner shroud 3a, a wing 3b, and an outer shroud 3c, and the wing 3b is sandwiched between the inner shroud 3a and the outer shroud 3c. When a steam flow occurs, the gap formed between the two adjacent blades 3b functions as a nozzle for ejecting steam toward the moving blade 5.

インナーシュラウド3aの内周端部には、分割内輪4Aの突起部4aに嵌合する嵌合溝3dがその内周端部に沿って形成され、アウターシュラウド3cの外周端部には、分割外輪2Aの溝部2aに嵌合する嵌合突起3eがその外周端部に沿って形成されている。
また、分割内輪4Aの平坦面4bは、上側半分の分割内輪の平坦部と連結される。
At the inner peripheral end of the inner shroud 3a, a fitting groove 3d that fits into the protrusion 4a of the split inner ring 4A is formed along the inner peripheral end thereof, and at the outer peripheral end of the outer shroud 3c, the split outer ring is formed. A fitting protrusion 3e that fits into the groove portion 2a of 2A is formed along the outer peripheral end portion thereof.
Further, the flat surface 4b of the divided inner ring 4A is connected to the flat portion of the upper half of the divided inner ring.

本実施形態に係る静翼3に形成されたインナーシュラウド3aは、内輪4と接合する。内輪4における蒸気流れの下流側の面4cには、内輪4から静翼3へ径方向に突出した突出部12が形成された押え板11が複数箇所に設置されている。突出部12は、静翼3のインナーシュラウド3aにおける蒸気流れ方向の下流側の面3fに形成された凹部14と係止する。押え板11は、周方向に複数個所配置されている。本実施形態では、周方向180°分の半リング状の分割内輪4Aに例えば3箇所配置されているが、この数に限定されなく、内輪4のサイズや静翼3のサイズなどから適宜に選定される。押え板11の突出部12が凹部14と係止することにより、分割内輪4Aに対する静翼3の周方向の移動が拘束される。 The inner shroud 3a formed on the stationary blade 3 according to the present embodiment is joined to the inner ring 4. On the surface 4c on the downstream side of the steam flow in the inner ring 4, holding plates 11 having protrusions 12 protruding in the radial direction from the inner ring 4 to the stationary blade 3 are installed at a plurality of places. The protruding portion 12 is locked with the recess 14 formed on the surface 3f on the downstream side in the steam flow direction in the inner shroud 3a of the stationary blade 3. A plurality of pressing plates 11 are arranged in the circumferential direction. In the present embodiment, for example, three locations are arranged on the semi-ring-shaped divided inner ring 4A for 180 ° in the circumferential direction, but the number is not limited to this, and the size of the inner ring 4 and the size of the stationary blade 3 are appropriately selected. Will be done. By locking the protruding portion 12 of the pressing plate 11 with the recess 14, the movement of the stationary blade 3 in the circumferential direction with respect to the split inner ring 4A is restricted.

また、図1に示すように、押え板11が蒸気流れ方向の下流側の面3fに形成されることから、蒸気流れ方向の上流側に位置する上流側端面3gに対しては、押え板11の突出部12との係止を考慮する必要がなくなる。従い、分割内輪4Aに対して、静翼3の翼3bにおけるインナーシュラウド3aの蒸気流れ方向の上流側端面3gは、分割内輪4Aの蒸気流れ方向の上流側端面4dよりも下流側に位置することができる。 Further, as shown in FIG. 1, since the presser plate 11 is formed on the surface 3f on the downstream side in the steam flow direction, the presser plate 11 with respect to the upstream end surface 3g located on the upstream side in the steam flow direction. It is not necessary to consider the locking with the protruding portion 12. Therefore, with respect to the split inner ring 4A, the upstream end face 3g of the inner shroud 3a in the blade 3b of the stationary blade 3 in the steam flow direction is located on the downstream side of the upstream end face 4d of the split inner ring 4A in the steam flow direction. Can be done.

