JP6302368B2 - Stator blades and vane units, steam turbines - Google Patents

Stator blades and vane units, steam turbines Download PDF

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JP6302368B2
JP6302368B2 JP2014133259A JP2014133259A JP6302368B2 JP 6302368 B2 JP6302368 B2 JP 6302368B2 JP 2014133259 A JP2014133259 A JP 2014133259A JP 2014133259 A JP2014133259 A JP 2014133259A JP 6302368 B2 JP6302368 B2 JP 6302368B2
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stationary blade
divided
end portion
rotor
groove
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JP2016011625A (en
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丸山 隆
隆 丸山
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Mitsubishi Power Ltd
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Mitsubishi Hitachi Power Systems Ltd
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Description

本発明は、回転機械などに適用される静翼、外輪と内輪が周方向に所定間隔で配置される複数の静翼により連結される静翼ユニット、複数の静翼と複数の動翼を有して蒸気を用いてロータを駆動回転する蒸気タービンに関するものである。   The present invention has a stationary blade applied to a rotary machine or the like, a stationary blade unit in which an outer ring and an inner ring are connected by a plurality of stationary blades arranged at predetermined intervals in the circumferential direction, and a plurality of stationary blades and a plurality of moving blades. The present invention relates to a steam turbine that drives and rotates a rotor using steam.

一般的な蒸気タービンは、ケーシングに回転軸であるロータが回転自在に支持され、このロータの外周部に動翼が設けられる一方、ケーシングに静翼が設けられ、蒸気通路に静翼と動翼の段が複数配設されて構成されている。従って、蒸気が蒸気通路を流れると、この蒸気が静翼により整流され、動翼を介してロータを駆動回転することができる。   In a general steam turbine, a rotor, which is a rotating shaft, is rotatably supported by a casing, and a moving blade is provided on the outer periphery of the rotor, while a stationary blade is provided on the casing, and a stationary blade and a moving blade are provided in a steam passage. A plurality of stages are arranged. Therefore, when the steam flows through the steam passage, the steam is rectified by the stationary blade, and the rotor can be driven and rotated through the moving blade.

このような蒸気タービンにて、一般的に、静翼は、基端部にシュラウドが固定され、先端部に分割環が固定され、この一体となった静翼とシュラウドと分割環がリング状に組付けられて静翼ユニットが構成されている。そして、静翼は、基端部がシュラウドに当接した状態で隅肉溶接により固定され、先端部が分割環に当接した状態で隅肉溶接により固定されている。ところが、静翼とシュラウド、静翼と分割環を隅肉溶接により固定すると、この隅肉溶接部が蒸気通路側に位置することとなり、蒸気流れを妨げてしまうおそれがある。   In such a steam turbine, a stationary blade generally has a shroud fixed to a base end portion, and a split ring is fixed to a distal end portion. The integrated stationary blade, shroud, and split ring are in a ring shape. The vane unit is assembled. The stationary blade is fixed by fillet welding with the base end in contact with the shroud, and is fixed by fillet welding with the tip in contact with the split ring. However, if the stationary blade and the shroud, and the stationary blade and the split ring are fixed by fillet welding, the fillet welded portion is positioned on the steam passage side, which may hinder the steam flow.

そこで、静翼の基端部をシュラウドに貫通すると共に、静翼の先端部を分割環に貫通し、各貫通部を開先溶接により固定することが提案されている。なお、静翼の各端部をシュラウドや分割環に貫通して溶接により固定するものとしては、例えば、下記特許文献1に記載されたものがある。また、静翼の各端部をシュラウドや分割環に対して開先溶接により固定するものとしては、例えば、下記特許文献2に記載されたものがある。   Therefore, it has been proposed to penetrate the base end portion of the stationary blade through the shroud, penetrate the distal end portion of the stationary blade through the split ring, and fix each through portion by groove welding. In addition, as what penetrates each edge part of a stationary blade through a shroud or a division | segmentation ring and is fixed by welding, there exist some which were described in the following patent document 1, for example. Moreover, as what fixes each edge part of a stationary blade with respect to a shroud or a division | segmentation ring by groove welding, there exist some which were described in the following patent document 2, for example.

特開平10−184311号公報JP-A-10-184111 実開平05−017101号公報Japanese Utility Model Publication No. 05-017101 特開2008−032001号公報JP 2008-032001 A

上述したように、静翼の端部をシュラウドや分割環に貫通し、この貫通部を開先溶接により固定する場合、シュラウドや分割環に静翼の端部が貫通する貫通孔を形成する必要がある。ところが、静翼は、外面が湾曲形状をなすと共に周方向に捩じられた3次元形状をなしていることから、シュラウドや分割環に形成する貫通孔は、静翼の端部の大きさよりも大きなものとなってしまう。すると、静翼における端部の外面とシュラウドや分割環における貫通孔の内面との間に大きな隙間が生じ、開先溶接が困難となってしまう。なお、プラットフォームを2分割することは、特許文献3に記載されているが、静翼と分割のプラットフォームが一体構造をなすものであり、隣接するプラットフォームと係合する構成であり、この隣接するプラットフォーム同士を溶接するものではない。   As described above, when the end of the stationary blade is passed through the shroud or the split ring and this through portion is fixed by groove welding, it is necessary to form a through hole through which the end of the stationary blade passes through the shroud or the split ring. There is. However, since the stationary blade has a three-dimensional shape in which the outer surface has a curved shape and is twisted in the circumferential direction, the through-hole formed in the shroud or the split ring is larger than the size of the end portion of the stationary blade. It will be big. Then, a large gap is generated between the outer surface of the end portion of the stationary blade and the inner surface of the through hole in the shroud or the split ring, and groove welding becomes difficult. In addition, although dividing | segmenting a platform into 2 is described in patent document 3, it is the structure which a stator blade and a division | segmentation platform make an integral structure, and engages with an adjacent platform, This adjacent platform They are not welded together.

本発明は、上述した課題を解決するものであり、通路側への突出部を抑制して性能の向上を図ると共に組付を容易として作業性の向上を図る静翼、静翼ユニット、蒸気タービンを提供することを目的とする。   SUMMARY OF THE INVENTION The present invention solves the above-described problems, and improves the performance by suppressing the protruding portion to the passage side and facilitates the assembly to improve the workability, the stationary blade unit, and the steam turbine. The purpose is to provide.

上記の目的を達成するための本発明の静翼は、静翼本体と、前記静翼本体の端部が貫通して固定される支持部材と、を有し、前記支持部材は、前記静翼本体の端部の周囲に配置される複数の分割体から構成され、前記複数の分割体同士の間に溶接部が設けられると共に、前記静翼本体の端部と前記分割体との間に開先溶接部が設けられる、ことを特徴とするものである。   In order to achieve the above object, a stationary blade of the present invention includes a stationary blade body and a support member to which an end portion of the stationary blade body passes and is fixed, and the support member includes the stationary blade. It is composed of a plurality of divided bodies arranged around the end of the main body, and a welded portion is provided between the plurality of divided bodies, and is opened between the end of the stationary blade body and the divided bodies. A pre-welded part is provided.

