JP5518118B2 - 回転するタービンブレードのためのシール装置 - Google Patents
回転するタービンブレードのためのシール装置 Download PDFInfo
- Publication number
- JP5518118B2 JP5518118B2 JP2012067225A JP2012067225A JP5518118B2 JP 5518118 B2 JP5518118 B2 JP 5518118B2 JP 2012067225 A JP2012067225 A JP 2012067225A JP 2012067225 A JP2012067225 A JP 2012067225A JP 5518118 B2 JP5518118 B2 JP 5518118B2
- Authority
- JP
- Japan
- Prior art keywords
- seal
- ring
- casing
- diaphragm
- turbine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000007789 sealing Methods 0.000 title description 9
- 239000012530 fluid Substances 0.000 claims description 7
- 230000000694 effects Effects 0.000 description 8
- 238000006073 displacement reaction Methods 0.000 description 5
- 238000011144 upstream manufacturing Methods 0.000 description 5
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 102000015933 Rim-like Human genes 0.000 description 1
- 108050004199 Rim-like Proteins 0.000 description 1
- 238000003491 array Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 239000010408 film Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000009420 retrofitting Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- 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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Description
11 ケーシングの周方向溝
12,13 可動ブレード
14,15 半径方向内側のT字形の部分
16,17 対応するスロット
18 ロータドラム
19,20 シュラウド
21,22 シール支持リング
28 支持キー
23,24 シールフィン/シールエレメント
25 ボルト
26 周方向切欠
27 半径方向の周方向延長部
29 弾性エレメント
30,31 固定ブレード
33,34 上流及び下流のダイヤフラムリング
51,52 内側及び外側の支持リング
53 横方向キー
54,55 横方向ピン
x 最大半径方向移動
α 回転角
Claims (6)
- 軸方向で交互に配置された固定ブレードの半径方向配置のための外側支持を提供する連続するダイヤフラムを有するタービンのためのシールにおいて、該シールが、回転するブレードの先端部周囲の流体の流れを低減するシールの一部を形成する半径方向及び軸方向で支持された外側シール部分を備え、該外側シール部分の半径方向支持部が、キー及び周方向延長部によって所定の位置に保持されたリングとして形成されており、前記キー及び周方向延長部が十分な間隙を有していることにより、圧力シール面及び軸方向の支持を保証しながらケーシングの部分及び/又はダイヤフラムと前記リングとの相対的な半径方向移動を許容するようになっており、前記リングが、ケーシングの部分及び/又はダイヤフラムから十分な間隙を有することにより、軸方向でのケーシングの部分及び/又はダイヤフラムの回転運動の際に半径方向に変位させられないようになっていることを特徴とする、タービンのためのシール。
- 前記軸方向の支持が、ケーシングに設けられた対応する溝における並置された面と接触するための軸方向に向けられた面を有する、リングの外周の延長部によって提供されている、請求項1記載のシール。
- 前記軸方向の支持が、ダイヤフラムとケーシングとの間の間隙内に配置された、リングの外周の延長部によって提供されている、請求項1記載のシール。
- 前記軸方向の支持が、リングの対応する溝又はエッジにおける並置された面と接触するための軸方向に向けられた面を有する、ケーシングの内周の延長部によって提供されている、請求項1記載のシール。
- 前記リングが、タービンのケーシング内に一緒に取り付けられかつ相対回転しないように固定された内側のリング及び外側のリングを有する、請求項1記載のシール。
- 前記リングが、前記外側のシール部分と、前記回転するブレードの先端部又はシュラウドに取り付けられたシール部分との間の間隙を閉鎖するように設計された半径方向に作用する弾性エレメントを有する、請求項1記載のシール。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH5452011 | 2011-03-25 | ||
CH00545/11 | 2011-03-25 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2012202409A JP2012202409A (ja) | 2012-10-22 |
JP5518118B2 true JP5518118B2 (ja) | 2014-06-11 |
Family
ID=43920997
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2012067225A Active JP5518118B2 (ja) | 2011-03-25 | 2012-03-23 | 回転するタービンブレードのためのシール装置 |
Country Status (5)
Country | Link |
---|---|
US (1) | US9062551B2 (ja) |
JP (1) | JP5518118B2 (ja) |
CN (1) | CN102705019B (ja) |
DE (1) | DE102012005771B4 (ja) |
IN (1) | IN2012DE00858A (ja) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9004495B2 (en) * | 2008-09-15 | 2015-04-14 | Stein Seal Company | Segmented intershaft seal assembly |
US9752592B2 (en) * | 2013-01-29 | 2017-09-05 | Rolls-Royce Corporation | Turbine shroud |
US10132187B2 (en) | 2013-08-07 | 2018-11-20 | United Technologies Corporation | Clearance control assembly |
FR3025261B1 (fr) * | 2014-09-03 | 2020-02-21 | Safran Helicopter Engines | Ensemble rotatif muni d'un dispositif de calage |
US9945243B2 (en) | 2014-10-14 | 2018-04-17 | Rolls-Royce Corporation | Turbine shroud with biased blade track |
US10161259B2 (en) * | 2014-10-28 | 2018-12-25 | General Electric Company | Flexible film-riding seal |
CA2915370A1 (en) | 2014-12-23 | 2016-06-23 | Rolls-Royce Corporation | Full hoop blade track with axially keyed features |
US10100649B2 (en) | 2015-03-31 | 2018-10-16 | Rolls-Royce North American Technologies Inc. | Compliant rail hanger |
KR101572903B1 (ko) * | 2015-04-03 | 2015-12-11 | 조정봉 | 기능향상형 오일 디플렉터 |
WO2016179608A2 (en) * | 2016-04-29 | 2016-11-10 | Stein Seal Company | Intershaft seal with asymmetric sealing ring |
US10598035B2 (en) * | 2016-05-27 | 2020-03-24 | General Electric Company | Intershaft sealing systems for gas turbine engines and methods for assembling the same |