したがって、図5のような内輪54と静翼53のインナーシュラウド53aが、蒸気流れ方向の上流側の面54a,53cにおいて互いに係止される場合に比べて、インナーシュラウド3aの長さLを短くすることができる。その結果、翼3bを含むインナーシュラウド3aに対して、インナーシュラウド3aと接する分割内輪4Aの蒸気流れ方向の上流側に位置する上流側端面4dは、蒸気流れ方向の上流側へ突出した形状となる。 Thus, the inner shroud 53a of the inner ring 54 and the stationary blade 53 as shown in FIG. 5, the steam flow direction of the upstream side surface 54a, as compared with the case to be locked to each other at 53c, the inner shroud 3a length L 1 Can be shortened. As a result, with respect to the inner shroud 3a including the blade 3b, the upstream end surface 4d located on the upstream side of the split inner ring 4A in contact with the inner shroud 3a in the steam flow direction has a shape protruding toward the upstream side in the steam flow direction. ..

インナーシュラウド3aの蒸気流れ方向の長さLは、内輪4の蒸気流れ方向の長さLよりも短く、静翼3の翼3bの蒸気流れ方向の長さLとほぼ同等である。そのため、静翼3を削り出し加工によって製作する際は、蒸気流れ方向のインナーシュラウド3aの長さLと翼3bの長さLの差により生じる無駄な削り代が少ない。なお、内輪4の蒸気流れ方向の長さLは、例えば、静翼3のインナーシュラウド3aの長さL及び翼3bの蒸気流れ方向の長さLに対して、1.5倍から2.5倍である。これにより、蒸気タービン仕切板1の内輪4の剛性を高めて、蒸気圧力による変形を抑制することができる。 The length L 1 of the inner shroud 3a in the steam flow direction is shorter than the length L 3 of the inner ring 4 in the steam flow direction, and is substantially the same as the length L 2 of the blade 3b of the stationary blade 3 in the steam flow direction. Therefore, when manufacturing by machining machined stator vanes 3 is less wasteful cutting margin caused by the difference in length L 1 of the length L 1 and wings 3b of the steam flow direction of the inner shroud 3a. The length L 3 of the inner ring 4 in the steam flow direction is, for example, 1.5 times the length L 1 of the inner shroud 3a of the stationary blade 3 and the length L 2 of the blade 3b in the steam flow direction. It is 2.5 times. As a result, the rigidity of the inner ring 4 of the steam turbine partition plate 1 can be increased, and deformation due to steam pressure can be suppressed.

上述のような蒸気タービン仕切板1を組み立てる際には、例えば、分割外輪2Aが車室7の内壁面に固定される。この固定の際には、結合部(図示せず。)を車室7の内壁面及び分割外輪2Aの外周端部に形成しておき、これらの結合部によって分割外輪2Aを車室7の内壁面に固定する。その後、分割外輪2Aの内周端部に沿って形成された溝部2aに対して、静翼3のアウターシュラウド3cに形成された嵌合突起3eを嵌合させて、分割外輪2Aの内周端部に沿って静翼3を配設する。また、分割内輪4Aに形成された突起部4aを、静翼3のインナーシュラウド3aに形成された嵌合溝3dに嵌合させて配設する。順次に複数の静翼3のアウターシュラウド3cの嵌合突起3eを、分割外輪2Aに嵌合させて配設して、また、分割内輪4Aに形成された突起部4aに、静翼3のインナーシュラウド3aに形成された嵌合溝3dに嵌合させて配設することを行う。 When assembling the steam turbine partition plate 1 as described above, for example, the split outer ring 2A is fixed to the inner wall surface of the vehicle interior 7. At the time of this fixing, a joint portion (not shown) is formed on the inner wall surface of the passenger compartment 7 and the outer peripheral end portion of the split outer ring 2A, and the split outer ring 2A is formed inside the passenger compartment 7 by these joint portions. Fix it to the wall. After that, the fitting projection 3e formed on the outer shroud 3c of the stationary blade 3 is fitted to the groove portion 2a formed along the inner peripheral end portion of the split outer ring 2A, and the inner peripheral end of the split outer ring 2A is fitted. The stationary blade 3 is arranged along the portion. Further, the protrusion 4a formed on the divided inner ring 4A is fitted into the fitting groove 3d formed on the inner shroud 3a of the stationary blade 3 and arranged. The fitting protrusions 3e of the outer shrouds 3c of the plurality of stationary blades 3 are sequentially arranged by being fitted to the divided outer ring 2A, and the inner of the stationary blade 3 is formed on the protrusions 4a formed on the divided inner ring 4A. It is fitted and arranged in the fitting groove 3d formed in the shroud 3a.

