WO2011118075A1 - 蛇腹状ベローズを用いてなるシール機構及び該シール機構を備えた蒸気タービン - Google Patents
蛇腹状ベローズを用いてなるシール機構及び該シール機構を備えた蒸気タービン Download PDFInfo
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- WO2011118075A1 WO2011118075A1 PCT/JP2010/069269 JP2010069269W WO2011118075A1 WO 2011118075 A1 WO2011118075 A1 WO 2011118075A1 JP 2010069269 W JP2010069269 W JP 2010069269W WO 2011118075 A1 WO2011118075 A1 WO 2011118075A1
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- Prior art keywords
- bellows
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- sealing mechanism
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
- F01D25/164—Flexible supports; Vibration damping means associated with the bearing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J3/00—Diaphragms; Bellows; Bellows pistons
- F16J3/04—Bellows
- F16J3/047—Metallic bellows
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/55—Seals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/501—Elasticity
Definitions
- the present invention is suitable for being applied to a rotor shaft or the like of a steam turbine, can easily set a natural frequency, and can easily avoid resonance with a rotor shaft system, and a steam turbine provided with the seal mechanism About.
- the steam turbine has an internal compartment inside the external compartment, and a rotor is rotatably supported at the center.
- a plurality of moving blades are fixed to the rotor at set intervals, and a plurality of stationary blades are fixed to a blade ring that is fixed to the internal casing.
- a steam passage is formed in which the moving blades and the stationary blades are alternately arranged in multiple stages.
- Steam entrances are provided in the external compartment and the internal compartment, and the steam entering the interior compartment from the steam entrance passes through the steam passage, rotates the rotor, and drives the generator connected to the rotor. To do.
- the rotor is rotatably supported by a bearing portion outside the external compartment, and the bearing portion is fixed on a foundation made of concrete or the like.
- a rotor shaft between the bearing portion and the external casing is provided with a ground portion (shaft seal portion) that prevents steam leakage, and the ground portion is supported by the bearing portion via a connecting portion.
- the low-pressure seal steam discharged from the internal casing is supplied to the gland portion after being subjected to rotation of the rotor.
- a cylindrical bellows-like bellows is installed between the outer casing and the ground portion so as to surround the rotor shaft in order to prevent vapor from leaking between the outer casing and the ground portion.
- the bellows-like bellows can absorb relative displacement between the external casing and the ground portion due to thermal expansion or pressure.
- Patent Document 1 discloses a seal mechanism in which a bellows-like bellows is disposed between an external casing and a ground portion.
- the sealing mechanism disclosed in Patent Document 1 will be described with reference to FIGS.
- a seal mechanism 100A shown in FIG. 4 a cylindrical bellows-like bellows 102 having a double layer structure is arranged around a rotor shaft (not shown) so as to surround the rotor shaft.
- the bellows-like bellows 102 is installed between a ring-shaped end plate 112 connected to an external casing (not shown) and a ring-shaped end plate 114 connected to a ground part (not shown). Airtight seal between the two parts prevents vapor leakage.
- the bellows-shaped bellows 102 is composed of an inner bellows 102a and an outer-layer bellows 102b which are formed by applying pressure from the inside by overlapping two cylinders, and having a bellows shape except for the flat surface portion 104.
- a ring-shaped rib 106 is fixed to the outer surface of the flat portion 104, and a weight 108 is inserted and fixed in a hole provided in the outer wall of the rib 106.
- the rib 106 and the weight 108 constitute vibration adjusting means.
- FIG. 5 shows another configuration example of the bellows-shaped bellows disclosed in Patent Document 1.
- the seal mechanism 100 ⁇ / b> B includes a double-layered bellows-like bellows 102 that does not include the vibration adjusting means, and a bellows 116 disposed outside the bellows-like bellows 102. Both ends of the bellows 116 are connected to the end plate 112 or the end plate 114 via support members 118, respectively. By providing the bellows 116, the natural frequency of the seal mechanism 100B can be adjusted.
- the bellows bellows provided at the ground part of the steam turbine has its natural frequency determined by the flexible bellows part.