従って、静翼は、静翼本体の端部の周囲に複数の分割体が配置され、複数の分割体同士が溶接部により連結されると共に、静翼本体の端部と各分割体が開先溶接により連結されて構成されている。支持部材を複数の分割体から構成することで、静翼本体が湾曲形状をなすと共に周方向に捩じられた3次元形状であっても、静翼本体の端部と各分割体を隙間なく適正に連結することができる。そして、開先溶接を実施可能であることから、通路側への溶接部の突出を抑制して蒸気流れを妨げることがない。その結果、通路側への突出部を抑制して性能の向上を図ることができると共に、組付を容易として作業性の向上を図ることができる。   Accordingly, the stationary blade has a plurality of divided bodies arranged around the end portion of the stationary blade body, the plurality of divided bodies are connected to each other by the welded portion, and the end portion of the stationary blade body and each divided body are grooved. They are connected by welding. By configuring the support member from a plurality of divided bodies, even if the stationary blade body has a curved shape and a three-dimensional shape twisted in the circumferential direction, the end of the stationary blade body and each divided body can be connected without gaps. It can be connected properly. And since groove welding can be implemented, the protrusion of the welding part to the channel | path side is suppressed and a steam flow is not prevented. As a result, it is possible to improve the performance by suppressing the protruding portion to the passage side, and to improve the workability by facilitating the assembly.

本発明の静翼では、前記複数の分割体は、前記静翼本体との連結部に開先部が設けられることを特徴としている。   In the stationary blade of the present invention, the plurality of divided bodies are characterized in that a groove portion is provided at a connection portion with the stationary blade body.

従って、静翼本体の外面形状に応じて各分割体における静翼本体との連結部に最適形状の開先部を設けることができ、静翼本体と分割体を適正に開先溶接することができる。   Therefore, it is possible to provide a groove portion of an optimal shape at the connecting portion of each divided body with the stationary blade body in accordance with the outer surface shape of the stationary blade body, and to appropriately weld the groove to the stationary blade body and the divided body. it can.

本発明の静翼では、前記複数の分割体は、前記開先部とは反対側の面に、隣接する前記支持部材との連結部が設けられることを特徴としている。   In the stationary blade of the present invention, the plurality of divided bodies are characterized in that a connecting portion with the adjacent support member is provided on a surface opposite to the groove portion.

従って、静翼本体の端部と各分割体が開先溶接により連結されて構成された静翼は、開先部の反対側に設けられた連結部により隣接する支持部材、つまり、静翼と連結することができ、各静翼(各支持部材)同士を高精度に連結することができる。   Therefore, the stationary blades configured by connecting the end portion of the stationary blade body and each divided body by groove welding are the supporting members adjacent to the connecting portion provided on the opposite side of the groove portion, that is, the stationary blades. The stator blades (support members) can be connected with high accuracy.

本発明の静翼では、前記複数の分割体は、前記静翼本体の背側に配置される第1分割体と、前記静翼本体の腹側に配置される第2分割体と、前記静翼本体の後縁部側に配置される第3分割体とを有することを特徴としている。   In the stationary blade of the present invention, the plurality of divided bodies include a first divided body disposed on the back side of the stationary blade body, a second divided body disposed on the ventral side of the stationary blade body, and the static body. It has the 3rd division body arrange | positioned at the rear-edge part side of a wing | blade main body, It is characterized by the above-mentioned.

従って、静翼本体の背側に配置される第1分割体と、静翼本体の腹側に配置される第2分割体と、静翼本体の後縁部側に配置される第3分割体とにより分割体を構成することで、組付性を向上することができる。   Accordingly, the first divided body disposed on the back side of the stationary blade body, the second divided body disposed on the ventral side of the stationary blade body, and the third divided body disposed on the rear edge portion side of the stationary blade body. Assembling property can be improved by constituting a divided body.

本発明の静翼では、前記第3分割体は、2個の連結部からなるV字形状部が設けられ、前記2個の連結部の交差部に非開先溶接部が設けられることを特徴としている。   In the stationary blade of the present invention, the third divided body is provided with a V-shaped portion including two connecting portions, and a non-groove welded portion is provided at an intersection of the two connecting portions. It is said.

従って、静翼の端部と第3分割体におけるV字形状部の交差部とは、開先溶接しないことから、静翼本体の端部における後縁部の溶接熱により形状変形を抑制することができる。   Therefore, since the end portion of the stationary blade and the intersection of the V-shaped portion in the third divided body are not groove-welded, shape deformation is suppressed by the welding heat of the trailing edge portion at the end portion of the stationary blade body. Can do.

本発明の静翼では、前記静翼本体の端部が前記支持部材より突出して配置されることを特徴としている。   The stationary blade according to the present invention is characterized in that an end portion of the stationary blade body is disposed so as to protrude from the support member.

従って、静翼本体を製造するとき、高精度の長さ設定を不要として、製造コストを低減することができる。   Therefore, when manufacturing the stationary blade body, it is not necessary to set the length with high accuracy, and the manufacturing cost can be reduced.

本発明の静翼では、前記静翼本体は、長手方向に貫通する中空部が設けられ、前記支持部材を貫通した端部に前記中空部に連通するドレン通路が設けられることを特徴としている。   In the stator blade according to the present invention, the stator blade main body is provided with a hollow portion penetrating in a longitudinal direction, and a drain passage communicating with the hollow portion is provided at an end portion penetrating the support member.

従って、静翼本体の中空部に対応してドレン通路が連通して設けられることで、静翼本体の中空部で発生したドレン水をドレン通路から容易に排出することができる。   Therefore, by providing the drain passage in communication with the hollow portion of the stationary blade body, the drain water generated in the hollow portion of the stationary blade body can be easily discharged from the drain passage.

また、本発明の静翼ユニットは、前記支持部材同士が連結されることで、前記静翼がリング形状に組付けられて構成される、ことを特徴とするものである。   Moreover, the stationary blade unit of the present invention is characterized in that the stationary blade is assembled in a ring shape by connecting the support members.