このようにして、仕切板部1Aを形成した後、蒸気タービンのロータ軸6が分割内輪4Aの内周端部にシール部材(図示せず。)を介して配置される。その後、下側半分の分割内輪4Aと上側半分の分割内輪とを連結する。この際、動翼5が配設されたロータ軸6は上側半分の分割内輪の内周端部に配置されることになる。 After forming the partition plate portion 1A in this way, the rotor shaft 6 of the steam turbine is arranged at the inner peripheral end portion of the divided inner ring 4A via a seal member (not shown). After that, the lower half of the split inner ring 4A and the upper half of the split inner ring are connected. At this time, the rotor shaft 6 on which the moving blades 5 are arranged is arranged at the inner peripheral end portion of the upper half of the divided inner ring.

一方では、上側半分の分割内輪に対しても同様に行われ、上側半分の分割内輪4Aの外周端部に形成された突起部4aに対して、静翼3のインナーシュラウド3aに形成された嵌合溝3dに嵌合させる。また、上側半分の分割外輪2Aの内周端部に沿って形成された溝部2aに対して静翼3のアウターシュラウド3cに形成された嵌合突起3eに嵌合させる。これにより、上側半分の仕切板部が形成される。これによって、蒸気タービン仕切板1が組み立てられることになる。 On the other hand, the same is performed for the split inner ring of the upper half, and the fitting formed on the inner shroud 3a of the stationary blade 3 with respect to the protrusion 4a formed on the outer peripheral end of the split inner ring 4A of the upper half. It is fitted into the joint groove 3d. Further, the groove portion 2a formed along the inner peripheral end portion of the upper half of the split outer ring 2A is fitted into the fitting projection 3e formed on the outer shroud 3c of the stationary blade 3. As a result, the partition plate portion of the upper half is formed. As a result, the steam turbine partition plate 1 is assembled.

さらに、本実施形態では、内輪4の蒸気流れ下流側の面4cと、静翼3の蒸気流れ下流側の面3fには、複数の押え板11が設置される
外輪2の内周端部と内輪4の外周端部の間には、複数の静翼3が周方向に列状に配置されている。押え板11の突出部12が静翼3に形成された凹部14と係止することによって、静翼3の周方向の移動が拘束される。また、上側半分の仕切板部1Aにも同様に、分割内輪4Aと静翼3とは、突起部4aとインナーシュラウド3aの嵌合溝3dとの嵌合に加えて、押え板11が設置されて突出部12と凹部14との係止がされている。その結果、組立や分解点検時において仕切板部1Aを吊り上げたとき、分割内輪4Aが位置ずれを生じたり、落下するのを防止することにも寄与する。
Further, in the present embodiment, on the surface 4c on the downstream side of the steam flow of the inner ring 4 and the surface 3f on the downstream side of the steam flow of the stationary blade 3, a plurality of pressing plates 11 are installed on the inner peripheral end portion of the outer ring 2. A plurality of stationary blades 3 are arranged in a row in the circumferential direction between the outer peripheral ends of the inner ring 4. By locking the protruding portion 12 of the pressing plate 11 with the recess 14 formed in the stationary blade 3, the movement of the stationary blade 3 in the circumferential direction is restricted. Similarly, in the partition plate portion 1A of the upper half, the split inner ring 4A and the stationary blade 3 are provided with a holding plate 11 in addition to the fitting of the protrusion 4a and the fitting groove 3d of the inner shroud 3a. The protrusion 12 and the recess 14 are locked. As a result, when the partition plate portion 1A is lifted during assembly or overhaul, it also contributes to prevent the split inner ring 4A from being displaced or dropped.