- the sealing mechanisms 100A and 100B disclosed in Patent Document 1 have a close contact structure with almost no gap between the inner layer bellows 102a and the outer layer bellows 102b. Therefore, the natural frequency varies due to the difference in the degree of adhesion at the time of manufacture, and it is not easy to set the required natural frequency, and it is difficult to set the natural frequency for avoiding resonance with the turbine rotor. There is a problem.
- the vibration adjusting means including the rib 106 and the weight 108 is provided to adjust the natural frequency of the seal mechanism 100A.
- the vibration adjusting means is provided. It takes extra effort and cost.
- the third bellows 116 is provided outside the double bellows-shaped bellows 102 to adjust the natural frequency.
- the bellows 116 and the support member 118 are divided into two to make the bellows. Therefore, there is a problem in that extra labor and time are required.
- the present invention has been made in view of the above-mentioned problems of the prior art, and does not require extra labor and cost, and is a sealing mechanism that allows easy adjustment of the natural frequency of the bellows-shaped bellows provided to surround the shaft to be sealed.
- An object of the present invention is to provide a sealing mechanism using a bellows-like bellows and a steam turbine provided with the sealing mechanism.
- the sealing mechanism using the bellows-shaped bellows of the present invention is constituted by a cylindrical bellows-shaped bellows surrounding the shaft to be sealed, and both ends of the bellows-shaped bellows of the shaft to be sealed are
- the bellows-shaped bellows includes an outer bellows-shaped bellows and a seal target.
- a single plate-like body is bent, and the outer bellows-like bellows and the inner bellows-like bellows are arranged in a non-contact state with each other.
- the outer bellows-shaped bellows and the inner bellows-shaped bellows are arranged in a non-contact state, and it is not necessary to consider the degree of contact between the two bellows-shaped bellows. It becomes easy. Therefore, setting of the natural frequency of the seal mechanism is facilitated, so that no extra effort and cost are required for adjusting the natural frequency. Therefore, it is not necessary to perform an excitation test for confirming the natural frequency for each unit, the cost required for the test can be reduced, and the labor and cost for remanufacturing the bellows-shaped bellows can be eliminated.
- a spacing forming ring member surrounding the shaft to be sealed is provided at the end portions of the supporting member facing each other, and the outer bellows-shaped bellows is connected to the outer edge of the spacing forming ring member. And an inner bellows-like bellows may be connected to the inner edge of the spacing ring member.
- the sealing mechanism of the present invention may be applied to the ground portion of the steam turbine. That is, the sealed shaft body is the rotor shaft of the steam turbine, the support member is the external casing and the ground portion, and the outer bellows-like bellows and the inner bellows-like bellows are airtight between the outer casing and the ground portion. It is held and constructed so that the periphery of the rotor shaft between the outer casing and the ground portion is hermetically sealed. This facilitates adjustment of the natural frequency of the seal mechanism at a simple and low cost, and thus avoids resonance with the rotor shaft.
- the outer bellows-like bellows and the inner bellows-like bellows are selected in thickness, number of ridges, pitch width or material so that they meet the required natural frequency and environmental conditions. It is good to do so.
- the plate thickness, number of ridges, pitch width, or material it becomes easier to set the required natural frequency, and the strength, durability performance, etc. according to the environmental conditions are given. it can.
- the steam turbine according to the present invention includes an external casing, an internal casing provided in the external casing, a rotor disposed in the internal casing, and a set interval in the axial direction of the rotor.
- the steam turbine has any one of the configurations described above between the outer casing and the gland portion.
- a seal mechanism is provided.
- seal mechanism of the present invention By applying the seal mechanism of the present invention to the rotor shaft of the steam turbine, it is possible to reliably prevent the steam from leaking between the outer casing and the ground portion, and the seal mechanism and the rotor with a simple and low-cost configuration. Resonance with the shaft can be avoided.
- the bellows-shaped bellows that surround the shaft to be sealed is connected to the support members disposed around the shaft to be sealed,
- the bellows-shaped bellows is concentric with the outer bellows-shaped bellows and the outer bellows-shaped bellows around the shaft to be sealed.
- the inner bellows-shaped bellows are nested inside the outer bellows-shaped bellows so that the outer bellows-shaped bellows and the inner bellows-shaped bellows are each formed by bending a single plate-like body.