従って、静翼は、静翼本体の端部の周囲に複数の分割体が配置され、複数の分割体同士が溶接部により連結されると共に、静翼本体の端部と各分割体が開先溶接により連結されて構成されている。支持部材を複数の分割体から構成することで、静翼が湾曲形状をなすと共に周方向に捩じられた3次元形状であっても、静翼本体の端部と各分割体を隙間なく適正に連結することができる。そして、開先溶接を実施可能であることから、通路側への溶接部の突出を抑制して蒸気流れを妨げることがない。また、複数の静翼をリング形状に組付けることで、容易に静翼ユニットを構成することができる。その結果、通路側への突出部を抑制して性能の向上を図ることができると共に、組付を容易として作業性の向上を図ることができる。   Accordingly, the stationary blade has a plurality of divided bodies arranged around the end portion of the stationary blade body, the plurality of divided bodies are connected to each other by the welded portion, and the end portion of the stationary blade body and each divided body are grooved. They are connected by welding. By configuring the support member from a plurality of divided bodies, even if the stationary blade has a curved shape and a three-dimensional shape that is twisted in the circumferential direction, the end of the stationary blade body and each divided body are properly arranged without gaps. Can be linked to. And since groove welding can be implemented, the protrusion of the welding part to the channel | path side is suppressed and a steam flow is not prevented. Moreover, a stationary blade unit can be easily configured by assembling a plurality of stationary blades into a ring shape. As a result, it is possible to improve the performance by suppressing the protruding portion to the passage side, and to improve the workability by facilitating the assembly.

また、本発明の蒸気タービンは、ケーシングと、前記ケーシング内に回転自在に支持されたロータと、動翼の基端部が前記ロータに支持されて前記ロータの周方向に所定間隔で複数配置される複数段の動翼ユニットと、静翼の基端部と先端部が前記ケーシングに支持されて前記ロータの周方向に所定間隔で複数配置される複数段の静翼動翼ユニットと、を有し、前記複数段の静翼ユニットのうちの最終段の静翼ユニットとして前記静翼ユニットが適用される、ことを特徴とするものである。   The steam turbine according to the present invention includes a casing, a rotor rotatably supported in the casing, and a plurality of base end portions of the moving blades supported by the rotor and arranged at predetermined intervals in the circumferential direction of the rotor. A plurality of stages of moving blade units, and a plurality of stages of stationary blade moving blade units that are supported by the casing and arranged at a predetermined interval in the circumferential direction of the rotor. However, the stationary blade unit is applied as a final-stage stationary blade unit among the plurality of stages of stationary blade units.

従って、通路側への突出部を抑制して性能の向上を図ることができると共に、組付を容易として作業性の向上を図ることができる。   Therefore, it is possible to improve the performance by suppressing the protruding portion to the passage side, and to improve the workability by facilitating the assembly.

本発明の静翼、静翼ユニット、蒸気タービンによれば、静翼本体とその端部が貫通して固定される支持部材から静翼を構成し、支持部材を複数の分割体から構成し、複数の分割体同士の間に溶接部を設けると共に、静翼本体の端部と分割体との間に開先溶接部を設けるので、通路側への突出部を抑制して性能の向上を図ることができると共に、組付を容易として作業性の向上を図ることができる。   According to the stationary blade, the stationary blade unit, and the steam turbine of the present invention, the stationary blade body is configured from a supporting member that is fixed by penetrating the stationary blade body, and the supporting member is configured by a plurality of divided bodies. Since the welded portion is provided between the plurality of divided bodies and the groove welded portion is provided between the end portion of the stationary blade body and the divided body, the projecting portion to the passage side is suppressed and the performance is improved. In addition, it is possible to improve the workability by facilitating the assembly.

図1は、本実施形態の蒸気タービンにおける静翼ユニットを表す概略図である。FIG. 1 is a schematic diagram illustrating a stationary blade unit in the steam turbine of the present embodiment. 図2は、静翼の分解状態を表す概略図である。FIG. 2 is a schematic diagram illustrating a disassembled state of the stationary blade. 図3は、静翼の組立状態を表す概略図である。FIG. 3 is a schematic view showing an assembled state of the stationary blade. 図4は、静翼と分割環との連結部を表す断面図である。FIG. 4 is a cross-sectional view illustrating a connecting portion between the stationary blade and the split ring. 図5は、本実施形態の蒸気タービンを表す概略構成図である。FIG. 5 is a schematic configuration diagram illustrating the steam turbine of the present embodiment.

以下に添付図面を参照して、本発明に係る静翼、静翼ユニット、蒸気タービンの好適な実施形態を詳細に説明する。なお、この実施形態により本発明が限定されるものではなく、また、実施形態が複数ある場合には、各実施形態を組み合わせて構成するものも含むものである。   Exemplary embodiments of a stationary blade, a stationary blade unit, and a steam turbine according to the present invention will be described below in detail with reference to the accompanying drawings. In addition, this invention is not limited by this embodiment, and when there are two or more embodiments, what comprises combining each embodiment is also included.

図5は、本実施形態の蒸気タービンを表す概略構成図である。   FIG. 5 is a schematic configuration diagram illustrating the steam turbine of the present embodiment.

蒸気タービンにおいて、図5に示すように、ケーシング11は、中空形状をなし、ロータ12が複数の軸受13により回転自在に支持されている。このロータ12は、ケーシング11の内部にて、外周部に軸方向に所定間隔で動翼ユニット14が複数設けられている。この動翼ユニット14は、ロータ12の外周部に軸方向に所定間隔で設けられた複数のディスク15と、各ディスク15の外周部に周方向に沿って固定される複数の動翼16により構成されている。   In the steam turbine, as shown in FIG. 5, the casing 11 has a hollow shape, and the rotor 12 is rotatably supported by a plurality of bearings 13. In the rotor 12, a plurality of blade units 14 are provided at predetermined intervals in the axial direction on the outer peripheral portion inside the casing 11. The blade unit 14 includes a plurality of disks 15 provided at predetermined intervals in the axial direction on the outer periphery of the rotor 12 and a plurality of blades 16 fixed to the outer periphery of each disk 15 along the circumferential direction. Has been.

また、ケーシング11は、内部にて、ロータ12の軸方向に所定間隔で静翼ユニット17が複数設けられている。この静翼ユニット17は、ロータ12の外周部に軸方向に所定間隔で配置される複数の外輪18及び内輪19と、各外輪18と各内輪19とを連結するように周方向に沿って固定される複数の静翼20により構成されている。このように、動翼ユニット14と静翼ユニット17は、ロータ12における軸方向に交互に配置されている。   The casing 11 is provided with a plurality of stationary blade units 17 at predetermined intervals in the axial direction of the rotor 12. The stationary blade unit 17 is fixed along the circumferential direction so as to connect a plurality of outer rings 18 and inner rings 19 arranged at predetermined intervals in the axial direction on the outer peripheral portion of the rotor 12, and the outer rings 18 and the inner rings 19. The plurality of stationary blades 20 are configured. Thus, the moving blade units 14 and the stationary blade units 17 are alternately arranged in the axial direction of the rotor 12.

また、ケーシング11は、この複数の動翼ユニット14と複数の静翼ユニット17が配設される通路に蒸気通路21が形成されている。そして、ケーシング11は、蒸気通路21に連通する蒸気供給口22と蒸気排出口23が設けられている。   Further, the casing 11 has a steam passage 21 formed in a passage in which the plurality of moving blade units 14 and the plurality of stationary blade units 17 are disposed. The casing 11 is provided with a steam supply port 22 and a steam discharge port 23 that communicate with the steam passage 21.