押え板11は、図1に示すように、板状部材であり、内輪4に対して例えばボルト15によって固定される。内輪4には、蒸気流れ下流側の面4c側に、内周端部から外周に向けて凹状の溝部13が形成されており、押え板11が溝部13内に設置される。溝部13の深さは、押え板11の厚さと略同一である。これにより、押え板11が溝部13内に設置されたとき、内輪4の面4cと押え板11の外面が略同一面となる。 As shown in FIG. 1, the pressing plate 11 is a plate-shaped member, and is fixed to the inner ring 4 by, for example, a bolt 15. The inner ring 4 is formed with a concave groove portion 13 from the inner peripheral end portion toward the outer circumference on the surface 4c side on the downstream side of the steam flow, and the pressing plate 11 is installed in the groove portion 13. The depth of the groove portion 13 is substantially the same as the thickness of the holding plate 11. As a result, when the pressing plate 11 is installed in the groove portion 13, the surface 4c of the inner ring 4 and the outer surface of the pressing plate 11 become substantially the same surface.

押え板11には、図3に示すように、板厚方向に対して平行方向に貫通孔16が形成されており、貫通孔16内にボルト15を挿入できる。本実施形態では1枚の押え板11に対して、二つの貫通孔16が形成され、2本のボルト15で、押え板11を内輪4(分割内輪4A)に固定することによって、押え板11自体の回動を防止して位置固定が確実にできる。内輪4の面4cには、2本のボルト15の固定位置に対応して、溝部13内に貫通孔17が形成され、貫通孔17にはネジ溝が形成されている。 As shown in FIG. 3, the presser plate 11 is formed with a through hole 16 in a direction parallel to the plate thickness direction, and a bolt 15 can be inserted into the through hole 16. In the present embodiment, two through holes 16 are formed in one presser plate 11, and the presser plate 11 is fixed to the inner ring 4 (divided inner ring 4A) with two bolts 15, whereby the presser plate 11 is formed. The position can be securely fixed by preventing the rotation of itself. On the surface 4c of the inner ring 4, a through hole 17 is formed in the groove portion 13 corresponding to the fixing position of the two bolts 15, and a screw groove is formed in the through hole 17.

また、押え板11が配設される位置にある静翼3には、蒸気流れ方向の下流側の面3f側に凹状の凹部14が形成されており、押え板11の突出部12が凹部14内に設置される。凹部14の深さは、押え板11の厚さと略同一である。これにより、押え板11の突出部12が凹部14内に設置されたとき、蒸気流れ方向の下流側の面3fと押え板11の外面が略同一面となる。 Further, the stationary blade 3 at the position where the pressing plate 11 is arranged has a concave recess 14 formed on the surface 3f side on the downstream side in the steam flow direction, and the protruding portion 12 of the pressing plate 11 is the recess 14. It is installed inside. The depth of the recess 14 is substantially the same as the thickness of the holding plate 11. As a result, when the protruding portion 12 of the pressing plate 11 is installed in the recess 14, the surface 3f on the downstream side in the steam flow direction and the outer surface of the pressing plate 11 become substantially the same surface.

押え板11の一端部側に形成された突出部12は、内輪4に固定される側とは反対側になる外周側を向くように配設されている。突出部12は、押え板11が内輪4に固定されているとき、内輪4から静翼3側へと突出している。突出部12の側面は、静翼3に形成された凹部14の内壁面と接触し、突出部12が凹部14と係止する。 The protruding portion 12 formed on one end side of the presser plate 11 is arranged so as to face the outer peripheral side which is opposite to the side fixed to the inner ring 4. When the pressing plate 11 is fixed to the inner ring 4, the projecting portion 12 projects from the inner ring 4 toward the stationary blade 3. The side surface of the protruding portion 12 comes into contact with the inner wall surface of the recess 14 formed in the stationary blade 3, and the protruding portion 12 locks with the recess 14.