- the outer bellows-shaped bellows and the inner bellows-shaped bellows are arranged in a non-contact state, so that the natural frequency can be adjusted by simple and low-cost means, and resonance with the sealed shaft body is avoided. Kill. Moreover, it has durability equivalent to that of a conventional double-layered bellows-like bellows, and can achieve a long life.
- the steam turbine according to the present invention includes an external casing, an internal casing provided in the external casing, a rotor disposed in the internal casing, and a set interval in the axial direction of the rotor.
- a steam turbine having a bearing portion and a gland portion that is provided in a portion where the rotor shaft passes through the outer casing and prevents steam leakage is provided with the seal mechanism configured as described above. Can be reliably prevented, and resonance between the rotor shaft and the seal mechanism can be avoided by simple and low-cost means.
- FIGS. 1 and 2 A first embodiment in which a sealing mechanism of the present invention is applied to a low-pressure steam turbine will be described with reference to FIGS. 1 and 2. First, the configuration on the steam exhaust side of the low-pressure steam turbine 10 will be described with reference to FIG.
- an external compartment 12 is provided so as to surround the rotor 20.
- the flow guide 16 forms an exhaust chamber 14 that exhausts the low-pressure steam s after rotating the rotor 20.
- the flow guide 16 is attached to the support member 18.
- a disk 22 and a blade 24 constituting the final stage moving blade are formed integrally with the rotor 20.
- An unillustrated final stationary blade fixed to an internal casing (not illustrated) is provided immediately upstream of the final stage moving blade.
- the rotor shaft 26 extending integrally from the rotor 20 is rotatably supported by a bearing pad (not shown) provided inside the bearing housing 28 outside the outer casing 12.
- the bearing box 28 is fixed on a foundation base 30 made of concrete or the like.
- a ground portion (shaft seal portion) 32 is provided between the outer casing 12 and the bearing box 28 for preventing steam from leaking through a gap between the rotor shaft 26 and the outer casing 12.
- a part of the low-pressure exhaust steam flowing through the exhaust chamber 14 is supplied to the gland part 32 as seal steam, thereby preventing steam leakage at the gland part.
- the casing 34 of the ground portion 32 is connected to the bearing box 28 via a connecting portion 36.
- a labyrinth seal 38 is provided at a portion in contact with the rotor shaft 26 to prevent steam from leaking from a gap with the rotor shaft 26.
- the sealing mechanism 40A In order to seal a region between the shielding wall 19 connected to the support member 18 of the outer casing 12 and the casing 34 of the ground portion 32 and prevent leakage of steam from this region, the sealing mechanism 40A according to the present embodiment. Is provided. Hereinafter, the configuration of the seal mechanism 40A will be described with reference to FIG.
- a ring-shaped end plate 42 is fixed to the surface of the shielding wall 19 facing the ground portion 32 side while maintaining airtightness by welding or bolt connection.
- a ring-shaped end plate 44 is fixed to the surface of the ground part 32 facing the shielding wall 19 of the casing 34 by welding or bolting. As shown in FIG. 2, these end plates have a rectangular cross section.
- an outer bellows-like bellows 46 and an inner bellows-like bellows 48 are mounted between these end plates. These two bellows-like bellows are formed by bending a single plate-like body made of metal into a bellows shape. Both ends of the outer bellows-shaped bellows 46 are hermetically welded to the outer edge of the end plate 42 or the end plate 44, respectively. Further, both ends of the inner bellows-shaped bellows 48 are air-tightly welded to the inner edge of the end plate 42 or the end plate 44, respectively.
- the sealing mechanism 40A is so as not to contact even if vibrations have an interval of at least 0.1 mm.
- the outer bellows-like bellows 46 and the inner bellows-like bellows 48 are arranged at intervals that do not always come into contact with each other, there is no variation in the natural frequency due to the difference in the degree of close contact as in the prior art. Therefore, the natural frequency of the seal mechanism 40A after being attached to the rotor shaft 26 can be easily set. Therefore, resonance between the seal mechanism 40A and the rotor shaft 26 can be easily avoided. Further, unlike the seal mechanism disclosed in Patent Document 1, no special means for adjusting the natural frequency is required, so that the manufacturing cost is not increased.
- both ends of the outer bellows-shaped bellows 46 are connected to outer edge ends of the end plates 42 and 44
- both ends of the inner bellows-shaped bellows 48 are connected to inner edge ends of the end plates 42 and 44
- both bellows-shaped bellows are connected to the end plates 42.