従って、蒸気が蒸気供給口22から蒸気通路21に供給されると、この蒸気は、複数の動翼ユニット14及び静翼ユニット17を通過することで、各動翼ユニット14を介してロータ12を駆動回転することができる。このロータ12は、図示しない発電機が連結されており、発電機を駆動して発電することができる。   Therefore, when steam is supplied from the steam supply port 22 to the steam passage 21, the steam passes through the plurality of blade units 14 and the stationary blade unit 17, thereby passing through the rotor 12 via each blade unit 14. It can be driven and rotated. The rotor 12 is connected to a generator (not shown), and can drive the generator to generate power.

本実施形態にて、図1に示すように、静翼20は、静翼本体31と、この静翼本体31の先端部が貫通して固定される分割環(支持部材)32と、静翼本体31の基端部が貫通して固定されるシュラウド(支持部材)33を有している。そして、複数の分割環32がリング状に連結されることで外輪18が構成され、複数のシュラウド33がリング状に連結されることで内輪19が構成されることから、静翼ユニット17は、静翼20がリング形状に組付けられて構成される。   In the present embodiment, as shown in FIG. 1, the stationary blade 20 includes a stationary blade body 31, a split ring (support member) 32 to which a tip portion of the stationary blade body 31 is fixed, and a stationary blade. A base end portion of the main body 31 has a shroud (supporting member) 33 that passes through and is fixed. Then, the outer ring 18 is configured by connecting the plurality of split rings 32 in a ring shape, and the inner ring 19 is configured by connecting the plurality of shrouds 33 in a ring shape. The stationary blade 20 is assembled in a ring shape.

そして、分割環32とシュラウド33は、複数の分割体から構成され、複数の分割体同士がレーザ溶接により連結されると共に、静翼本体31の端部と各分割体とが開先溶接により連結される。   And the division | segmentation ring 32 and the shroud 33 are comprised from the some division body, and while the some division body is connected by laser welding, the edge part of the stationary blade main body 31 and each division body are connected by groove welding. Is done.

即ち、図2に示すように、静翼本体31の先端部と分割環32との連結構造において、静翼本体31は、板金プレス加工により形成された背側プレート41と腹側プレート42とが溶接より連結されている。背側プレート41と腹側プレート42は、各前縁部が溶接により連結されて前縁溶接部43が設けられ、各後縁部が溶接により連結されて後縁溶接部44が設けられることで、静翼本体31が翼形状をなして構成されている。ここで、静翼本体31は板金による製造の他に、例えば、鋳造や削り出しにより製造されてもよい。   That is, as shown in FIG. 2, in the connection structure between the tip of the stationary blade body 31 and the split ring 32, the stationary blade body 31 is welded to the back side plate 41 and the abdominal side plate 42 formed by sheet metal pressing. More connected. The back side plate 41 and the abdominal side plate 42 are connected to each front edge portion by welding to provide a front edge weld portion 43, and each rear edge portion is connected to each other by welding to provide a rear edge weld portion 44. The stationary blade body 31 is configured to have a blade shape. Here, the stationary blade body 31 may be manufactured by casting or cutting, for example, in addition to manufacturing by sheet metal.

分割環32は、静翼本体31における背側プレート41側に配置される第1分割体51と、静翼本体31における腹側プレート42側に配置される第2分割体52と、静翼本体31の後縁部31a側に配置される第3分割体53とを有している。第1分割体51は、背側プレート41における前縁部側に沿って凹状に湾曲して第1連結部51aが形成されると共に、この第1連結部51aの厚さ方向に対して斜めに形成される第1開先部51bが形成されている。第2分割体52は、腹側プレート42における前縁部側に沿って凸状に湾曲して第2連結部52aが形成されると共に、この第2連結部52aの厚さ方向に対して斜めに形成される第2開先部52bが形成されている。第3分割体53は、背側プレート41及び腹側プレート42における後縁部31a側に沿って2個の第3連結部53a,53bからなるV字形状部54が設けられると共に、この第3連結部53a,53bの厚さ方向に対して斜めに形成される第3開先部53c,53dが形成されている。なお、第3連結部53a,53bは、第3開先部53c,53dが途中まで形成され、後縁部41aに対応したV字形状部54の交差部54aには開先部が形成されていない。   The split ring 32 includes a first divided body 51 disposed on the back plate 41 side in the stationary blade body 31, a second divided body 52 disposed on the ventral plate 42 side in the stationary blade body 31, and the stationary blade body. 31 and a third divided body 53 disposed on the rear edge portion 31a side. The first divided body 51 is concavely curved along the front edge portion side of the back side plate 41 to form a first connecting portion 51a, and obliquely with respect to the thickness direction of the first connecting portion 51a. A first groove 51b to be formed is formed. The second divided body 52 is curved in a convex shape along the front edge portion side of the ventral plate 42 to form a second connecting portion 52a, and is inclined with respect to the thickness direction of the second connecting portion 52a. A second groove portion 52b is formed. The third divided body 53 is provided with a V-shaped portion 54 including two third connecting portions 53a and 53b along the rear edge portion 31a side of the back side plate 41 and the ventral side plate 42. Third groove portions 53c and 53d formed obliquely with respect to the thickness direction of the coupling portions 53a and 53b are formed. Note that the third connecting portions 53a and 53b have third groove portions 53c and 53d formed partway, and a groove portion is formed at the intersecting portion 54a of the V-shaped portion 54 corresponding to the rear edge portion 41a. Absent.

第1分割体51と第2分割体52は、対向する位置に連結面55a,56aが形成され、第1分割体51と第3分割体53は、対向する位置に連結面55b,57aが形成され、第2分割体52と第3分割体53は、対向する位置に連結面56b,57bが形成されている。また、第1分割体51は、第1開先部51bとは反対側に隣接する分割環32との連結面55c,55dが形成されている。第2分割体52は、第2開先部52bとは反対側に隣接する分割環32との連結面56cが形成され、連結面56b,56cが直線状に設けられている。第3分割体53は、第3開先部53c,53d側に隣接する分割環32との連結面57cが形成されると共に、第3開先部53c,53dとは反対側に隣接する分割環32との連結面57d,57eが形成されている。なお、第3分割体53は、連結面57a,57cが直線状に設けられている。   The first divided body 51 and the second divided body 52 are formed with connecting surfaces 55a and 56a at opposing positions, and the first divided body 51 and the third divided body 53 are formed with connecting surfaces 55b and 57a at opposed positions. In addition, the second divided body 52 and the third divided body 53 have connection surfaces 56b and 57b formed at opposing positions. Moreover, the 1st division body 51 has the connection surfaces 55c and 55d with the division | segmentation ring 32 adjacent on the opposite side to the 1st groove part 51b. In the second divided body 52, a connection surface 56c with the adjacent split ring 32 is formed on the side opposite to the second groove portion 52b, and the connection surfaces 56b and 56c are linearly provided. The third split body 53 is formed with a connecting surface 57c with the split ring 32 adjacent to the third groove portions 53c and 53d, and the split ring adjacent to the opposite side of the third groove portions 53c and 53d. The connection surfaces 57d and 57e with 32 are formed. In addition, as for the 3rd division body 53, the connection surfaces 57a and 57c are provided in linear form.