押え板11は、各静翼3に対して1枚ずつ設置する必要はなく、図2に示すように、複数個の静翼3を間に挟んで、間隔を空けて配置される。本実施形態では、分割内輪4Aに例えば3箇所配置されている。押え板11は、内輪4の周方向に沿って、複数個が内輪4に設置される。複数の押え板11が設置される位置に対応して、複数の凹部14が静翼3に形成されている。これにより、突出部12を有する押え板11と凹部14が、内輪4の周方向に沿って複数設置されることから、内輪4と静翼3が確実に固定され、静翼3の周方向の移動が更に拘束される。 It is not necessary to install one pressing plate 11 for each of the stationary blades 3, and as shown in FIG. 2, the pressing plates 11 are arranged with a plurality of stationary blades 3 sandwiched between them. In the present embodiment, for example, three locations are arranged on the divided inner ring 4A. A plurality of pressing plates 11 are installed on the inner ring 4 along the circumferential direction of the inner ring 4. A plurality of recesses 14 are formed in the stationary blade 3 corresponding to the positions where the plurality of holding plates 11 are installed. As a result, a plurality of pressing plates 11 and recesses 14 having the protrusions 12 are installed along the circumferential direction of the inner ring 4, so that the inner ring 4 and the stationary blade 3 are securely fixed, and the stationary blade 3 is in the circumferential direction. Movement is further constrained.

押え板11を設置する手順としては、まず、外輪2の内周端部に静翼3を固定配置し、内輪4の外周端部を静翼3に固定した後、溝部13内に押え板11を設置する。このとき、静翼3に形成された凹部14内に、押え板11の突出部12を嵌合する。 As a procedure for installing the pressing plate 11, first, the stationary blade 3 is fixedly arranged at the inner peripheral end of the outer ring 2, the outer peripheral end of the inner ring 4 is fixed to the stationary blade 3, and then the pressing plate 11 is installed in the groove 13. To install. At this time, the protruding portion 12 of the holding plate 11 is fitted into the recess 14 formed in the stationary blade 3.

そして、ボルト15を貫通孔16へ挿入して内輪4の貫通孔17と螺合し、押え板11を内輪4へ固定する。その結果、内輪4側から突出部12が径方向に突出した状態で、突出部12が、静翼3の凹部14と係止する。 Then, the bolt 15 is inserted into the through hole 16 and screwed into the through hole 17 of the inner ring 4, and the holding plate 11 is fixed to the inner ring 4. As a result, the protruding portion 12 is locked with the recess 14 of the stationary blade 3 in a state where the protruding portion 12 protrudes in the radial direction from the inner ring 4 side.

以上、本実施形態によれば、次の効果が得られる。
内輪4における蒸気流れ方向の下流側の面4cには、内輪4から静翼3へ径方向に突出した突出部12が形成された押え板11が設置されており、突出部12は、静翼3における蒸気流れ方向の下流側の面3fに形成された凹部14と係止する。これにより、突出部12が凹部14と係止して、静翼3の周方向の移動が拘束される。
As described above, according to the present embodiment, the following effects can be obtained.
On the surface 4c on the downstream side in the steam flow direction of the inner ring 4, a pressing plate 11 having a protrusion 12 formed with a protrusion 12 protruding in the radial direction from the inner ring 4 to the stationary blade 3 is installed, and the protruding portion 12 is a stationary blade. It locks with the recess 14 formed on the surface 3f on the downstream side in the steam flow direction in 3. As a result, the protruding portion 12 is locked with the recess 14, and the movement of the stationary blade 3 in the circumferential direction is restricted.