- 44 is fixed to the shielding wall 19 and the casing 34, the positioning of the bellows bellows is facilitated, and the bellows bellows can be easily attached in a non-contact state.
- the natural frequency of the seal mechanism 40A can be easily set, it is not necessary to remanufacture, and after the seal mechanism 40A is attached to the rotor shaft 26, it is necessary to perform an excitation test for each unit. The cost required for the vibration test can be eliminated.
- the outer bellows-shaped bellows 46 and the inner bellows-shaped bellows 48 have the same plate thickness, number of peaks, peak height, pitch width, and material, but the seal mechanism 40B of the present embodiment has an inner bellows.
- An outer bellows-like bellows 50 in which the number of peaks, the peak height, the pitch width, and the material are different from each other is used.
- Other configurations are the same as those in the first embodiment, including the method of attaching the bellows-shaped bellows, and this embodiment is also applied to the rotor shaft 26 of the low-pressure steam turbine 10 as in the first embodiment. It is.
- the peak height H 1 and the pitch width P 1 of the outer bellows-shaped bellows 50 are in a relationship of P 2 ⁇ P 1 and H 1 ⁇ H 2 with respect to the peak height H 2 and the pitch width P 2 of the inner bellows-shaped bellows 48.
- the height of the outer bellows bellows 50 is lower than the height of the inner bellows bellows 48.
- An interval C 2 between the upper end of the lower end and an inner bellows bellows 48 outside the bellows-shaped bellows 50 is larger than the interval C 1 of the first embodiment.
- the material of the inner bellows-like bellows 48 in a high temperature environment is stainless steel (SUS310 or SUS410) having excellent heat resistance
- the material of the outer bellows-like bellows 50 is chromium steel (SCr) having excellent corrosion resistance. Yes.
- the natural frequency can be set more easily by changing the specifications of the outer bellows-like bellows 50 and the inner bellows-like bellows 48 in accordance with the respective requirements and use environments. As a result, the life of the seal mechanism 40B can be extended. In the present embodiment, the thickness of the outer bellows-like bellows 50 may be changed.
- the natural frequency can be easily set while maintaining the sealing performance with respect to the sealed shaft body, and resonance with the sealed shaft body can be easily avoided.
- the ground portion of the rotor shaft of the steam turbine It is possible to realize a seal mechanism suitable for sealing.
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- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
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Abstract
Description
また、シール機構100Bでは、二重構造の蛇腹状ベローズ102の外側に、第3のベローズ116を設けて、固有振動数を調整しているが、ベローズ116と支持部材118とを二つ割りにして蛇腹状ベローズ102の外側に取り付ける必要があり、このために余分な手間と時間がかかるという問題がある。