そして、静翼20は、図3及び図4に示すように、静翼本体31の端部の周囲に各分割体51,52,53が配置され、複数の分割体51,52,53同士がレーザ溶接により連結されると共に、静翼本体31の端部と各分割体51,52,53とが開先溶接により連結される。即ち、静翼20は、静翼本体31の端部の外周面に各分割体51,52,53の連結部51a,52a,53a,53bが密着する。また、第1分割体51と第2分割体52は、連結面55a,56aにより密着し、第1分割体51と第3分割体53は、連結面55b,57aにより密着し、第2分割体52と第3分割体53は、連結面56b,57bにより密着する。   As shown in FIGS. 3 and 4, the stationary blade 20 has the divided bodies 51, 52, 53 arranged around the end portion of the stationary blade body 31, and the plurality of divided bodies 51, 52, 53 are connected to each other. While being connected by laser welding, the end part of the stationary blade body 31 and each divided body 51, 52, 53 are connected by groove welding. That is, in the stationary blade 20, the connection portions 51 a, 52 a, 53 a, and 53 b of the divided bodies 51, 52, and 53 are in close contact with the outer peripheral surface of the end portion of the stationary blade body 31. Further, the first divided body 51 and the second divided body 52 are in close contact with each other through the connecting surfaces 55a and 56a, and the first divided body 51 and the third divided body 53 are in close contact with each other through the connecting surfaces 55b and 57a. 52 and the 3rd division body 53 adhere | attach by connection surface 56b, 57b.

この状態で、第1分割体51と第2分割体52は、連結面55a,56aがレーザ溶接(レーザ溶接部61)により連結され、第1分割体51と第3分割体53は、連結面55b,57aがレーザ溶接(レーザ溶接部62)により連結され、第2分割体52と第3分割体53は、連結面56b,57bがレーザ溶接(レーザ溶接部63)により連結される。また、静翼本体31の外周面と第1分割体51の第1開先部51bが開先溶接(開先溶接部71)により連結される。静翼本体31の外周面と第2分割体52の第2開先部52bが開先溶接(開先溶接部72)により連結される。静翼本体31の外周面と第3分割体53の第3開先部53c,53dが開先溶接(開先溶接部73,74)により連結される。このとき、静翼本体31の後縁部31aと第3分割体53の交差部54aは、開先溶接されることはなく、非開先溶接部75が設けられる。   In this state, the connection surfaces 55a and 56a of the first divided body 51 and the second divided body 52 are connected by laser welding (laser welding portion 61), and the first divided body 51 and the third divided body 53 are connected to each other. 55b and 57a are connected by laser welding (laser welding part 62), and the connection surfaces 56b and 57b of the second divided body 52 and the third divided body 53 are connected by laser welding (laser welding part 63). Moreover, the outer peripheral surface of the stationary blade body 31 and the first groove portion 51b of the first divided body 51 are connected by groove welding (groove welding portion 71). The outer peripheral surface of the stationary blade body 31 and the second groove portion 52b of the second divided body 52 are connected by groove welding (groove welding portion 72). The outer peripheral surface of the stationary blade body 31 and the third groove portions 53c and 53d of the third divided body 53 are connected by groove welding (groove weld portions 73 and 74). At this time, the rear edge portion 31a of the stationary blade body 31 and the intersecting portion 54a of the third divided body 53 are not groove-welded, and the non-groove weld portion 75 is provided.

各分割体51,52,53が連結される分割環32は、複数リング状に連結されて外輪18が構成される。即ち、第1分割体51は、一方側に隣接する分割環32の第2分割体52と連結面55c,56cが密着して溶接により連結されると共に、第3分割体53と連結面55c,57eが密着して溶接により連結される。第2分割体52は、他方側に隣接する分割環32の第1分割体51と連結面55c,56cが密着して溶接により連結される。第3分割体53は、一方側に隣接する分割環32の第3分割体53と連結面57c,57dが密着して溶接により連結され、他方側に隣接する分割環32の第3分割体53と連結面57c,57dが密着して溶接により連結されると共に、第1分割体51と連結面55d,57eが密着して溶接により連結される。   The split ring 32 to which the respective divided bodies 51, 52, 53 are connected is connected in a plurality of rings to form the outer ring 18. That is, the first divided body 51 is connected to the second divided body 52 of the divided ring 32 adjacent to one side and the connection surfaces 55c and 56c by close contact, and is connected by welding, and the third divided body 53 and the connection surface 55c, 57e comes into close contact and is connected by welding. In the second divided body 52, the first divided body 51 and the connecting surfaces 55c, 56c of the divided ring 32 adjacent to the other side are in close contact with each other and connected by welding. In the third divided body 53, the third divided body 53 of the divided ring 32 adjacent to one side and the connection surfaces 57c, 57d are in close contact and connected by welding, and the third divided body 53 of the divided ring 32 adjacent to the other side is connected. And the connecting surfaces 57c and 57d are in close contact and connected by welding, and the first divided body 51 and the connecting surfaces 55d and 57e are in close contact and connected by welding.

ここで、静翼本体31と各分割体51,52,53を連結する各種の溶接は、蒸気通路21(図1参照)側から実施される。   Here, the various welding which connects the stationary blade body 31 and each division body 51,52,53 is implemented from the steam channel 21 (refer FIG. 1) side.

また、静翼20は、図1に示すように、静翼本体31の端部が分割環32(外輪18)を貫通し、所定長さだけ突出してこの分割環32に固定される。分割環32は、両側のフランジ部32aを介して蓋プレート81が複数のボルト82により固定された箱型形状をなし、静翼本体31の端部が蓋プレート81に当接している。この蓋プレート81は、ドレン通路83が設けられている。そして、静翼本体31は、長手方向に貫通する中空部45が設けられ、この中空部45は、蓋プレート81に形成された貫通孔81aを介してドレン通路83に連通している。   Further, as shown in FIG. 1, the stationary blade 20 has an end portion of the stationary blade body 31 that passes through the split ring 32 (outer ring 18), protrudes a predetermined length, and is fixed to the split ring 32. The split ring 32 has a box shape in which the lid plate 81 is fixed by a plurality of bolts 82 via the flange portions 32 a on both sides, and the end portion of the stationary blade body 31 is in contact with the lid plate 81. The lid plate 81 is provided with a drain passage 83. The stationary blade body 31 is provided with a hollow portion 45 penetrating in the longitudinal direction, and the hollow portion 45 communicates with the drain passage 83 through a through hole 81 a formed in the lid plate 81.