また、静翼3には、内輪4と接合するインナーシュラウド3aが形成されており、静翼3におけるインナーシュラウド3aは、蒸気流れ方向の長さLが、内輪4の蒸気流れ方向の長さLよりも短い。これは、押え板11が内輪4における蒸気流れ方向の下流側の面4cに配設されて、蒸気流れ方向の上流側に位置する上流側端面4dに配設する必要がない。このため、蒸気流れの上流側に関して、静翼3は、翼3bとインナーシュラウド3aとこれに接する内輪4の間に段差部が設けられる。段差部は、翼3bの内周側にあるインナーシュラウド3aに対して、内輪4の蒸気流れ方向の上流側に位置する上流側端面4dが蒸気流れの上流側へ突出した形状を有する。そして、内輪4及び静翼3は、蒸気流れ方向の下流側の面4c,3fにおいて、突出部12と凹部14によって互いに係止されている。図1に示すように、静翼3におけるインナーシュラウド3aの蒸気流れ方向の上流側端面3gは、内輪4の蒸気流れ方向の上流側に位置する上流側端面4dよりも下流側に位置する。 Further, the stationary blade 3, which is the inner shroud 3a is formed to be bonded to the inner ring 4, the inner shroud 3a in the stationary blade 3, the length L 1 is the vapor flow direction, the length of the steam flow direction of the inner ring 4 shorter than L 3. This does not need to dispose the holding plate 11 on the surface 4c on the downstream side in the steam flow direction of the inner ring 4 and on the upstream end surface 4d located on the upstream side in the steam flow direction. Therefore, on the upstream side of the steam flow, the stationary blade 3 is provided with a stepped portion between the blade 3b, the inner shroud 3a, and the inner ring 4 in contact with the inner shroud 3a. The stepped portion has a shape in which the upstream end surface 4d located on the upstream side of the inner ring 4 in the steam flow direction protrudes to the upstream side of the steam flow with respect to the inner shroud 3a on the inner peripheral side of the blade 3b. The inner ring 4 and the stationary blade 3 are locked to each other by the protrusion 12 and the recess 14 on the surfaces 4c and 3f on the downstream side in the steam flow direction. As shown in FIG. 1, the upstream end surface 3g of the inner shroud 3a in the stationary blade 3 in the steam flow direction is located on the downstream side of the upstream end surface 4d located on the upstream side in the steam flow direction of the inner ring 4.

したがって、図5に示すように、内輪54及び静翼53が、押え板61によって、蒸気流れ方向の上流側の面54a,53cにおいて互いに係止される場合に比べて、本実施形態では、静翼3におけるインナーシュラウド3aの長さLを短くすることができる。その結果、翼3bを含む静翼3を削り出し加工によって製作する際に生じる余分な削り代を低減できる。また、押え板11の突出部12と凹部14が、蒸気流れ方向の下流側に位置することから、図5に示すように、押え板61が上流側に設置される場合に比べて、押え板11の周囲にスケールが付着しにくい。特に、本実施形態に係る蒸気タービンを地熱発電に用いられる蒸気タービンに適用した場合、地熱蒸気が蒸気タービンに供給され、蒸気タービンは、地熱蒸気によって駆動される。このとき、押え板11やボルト15で形成される小さな段差溝を起点にして周囲にスケールが付着しにくくなり、静翼3が閉塞したり腐食したりすることを抑制できる。 Therefore, as shown in FIG. 5, in the present embodiment, the inner ring 54 and the stationary blade 53 are stationary as compared with the case where the inner ring 54 and the stationary blade 53 are locked to each other by the pressing plate 61 on the surfaces 54a and 53c on the upstream side in the steam flow direction. it is possible to shorten the length L 1 of the inner shroud 3a in the blade 3. As a result, it is possible to reduce the extra cutting allowance generated when the stationary blade 3 including the blade 3b is manufactured by cutting. Further, since the protrusion 12 and the recess 14 of the presser plate 11 are located on the downstream side in the steam flow direction, as shown in FIG. 5, the presser plate 61 is installed on the upstream side as compared with the case where the presser plate 61 is installed on the upstream side. The scale does not easily adhere to the periphery of 11. In particular, when the steam turbine according to the present embodiment is applied to a steam turbine used for geothermal power generation, geothermal steam is supplied to the steam turbine, and the steam turbine is driven by geothermal steam. At this time, it becomes difficult for the scale to adhere to the surroundings starting from the small step groove formed by the pressing plate 11 and the bolt 15, and it is possible to prevent the stationary blade 3 from being blocked or corroded.