また、外側蛇腹状ベローズの内側に内側蛇腹状ベローズを入れ子状に設置するため、図5に示すように、蛇腹状ベローズ102の外側に二つ割りした蛇腹状ベローズを取り付ける場合より、製作が容易である。
このように、外側蛇腹状ベローズ及び内側蛇腹状ベローズを、この間隔形成用リング部材を介して支持部材に取り付けることにより、両蛇腹状ベローズを互いの間隔を空けて、非接触状態で支持部材に取り付けるのが容易になる。
このように、板厚、山数、ピッチ幅又は材質を選択することで、要求された固有振動数に設定するのがさらに容易になり、また、環境条件に合った強度や耐久性能等を付与できる。
本発明のシール機構を低圧蒸気タービンに適用した第1実施形態を図1及び図2に基づいて説明する。まず、図1により、低圧蒸気タービン10の蒸気排気側の構成を説明する。図1において、ロータ20を囲むように外部車室12が設けられている。外部車室12では、フローガイド16が、ロータ20を回転させた後の低圧蒸気sを排気させる排気室14を形成している。フローガイド16は支持部材18に取り付けられている。
次に、本発明のシール機構の第2実施形態を図3により説明する。前記第1実施形態は、外側蛇腹状ベローズ46と内側蛇腹状ベローズ48の板厚、山数、山高、ピッチ幅、及び材質が同一であったが、本実施形態のシール機構40Bは、内側蛇腹状ベローズ48に対して、山数、山高、ピッチ幅及び材質を異ならせた外側蛇腹状ベローズ50を用いている。その他の構成は、両蛇腹状ベローズの取り付け方法も含めて、第1実施形態と同一であり、本実施形態も第1実施形態と同様に、低圧蒸気タービン10のロータ軸26に適用されたものである。
Claims (5)
- 被シール軸体を囲む筒状の蛇腹状ベローズで構成され、該蛇腹状ベローズの両端が該被シール軸体の周囲に配置された支持部材に接続され、該支持部材間の相対変位を許容しながら被シール軸体の周囲を気密シールするシール機構において、
前記蛇腹状ベローズが、外側蛇腹状ベローズと、被シール軸体を中心に該外側蛇腹状ベローズと同心状となるように外側蛇腹状ベローズの内側に入れ子状に設けられた内側蛇腹状ベローズとからなり、
外側蛇腹状ベローズ及び内側蛇腹状ベローズは、夫々単一の板状体を曲折して構成され、外側蛇腹状ベローズと内側蛇腹状ベローズとは互いに非接触状態で配置されていることを特徴とする蛇腹状ベローズを用いてなるシール機構。 - 前記支持部材の互いに対面する端部に、前記被シール軸体を取り巻く間隔形成用リング部材が設けられ、外側蛇腹状ベローズが該間隔形成用リング部材の外縁端に接続されていると共に、内側蛇腹状ベローズが該間隔形成用リング部材の内縁端に接続されていることを特徴とする請求項1に記載の蛇腹状ベローズを用いてなるシール機構。
- 前記被シール軸体が蒸気タービンのロータ軸であって、前記支持部材が外部車室及びグランド部であり、
前記外側蛇腹状ベローズ及び内側蛇腹状ベローズが外部車室とグランド部との間に気密を保持して架設され、外部車室とグランド部間のロータ軸の周囲を気密シールするものであることを特徴とする請求項1又は2に記載の蛇腹状ベローズを用いてなるシール機構。 - 前記外側蛇腹状ベローズ及び内側蛇腹状ベローズは、それらが要求された固有振動数及び環境条件に適合するように、板厚、山数、ピッチ幅又は材質が選択されていることを特徴とする請求項1~3のいずれかの項に記載の蛇腹状ベローズを用いてなるシール機構。
- 外部車室と、該外部車室の内部に設けられた内部車室と、該内部車室の内部に配置されたロータと、該ロータに軸方向に設定間隔で固定された複数の動翼と、内部車室の内部に各動翼間に位置するように固定された複数の静翼と、外部車室の外側に設けられロータ軸を回転自在に支持する軸受部と、該ロータ軸が外部車室を貫通する部位に設けられ蒸気漏れを防ぐグランド部と、を備えた蒸気タービンにおいて、
前記外部車室とグランド部との間に請求項1~4のいずれかの項に記載の蛇腹状ベローズを用いてなるシール機構を設けたことを特徴とする蒸気タービン。
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CN201080061459.2A CN102713165B (zh) | 2010-03-25 | 2010-10-29 | 使用折皱状波纹管构成的密封机构及具备该密封机构的汽轮机 |
KR1020127020052A KR101464422B1 (ko) | 2010-03-25 | 2010-10-29 | 아코디언 형상 벨로즈를 사용하여 이루어지는 시일 기구 및 그 시일 기구를 구비한 증기 터빈 |
EP10848467.6A EP2511483B1 (en) | 2010-03-25 | 2010-10-29 | Sealing mechanism using accordioned bellows, and steam turbine provided with said sealing mechanism |
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JP2010070027A JP5578903B2 (ja) | 2010-03-25 | 2010-03-25 | シール機構及び蒸気タービン |
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US (1) | US8684670B2 (ja) |
EP (1) | EP2511483B1 (ja) |
JP (1) | JP5578903B2 (ja) |
KR (1) | KR101464422B1 (ja) |
CN (1) | CN102713165B (ja) |
WO (1) | WO2011118075A1 (ja) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
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DE102010031124A1 (de) * | 2010-07-08 | 2012-01-12 | Man Diesel & Turbo Se | Strömungsmaschine |
JP6189239B2 (ja) | 2014-03-24 | 2017-08-30 | 三菱日立パワーシステムズ株式会社 | 蒸気タービン |
EP2927431A1 (de) * | 2014-04-02 | 2015-10-07 | Siemens Aktiengesellschaft | Bauteil zur Führung von Heißgas |