なお、ここでは、静翼20にて、静翼本体31の先端部と分割環32との連結構造について説明したが、静翼本体31の基端部とシュラウド33との連結構造についてもほぼ同様の構成となっている。   Here, the connection structure between the distal end portion of the stationary blade body 31 and the split ring 32 in the stationary blade 20 has been described, but the connection structure between the proximal end portion of the stationary blade body 31 and the shroud 33 is substantially the same. It becomes the composition of.

このように本実施形態の静翼にあっては、静翼本体31の端部が分割環32(シュラウド33)に貫通して固定されて構成される静翼20であって、分割環32は、静翼本体31の端部の周囲に配置される複数の分割体51,52,53から構成され、複数の分割体51,52,53同士の間にレーザ溶接部61,62,63が設けられると共に、静翼本体31の端部と分割体51,52,53との間に開先溶接部71,72,73,74が設けられている。   As described above, in the stationary blade of the present embodiment, the stationary blade main body 31 is the stationary blade 20 that is configured such that the end portion of the stationary blade body 31 penetrates and is fixed to the split ring 32 (the shroud 33). The plurality of divided bodies 51, 52, 53 are arranged around the end of the stationary blade body 31, and laser welded portions 61, 62, 63 are provided between the plurality of divided bodies 51, 52, 53. In addition, groove welds 71, 72, 73, 74 are provided between the end of the stationary blade body 31 and the divided bodies 51, 52, 53.

従って、分割環32を複数の分割体51,52,53から構成することで、静翼本体31が湾曲形状をなすと共に周方向に捩じられた3次元形状であっても、静翼本体31の端部と各分割体51,52,53を隙間なく適正に密着させることができ、静翼本体31の端部と各分割体51,52,53を高精度に連結することができる。そして、静翼本体31の端部と各分割体51,52,53とが適正に密着することから、両者間で開先溶接を実施することができ、蒸気通路21側への開先溶接部71,72,73,74の突出を抑制することができ、蒸気通路21を流れる蒸気流れを妨げることがない。その結果、蒸気通路21側への開先溶接部71,72,73,74の突出量を抑制して静翼20の性能を向上することができると共に、静翼20の組付を容易として作業性を向上することができる。   Accordingly, by forming the split ring 32 from the plurality of split bodies 51, 52, 53, even if the stationary blade body 31 has a curved shape and a three-dimensional shape twisted in the circumferential direction, the stationary blade body 31 The end portions of the stationary blade main body 31 and the respective divided bodies 51, 52, 53 can be connected to each other with high accuracy. And since the edge part of the stationary blade body 31 and each division | segmentation body 51,52,53 contact | adhere closely, groove welding can be implemented between both, and the groove welding part to the steam channel 21 side is carried out. The protrusion of 71, 72, 73, 74 can be suppressed, and the steam flow flowing through the steam passage 21 is not hindered. As a result, it is possible to improve the performance of the stationary blade 20 by suppressing the protruding amount of the groove welds 71, 72, 73, 74 to the steam passage 21 side, and to facilitate the assembly of the stationary blade 20. Can be improved.

本実施形態の静翼では、複数の分割体51,52,53における静翼本体31との連結部51a,52a,53a,53bに開先部51b,52b,53c,53dを設けている。従って、静翼本体31の外面形状に応じて各分割体51,52,53における静翼本体31との連結部51a,52a,53a,53bに最適形状の開先部51b,52b,53c,53dを設けることができ、静翼本体31と分割体51,52,53を高精度に開先溶接することができる。   In the stationary blade of the present embodiment, groove portions 51b, 52b, 53c, and 53d are provided in the connecting portions 51a, 52a, 53a, and 53b of the plurality of divided bodies 51, 52, and 53 with the stationary blade body 31. Therefore, the groove portions 51b, 52b, 53c, 53d of the optimum shape are connected to the connecting portions 51a, 52a, 53a, 53b of the divided bodies 51, 52, 53 with the stationary blade body 31 according to the outer surface shape of the stationary blade body 31. Can be provided, and the stator blade body 31 and the divided bodies 51, 52, 53 can be groove-welded with high accuracy.

本実施形態の静翼では、複数の分割体51,52,53における開先部51b,52b,53c,53dとは反対側に、隣接する分割環32との連結面55b,55c,56c,57c,57d,57eを設けている。従って、静翼本体31の端部に各分割体51,52,53が開先溶接により連結されて構成された静翼20は、連結面55b,55c,56c,57c,57d,57eを介して隣接する静翼20の分割環32と連結されることとなり、各静翼20(各分割環32)同士を高精度に連結することができる。   In the stationary blade of the present embodiment, the connecting surfaces 55b, 55c, 56c, 57c with the adjacent split ring 32 on the opposite side to the groove portions 51b, 52b, 53c, 53d in the plurality of split bodies 51, 52, 53. , 57d, 57e. Therefore, the stationary blade 20 configured by connecting the divided bodies 51, 52, 53 to the end portion of the stationary blade body 31 by groove welding is provided via the connection surfaces 55b, 55c, 56c, 57c, 57d, 57e. It will be connected with the division | segmentation ring 32 of the adjacent stator blade 20, and each stator blade 20 (each division | segmentation ring 32) can be connected with high precision.

本実施形態の静翼では、複数の分割体として、静翼本体31の背側に配置される第1分割体51と、静翼本体31の腹側に配置される第2分割体52と、静翼本体31の後縁部31a側に配置される第3分割体53とを設けている。従って、3次元形状をなす静翼本体31の端部に対して3個の分割体51,52,53を適正に密着させて連結することができ、組付性を向上することができる。   In the stationary blade of the present embodiment, as a plurality of divided bodies, a first divided body 51 disposed on the back side of the stationary blade body 31, a second divided body 52 disposed on the ventral side of the stationary blade body 31, A third divided body 53 disposed on the rear edge portion 31a side of the stationary blade body 31 is provided. Therefore, the three divided bodies 51, 52, and 53 can be appropriately brought into close contact with the end of the stationary blade body 31 having a three-dimensional shape, and the assemblability can be improved.

本実施形態の静翼では、第3分割体53に2個の連結部53a,53bからなるV字形状部54を設け、2個の連結部53a,53bの交差部54aに非開先溶接部75を設けている。従って、静翼本体31の端部と第3分割体53におけるV字形状部54の交差部54aとは、開先溶接しないことから、静翼本体31の端部における後縁部31aの溶接熱により形状変形(溶融)を抑制することができる。   In the stationary blade of the present embodiment, the V-shaped portion 54 including the two connecting portions 53a and 53b is provided in the third divided body 53, and the non-groove welded portion is provided at the intersecting portion 54a of the two connecting portions 53a and 53b. 75 is provided. Accordingly, since the end portion of the stationary blade body 31 and the intersecting portion 54a of the V-shaped portion 54 in the third divided body 53 are not groove-welded, the welding heat of the trailing edge portion 31a at the end portion of the stationary blade body 31 Therefore, shape deformation (melting) can be suppressed.