1 :蒸気タービン仕切板
1A :仕切板部
2 :外輪
2A :分割外輪(外輪部材)
2a :溝部
3 :静翼(静翼部材)
3a :インナーシュラウド(接合部)
3b :翼
3c :アウターシュラウド
3d :嵌合溝
3e :嵌合突起
3f :面
3g :上流側端面
4 :内輪
4A :分割内輪(内輪部材)
4a :突起部
4b :平坦面
4c :面
4d :上流側端面
5 :動翼
6 :ロータ軸
7 :車室
10 :内部通路
11 :押え板
12 :突出部
13 :溝部
14 :凹部
15 :ボルト
16 :貫通孔
17 :貫通孔
51 :仕切板
52 :外輪
53 :静翼
53a :インナーシュラウド
53b :翼
53c :面
54 :内輪
54a :面
61 :押え板
62 :突出部
64 :凹部
65 :ボルト
1: Steam turbine partition plate 1A: Partition plate part 2: Outer ring 2A: Divided outer ring (outer ring member)
2a: Groove 3: Static blade (static blade member)
3a: Inner shroud (joint)
3b: Wing 3c: Outer shroud 3d: Fitting groove 3e: Fitting protrusion 3f: Surface 3g: Upstream end surface 4: Inner ring 4A: Divided inner ring (inner ring member)
4a: Protrusion 4b: Flat surface 4c: Surface 4d: Upstream end surface 5: Moving blade 6: Rotor shaft 7: Vehicle interior 10: Internal passage 11: Holding plate 12: Projection 13: Groove 14: Recess 15: Bolt 16 : Through hole 17: Through hole 51: Partition plate 52: Outer ring 53: Static blade 53a: Inner shroud 53b: Blade 53c: Surface 54: Inner ring 54a: Surface 61: Pressing plate 62: Protruding portion 64: Recessed portion 65: Bolt

Claims (8)