EP3284919B1 (en) * | 2016-08-16 | 2024-09-25 | General Electric Technology GmbH | Axial flow turbine having a diaphragm split in two halves at a joint plane |
FR3059041B1 (fr) * | 2016-11-21 | 2020-05-08 | Safran Aircraft Engines | Dispositif de pilotage rotor/stator avec lechette a ressort |
US10533567B2 (en) * | 2017-05-30 | 2020-01-14 | United Technologies Corporation | Deflection spring seal |
US10392957B2 (en) | 2017-10-05 | 2019-08-27 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having load distribution features |
DE102018210601A1 (de) * | 2018-06-28 | 2020-01-02 | MTU Aero Engines AG | Segmentring zur montage in einer strömungsmaschine |
CN109441568B (zh) * | 2018-11-16 | 2024-04-19 | 华电电力科学研究院有限公司 | 一种高效率的低压隔板套装置及其装配方法 |
DE102019123646B4 (de) * | 2019-09-04 | 2023-08-03 | Schaeffler Technologies AG & Co. KG | Kühlmittelregler mit einem Wellendichtring |
US11149563B2 (en) * | 2019-10-04 | 2021-10-19 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having axial reaction load distribution features |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3501246A (en) | 1967-12-29 | 1970-03-17 | Westinghouse Electric Corp | Axial fluid-flow machine |
US4326835A (en) | 1979-10-29 | 1982-04-27 | General Motors Corporation | Blade platform seal for ceramic/metal rotor assembly |
DE69002064T2 (de) | 1989-01-09 | 1993-12-23 | Northern Eng Ind | Befestigung und Anordnung von segmentförmigen Elementen in Turbomaschinen. |
US5080557A (en) * | 1991-01-14 | 1992-01-14 | General Motors Corporation | Turbine blade shroud assembly |
US6131910A (en) | 1992-11-19 | 2000-10-17 | General Electric Co. | Brush seals and combined labyrinth and brush seals for rotary machines |
US5501573A (en) | 1993-01-29 | 1996-03-26 | Steam Specialties, Inc. | Segmented seal assembly and method for retrofitting the same to turbines and the like |
US5639211A (en) | 1995-11-30 | 1997-06-17 | United Technology Corporation | Brush seal for stator of a gas turbine engine case |
JPH09264104A (ja) | 1996-03-27 | 1997-10-07 | Ishikawajima Harima Heavy Ind Co Ltd | セラミック製シュラウドリング |
EP1243756A1 (de) * | 2001-03-23 | 2002-09-25 | Siemens Aktiengesellschaft | Turbine |
JP2002285802A (ja) | 2001-03-26 | 2002-10-03 | Toshiba Corp | 回転機械のラビリンスシール装置 |
US6547522B2 (en) * | 2001-06-18 | 2003-04-15 | General Electric Company | Spring-backed abradable seal for turbomachinery |
US7059821B2 (en) | 2003-05-07 | 2006-06-13 | General Electric Company | Method and apparatus to facilitate sealing within turbines |
US7229246B2 (en) * | 2004-09-30 | 2007-06-12 | General Electric Company | Compliant seal and system and method thereof |
US7287956B2 (en) | 2004-12-22 | 2007-10-30 | General Electric Company | Removable abradable seal carriers for sealing between rotary and stationary turbine components |
US7645117B2 (en) * | 2006-05-05 | 2010-01-12 | General Electric Company | Rotary machines and methods of assembling |
JP2007321721A (ja) | 2006-06-05 | 2007-12-13 | Toshiba Corp | 軸流タービン段落および軸流タービン |
US7686575B2 (en) | 2006-08-17 | 2010-03-30 | Siemens Energy, Inc. | Inner ring with independent thermal expansion for mounting gas turbine flow path components |
US20100074741A1 (en) | 2007-01-04 | 2010-03-25 | Luciano Cozza | Highly corrosion-resistant fixed blade assembly for a steam turbine, in particular a geothermal impulse turbine |
US8393858B2 (en) | 2009-03-13 | 2013-03-12 | Honeywell International Inc. | Turbine shroud support coupling assembly |
US8142141B2 (en) * | 2009-03-23 | 2012-03-27 | General Electric Company | Apparatus for turbine engine cooling air management |
-
2012
- 2012-03-21 DE DE102012005771.7A patent/DE102012005771B4/de active Active
- 2012-03-22 US US13/426,704 patent/US9062551B2/en active Active
- 2012-03-23 IN IN858DE2012 patent/IN2012DE00858A/en unknown
- 2012-03-23 CN CN201210093826.8A patent/CN102705019B/zh active Active
- 2012-03-23 JP JP2012067225A patent/JP5518118B2/ja active Active
Also Published As
Publication number | Publication date |
---|---|
JP2012202409A (ja) | 2012-10-22 |
US9062551B2 (en) | 2015-06-23 |
CN102705019A (zh) | 2012-10-03 |
US20120243977A1 (en) | 2012-09-27 |
CN102705019B (zh) | 2015-10-21 |
DE102012005771B4 (de) | 2022-06-30 |
DE102012005771A1 (de) | 2012-09-27 |
IN2012DE00858A (ja) | 2015-08-28 |
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