本実施形態の静翼では、静翼本体31の端部を分割環32(シュラウド33)より突出して配置している。従って、静翼本体31の端部の長さ方向における所定の位置に各分割体51,52,53を固定すればよく、静翼本体31の端部の位置を位置決めする必要がない。静翼本体31は、板金プレス加工により形成された背側プレート41と腹側プレート42とを溶接より連結して製造しているが、このとき、各プレート41,42の長さを高精度に製造する必要はなく、製造コストを低減することができる。   In the stationary blade of the present embodiment, the end portion of the stationary blade body 31 is disposed so as to protrude from the split ring 32 (the shroud 33). Therefore, it is only necessary to fix each of the divided bodies 51, 52, 53 at a predetermined position in the length direction of the end portion of the stationary blade body 31, and it is not necessary to position the end portion of the stationary blade body 31. The stationary blade body 31 is manufactured by connecting the back side plate 41 and the abdominal side plate 42 formed by sheet metal press working by welding. At this time, the length of each plate 41, 42 is manufactured with high accuracy. It is not necessary to reduce the manufacturing cost.

本実施形態の静翼では、静翼本体31に長手方向に貫通する中空部45を設け、分割環32を貫通した端部に中空部45に連通するドレン通路83を設けている。従って、静翼本体31の中空部45に対応してドレン通路83が連通して設けられることで、静翼本体31の中空部45で発生したドレン水をドレン通路83から容易に外部に排出することができる。   In the stationary blade of the present embodiment, a hollow portion 45 penetrating in the longitudinal direction is provided in the stationary blade body 31, and a drain passage 83 communicating with the hollow portion 45 is provided at an end portion that penetrates the split ring 32. Accordingly, the drain passage 83 is provided so as to communicate with the hollow portion 45 of the stationary blade body 31, so that drain water generated in the hollow portion 45 of the stationary blade body 31 is easily discharged from the drain passage 83 to the outside. be able to.

また、本実施形態の静翼ユニットにあっては、複数の分割環32をリング状に連結して外輪18とすると共に、複数のシュラウド33をリング状に連結して内輪19とし、静翼20をリング形状として構成し、分割環32(シュラウド33)を複数の分割体51,52,53により構成している。従って、静翼本体31の端部と各分割体51,52,53を隙間なく適正に密着させることができ、静翼本体31の端部と各分割体51,52,53を高精度に連結することができる。そして、静翼本体31の端部と各分割体51,52,53とを開先溶接により連結することができ、蒸気通路21側への開先溶接部71,72,73,74の突出を抑制することができ、蒸気通路21を流れる蒸気流れを妨げることがない。その結果、蒸気通路21側への開先溶接部71,72,73,74の突出量を抑制して静翼20の性能を向上することができると共に、静翼20の組付を容易として作業性を向上することができる。   In the stationary blade unit of the present embodiment, the plurality of split rings 32 are connected in a ring shape to form the outer ring 18, and the plurality of shrouds 33 are connected in a ring shape to form the inner ring 19, and the stationary blade 20. Is configured as a ring shape, and the split ring 32 (the shroud 33) is configured by a plurality of split bodies 51, 52, 53. Therefore, the end portion of the stationary blade body 31 and each of the divided bodies 51, 52, 53 can be properly adhered without gaps, and the end portion of the stationary blade body 31 and each of the divided bodies 51, 52, 53 are connected with high accuracy. can do. And the edge part of the stationary blade main body 31 and each division body 51,52,53 can be connected by groove welding, and the protrusion of the groove welding parts 71,72,73,74 to the steam channel 21 side is made. It can suppress and does not disturb the steam flow which flows through the steam passage 21. As a result, it is possible to improve the performance of the stationary blade 20 by suppressing the protruding amount of the groove welds 71, 72, 73, 74 to the steam passage 21 side, and to facilitate the assembly of the stationary blade 20. Can be improved.

また、本実施形態の蒸気タービンにあっては、ケーシング11と、ケーシング11内に回転自在に支持されたロータ12と、動翼16の基端部がロータ12に支持されてロータ12の周方向に所定間隔で複数配置される複数段の動翼ユニット14と、静翼20の基端部と先端部がケーシング11に支持されてロータ12の周方向に所定間隔で複数配置される複数段の静翼ユニット17とを設け、複数段の静翼ユニット17のうちの最終段の静翼ユニット17として上述した静翼ユニットを適用している。   Further, in the steam turbine of the present embodiment, the casing 11, the rotor 12 rotatably supported in the casing 11, and the base end portion of the moving blade 16 are supported by the rotor 12, so that the circumferential direction of the rotor 12 is A plurality of stages of moving blade units 14 arranged at a predetermined interval on each other, and a plurality of stages arranged at a predetermined interval in the circumferential direction of the rotor 12 with the base end portion and the tip end portion of the stationary blade 20 supported by the casing 11. The stationary blade unit 17 is provided, and the above-described stationary blade unit is applied as the final stage stationary blade unit 17 of the plurality of stages of stationary blade units 17.

従って、蒸気通路21側への開先溶接部71,72,73,74の突出量を抑制して静翼20の性能を向上することができると共に、静翼20の組付を容易として作業性を向上することができる。   Accordingly, it is possible to improve the performance of the stationary blade 20 by suppressing the protruding amount of the groove welds 71, 72, 73, 74 to the steam passage 21 side, and to facilitate the assembly of the stationary blade 20 and to improve the workability. Can be improved.

なお、上述した実施形態にて、分割環32(シュラウド33)を静翼本体31における背側プレート41側に配置される第1分割体51と、静翼本体31における腹側プレート42側に配置される第2分割体52と、静翼本体31の後縁部31a側に配置される第3分割体53とから構成したが、この構成に限定されるものではない。即ち、分割体の分割位置は、実施形態に限定されずにどの位置で分割してもよい。また、分割体の分割数は、実施形態(3個)に限定されずに2個または4個以上としてもよい。   In the embodiment described above, the split ring 32 (the shroud 33) is disposed on the first split body 51 disposed on the back plate 41 side of the stationary blade body 31 and on the ventral plate 42 side of the stationary blade body 31. The second divided body 52 and the third divided body 53 arranged on the rear edge portion 31a side of the stationary blade body 31 are configured, but the present invention is not limited to this configuration. That is, the division position of the divided body is not limited to the embodiment, and may be divided at any position. Further, the number of divisions of the divided body is not limited to the embodiment (three), and may be two or four or more.

また、上述した実施形態では、静翼本体31の端部を分割環32(シュラウド33)から突出して連結したが、この構成に限定されるものではない。例えば、静翼本体31の端部を分割環32(シュラウド33)の内面と同じ位置に連結してもよい。即ち、静翼本体31の端部を分割環32(シュラウド33)から突出させなくてもよい。   In the above-described embodiment, the end portion of the stationary blade body 31 protrudes from the split ring 32 (the shroud 33) and is connected, but the configuration is not limited to this. For example, the end of the stationary blade body 31 may be connected to the same position as the inner surface of the split ring 32 (the shroud 33). That is, the end portion of the stationary blade body 31 may not protrude from the split ring 32 (the shroud 33).