CN106014509A (zh) * | 2016-07-28 | 2016-10-12 | 中国核动力研究设计院 | 一种以超临界二氧化碳为工质的透平发电机组 |
CN108843616A (zh) * | 2018-07-23 | 2018-11-20 | 深圳市能源环保有限公司 | 一种垃圾焚烧发电厂离心风机的防臭密封装置 |
CN112576317B (zh) * | 2020-12-08 | 2023-11-24 | 内蒙古汇能集团蒙南发电有限公司 | 一种多级涡轮发电机 |
US11913301B2 (en) * | 2021-04-09 | 2024-02-27 | Schlumberger Technology Corporation | Integral bellows for oilfield equipment |
Citations (2)
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JP3831617B2 (ja) | 2001-02-06 | 2006-10-11 | 三菱重工業株式会社 | 蒸気タービンの車室構造 |
JP2009235971A (ja) | 2008-03-26 | 2009-10-15 | Mitsubishi Heavy Ind Ltd | シール部材、蒸気タービン及び共振回避方法 |
Family Cites Families (10)
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US3051515A (en) * | 1960-08-17 | 1962-08-28 | Aeroquip Corp | Pressure compensating expansion joint |
US4710050A (en) * | 1986-10-20 | 1987-12-01 | Pacific Scientific Co. | Modular metallic bellows assembly |
GB8906901D0 (en) * | 1989-03-28 | 1989-05-10 | Crane John Uk Ltd | Mechanical face seals |
FR2735552B1 (fr) * | 1995-06-14 | 1997-07-18 | Cogema | Systeme d'etancheite pour l'accostage d'un conteneur sous un four de fusion |
JP2002323145A (ja) | 2001-04-26 | 2002-11-08 | Uno Kogyo Kk | 高温ガス用ダンパーのシール構造 |
JP3564441B2 (ja) | 2001-08-09 | 2004-09-08 | 三菱重工業株式会社 | 一軸型コンバインドサイクル発電プラント |
US6773017B2 (en) * | 2002-07-16 | 2004-08-10 | Pittsburgh Cryogenic Services, Inc. | Single-piece seal assembly |
US7334799B2 (en) * | 2002-12-23 | 2008-02-26 | Caterpillar Inc. | Sealing device for a turbocharger |
CN2735089Y (zh) * | 2004-06-02 | 2005-10-19 | 上海万安企业总公司 | 一种波纹管密封装置 |
CN1932342A (zh) * | 2006-09-06 | 2007-03-21 | 中国船舶重工集团公司第七�三研究所 | 检修密封结构 |
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- 2010-03-25 JP JP2010070027A patent/JP5578903B2/ja active Active
- 2010-10-29 CN CN201080061459.2A patent/CN102713165B/zh active Active
- 2010-10-29 KR KR1020127020052A patent/KR101464422B1/ko active IP Right Grant
- 2010-10-29 WO PCT/JP2010/069269 patent/WO2011118075A1/ja active Application Filing
- 2010-10-29 EP EP10848467.6A patent/EP2511483B1/en active Active
- 2010-12-02 US US12/958,847 patent/US8684670B2/en active Active
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JP3831617B2 (ja) | 2001-02-06 | 2006-10-11 | 三菱重工業株式会社 | 蒸気タービンの車室構造 |
JP2009235971A (ja) | 2008-03-26 | 2009-10-15 | Mitsubishi Heavy Ind Ltd | シール部材、蒸気タービン及び共振回避方法 |
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Also Published As
Publication number | Publication date |
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EP2511483B1 (en) | 2019-01-02 |
US20110236205A1 (en) | 2011-09-29 |
JP5578903B2 (ja) | 2014-08-27 |
EP2511483A4 (en) | 2013-11-20 |
EP2511483A1 (en) | 2012-10-17 |
US8684670B2 (en) | 2014-04-01 |
JP2011202570A (ja) | 2011-10-13 |
CN102713165A (zh) | 2012-10-03 |
KR20120098949A (ko) | 2012-09-05 |
CN102713165B (zh) | 2015-06-03 |
KR101464422B1 (ko) | 2014-11-21 |
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