車室に固定された板状部材であり、周方向に配置されてリング状の外輪を構成する複数の外輪部材と、
ロータ軸側に設置された板状部材であり、周方向に配置されてリング状の内輪を構成する複数の内輪部材と、
前記外輪の内周端部と、前記内輪の外周端部の間に支持され、翼が形成された静翼部材と、
前記内輪部材における蒸気流れ方向の下流側の面に設置され、前記内輪部材から前記静翼部材側へ突出した突出部を有する複数の押え板と、
前記静翼部材における前記蒸気流れ方向の下流側の面において凹状に形成され、前記突出部と係止する凹部と、
を備え、
前記静翼部材に形成された前記内輪部材と接合する接合部は、前記蒸気流れ方向の長さが、前記内輪部材の前記蒸気流れ方向の長さよりも短いことを特徴とする蒸気タービン仕切板。
A plurality of outer ring members that are plate-shaped members fixed to the passenger compartment and are arranged in the circumferential direction to form a ring-shaped outer ring.
A plate-shaped member installed on the rotor shaft side, and a plurality of inner ring members arranged in the circumferential direction to form a ring-shaped inner ring.
A stationary blade member supported between the inner peripheral end of the outer ring and the outer peripheral end of the inner ring to form a wing.
A plurality of pressing plates installed on the surface of the inner ring member on the downstream side in the steam flow direction and having protrusions protruding from the inner ring member toward the stationary blade member.
A recess formed in a concave shape on the surface of the stationary blade member on the downstream side in the steam flow direction and engaging with the protrusion,
With
The joint portion formed on the stationary blade member and joined to the inner ring member is a steam turbine partition plate characterized in that the length in the steam flow direction is shorter than the length in the steam flow direction of the inner ring member.
前記内輪部材の前記蒸気流れ方向の長さは、前記接合部の前記蒸気流れ方向の長さの1.5倍から2.5倍である請求項1に記載の蒸気タービン仕切板。 The steam turbine partition plate according to claim 1, wherein the length of the inner ring member in the steam flow direction is 1.5 to 2.5 times the length of the joint portion in the steam flow direction. 前記突出部は、前記内輪の周方向に沿って、前記内輪部材に複数設置され、
前記複数の押え板が設置される位置にそれぞれ対応して、複数の溝部が、前記内輪部材に形成され、
複数の前記突出部が設置される位置にそれぞれ対応して、複数の前記凹部が、前記静翼部材に形成される請求項1又は2に記載の蒸気タービン仕切板。
A plurality of the protruding portions are installed on the inner ring member along the circumferential direction of the inner ring.
A plurality of grooves are formed in the inner ring member corresponding to the positions where the plurality of holding plates are installed.
The steam turbine partition plate according to claim 1 or 2, wherein the plurality of recesses are formed in the vane member corresponding to the positions where the plurality of protrusions are installed.
前記静翼部材は、前記翼の内周側で前記蒸気流れ方向の上流側に関し、前記接合部の端面と前記内輪の内周端面の間に段差部が設けられて、前記内輪の前記内周端面が、前記蒸気流れ方向の上流側へ突出した形状を有する請求項1から3のいずれか1項に記載の蒸気タービン仕切板。 The stationary blade member is provided with a step portion between the end surface of the joint portion and the inner peripheral end surface of the inner ring with respect to the upstream side in the steam flow direction on the inner peripheral side of the blade, and the inner circumference of the inner ring is provided. The steam turbine partition plate according to any one of claims 1 to 3, wherein the end face has a shape protruding upstream in the steam flow direction. ロータ軸と、
前記ロータ軸に設置された動翼と、
前記動翼に隣接して設置された、請求項1から4のいずれか1項に記載の蒸気タービン仕切板と、
を備える蒸気タービン。
With the rotor shaft
The rotor blades installed on the rotor shaft and
The steam turbine partition plate according to any one of claims 1 to 4, which is installed adjacent to the rotor blade.
A steam turbine equipped with.
前記蒸気タービン仕切板は、衝動段に設置される請求項5に記載の蒸気タービン。 The steam turbine according to claim 5, wherein the steam turbine partition plate is installed in an impulse stage. 地熱蒸気が供給され、前記地熱蒸気の少なくとも一部を含む蒸気によって駆動される請求項5又は6に記載の蒸気タービン。 The steam turbine according to claim 5 or 6, wherein geothermal steam is supplied and driven by steam containing at least a part of the geothermal steam. 車室に固定された板状部材であり、周方向に配置されてリング状の外輪を構成する複数の外輪部材と、ロータ軸側に設置された板状部材であり、周方向に配置されてリング状の内輪を構成する複数の内輪部材と、前記外輪の内周端部と、前記内輪の外周端部の間に支持され、翼が形成された静翼部材とを備え、前記静翼部材に形成された前記内輪部材と接合する接合部は、蒸気流れ方向の長さが、前記内輪部材の前記蒸気流れ方向の長さよりも短いことを特徴とする蒸気タービン仕切板の製造方法であって、
前記内輪部材から前記静翼部材側へ突出した突出部を有する複数の押え板を、前記内輪部材における前記蒸気流れ方向の下流側の面に形成された溝に設置するステップと、
前記静翼部材における前記蒸気流れ方向の下流側の面において凹状に形成された凹部に対して、前記突出部を係止させるステップと、
を備える蒸気タービン仕切板の製造方法。
A plate-shaped member fixed to the passenger compartment, a plurality of outer ring members arranged in the circumferential direction to form a ring-shaped outer ring, and a plate-shaped member installed on the rotor shaft side, arranged in the circumferential direction. The stationary wing member includes a plurality of inner ring members forming a ring-shaped inner ring, a stationary wing member supported between the inner peripheral end portion of the outer ring and the outer peripheral end portion of the inner ring, and a wing is formed. The joint portion to be joined to the inner ring member formed in is a method for manufacturing a steam turbine partition plate, characterized in that the length in the steam flow direction is shorter than the length in the steam flow direction of the inner ring member. ,
A step of installing a plurality of holding plates having protrusions protruding from the inner ring member toward the stationary blade member in a groove formed on a surface of the inner ring member on the downstream side in the steam flow direction.
A step of locking the protruding portion with respect to a concave portion formed in a concave shape on a surface of the stationary blade member on the downstream side in the steam flow direction.
A method of manufacturing a steam turbine partition plate comprising.
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