また、上述した実施形態では、本発明の静翼及び静翼ユニットを蒸気タービンの最終段の静翼及び静翼ユニットに適用したが、その他の静翼及び静翼ユニットに適用してもよい。   Further, in the above-described embodiment, the stationary blade and the stationary blade unit of the present invention are applied to the stationary blade and the stationary blade unit in the final stage of the steam turbine, but may be applied to other stationary blades and the stationary blade unit.

11 ケーシング
12 ロータ
13 軸受
14 動翼ユニット
15 ディスク
16 動翼
17 静翼ユニット
18 外輪
19 内輪
20 静翼
21 蒸気通路
31 静翼本体
31a 後縁部
32 分割環(支持部材)
33 シュラウド(支持部材)
41 背側プレート
42 腹側プレート
51 第1分割体
51a 第1連結部
51b 第1開先部
52 第2分割体
52a 第2連結部
52b 第2開先部
53 第3分割体
53a,53b 第3連結部
53c,53d 第3開先部
54 V字形状部
54a 交差部
55a,55b,55c,55d,56a,56b,56c,57a,57b,57c,57d,57e 連結面(連結部)
61,62,63 レーザ溶接部
71,72,73,74 開先溶接部
75 非開先溶接部
83 ドレン通路
DESCRIPTION OF SYMBOLS 11 Casing 12 Rotor 13 Bearing 14 Rotor unit 15 Disc 16 Rotor blade 17 Stator blade unit 18 Outer ring 19 Inner ring 20 Stator blade 21 Steam passage 31 Stator blade main body 31a Rear edge part 32 Split ring (support member)
33 Shroud (support member)
41 Back side plate 42 Ventral side plate 51 1st division body 51a 1st connection part 51b 1st groove part 52 2nd division body 52a 2nd connection part 52b 2nd groove part 53 3rd division body 53a, 53b 3rd Connection part 53c, 53d 3rd groove part 54 V-shaped part 54a Intersection part 55a, 55b, 55c, 55d, 56a, 56b, 56c, 57a, 57b, 57c, 57d, 57e Connection surface (connection part)
61, 62, 63 Laser weld 71, 72, 73, 74 Groove weld 75 Non-groove weld 83 Drain passage

Claims (8)

静翼本体と、
前記静翼本体の端部が貫通して固定される支持部材と、
を有し、
前記支持部材は、前記静翼本体の端部の周囲に配置される複数の分割体から構成され、
前記複数の分割体同士の間に溶接部が設けられると共に、
前記静翼本体の端部と前記分割体との間に開先溶接部が設けられ、
前記複数の分割体は、前記静翼本体の背側に配置される第1分割体と、前記静翼本体の腹側に配置される第2分割体と、前記静翼本体の後縁部側に配置される第3分割体とを有する
ことを特徴とする静翼。
A stationary blade body,
A support member through which an end of the stationary blade body is fixed, and
Have
The support member is composed of a plurality of divided bodies arranged around the end of the stationary blade body,
While a weld is provided between the plurality of divided bodies,
Groove weld provided we are between the dividing member and the end portion of the stationary blade body,
The plurality of divided bodies include a first divided body disposed on the back side of the stationary blade body, a second divided body disposed on the ventral side of the stationary blade body, and a rear edge portion side of the stationary blade body. A third divided body arranged in
A stationary blade characterized by that.
前記複数の分割体は、前記静翼本体との連結部に開先部が設けられることを特徴とする請求項1に記載の静翼。   The stationary blade according to claim 1, wherein the plurality of divided bodies are provided with a groove portion at a connection portion with the stationary blade body. 前記複数の分割体は、前記開先部とは反対側の面に、隣接する前記支持部材との連結部が設けられることを特徴とする請求項2に記載の静翼。   The stationary blade according to claim 2, wherein the plurality of divided bodies are provided with a connecting portion with the adjacent support member on a surface opposite to the groove portion. 前記第3分割体は、2個の連結部からなるV字形状部が設けられ、前記2個の連結部の交差部に非開先溶接部が設けられることを特徴とする請求項1から請求項3のいずれか一項に記載の静翼。 The third split body, V-shaped section consisting of two coupling parts is provided, according claim 1, characterized in that HiHiraku destination weld portion is provided at the intersection of the two connecting portions Item 4. The stator blade according to any one of Items 3 to 3 . 前記静翼本体の端部が前記支持部材より突出して配置されることを特徴とする請求項1から請求項4のいずれか一項に記載の静翼。 The stationary blade according to any one of claims 1 to 4 , wherein an end portion of the stationary blade main body is disposed so as to protrude from the support member. 前記静翼本体は、長手方向に貫通する中空部が設けられ、前記支持部材を貫通した端部に前記中空部に連通するドレン通路が設けられることを特徴とする請求項5に記載の静翼。 The stator blade according to claim 5 , wherein the stator blade body is provided with a hollow portion penetrating in a longitudinal direction, and a drain passage communicating with the hollow portion is provided at an end portion penetrating the support member. . 前記支持部材同士が連結されることで、請求項1から請求項6のいずれか一項に記載の静翼がリング形状に組付けられて構成される、
ことを特徴とする静翼ユニット。
By connecting the supporting members, the stationary blade according to any one of claims 1 to 6 is assembled in a ring shape, and configured.
A stationary blade unit characterized by that.
ケーシングと、
前記ケーシング内に回転自在に支持されたロータと、
動翼の基端部が前記ロータに支持されて前記ロータの周方向に所定間隔で複数配置される複数段の動翼ユニットと、
静翼の基端部と先端部が前記ケーシングに支持されて前記ロータの周方向に所定間隔で複数配置される複数段の静翼動翼ユニットと、
を有し、
前記複数段の静翼ユニットのうちの最終段の静翼ユニットとして請求項7に記載の静翼ユニットが適用される、
ことを特徴とする蒸気タービン。
A casing,
A rotor rotatably supported in the casing;
A plurality of rotor blade units in which a base end portion of a rotor blade is supported by the rotor and is arranged in a plurality at predetermined intervals in the circumferential direction of the rotor;
A plurality of stages of stationary blade moving blade units in which a base end portion and a distal end portion of a stationary blade are supported by the casing and are arranged at a predetermined interval in the circumferential direction of the rotor;
Have
The stationary blade unit according to claim 7 is applied as a final-stage stationary blade unit among the plurality of stages of stationary blade units.
A steam turbine characterized by that.
JP2014133259A 2014-06-27 2014-06-27 Stator blades and vane units, steam turbines Expired - Fee Related JP6302368B2 (en)

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