UA73345C2 - Проміжний сегмент для утримання статорного кільця турбіни високого тиску в турбомашині, виконаний з можливістю корекції величини зазорів - Google Patents
Проміжний сегмент для утримання статорного кільця турбіни високого тиску в турбомашині, виконаний з можливістю корекції величини зазорів Download PDFInfo
- Publication number
- UA73345C2 UA73345C2 UA2002097182A UA2002097182A UA73345C2 UA 73345 C2 UA73345 C2 UA 73345C2 UA 2002097182 A UA2002097182 A UA 2002097182A UA 2002097182 A UA2002097182 A UA 2002097182A UA 73345 C2 UA73345 C2 UA 73345C2
- Authority
- UA
- Ukraine
- Prior art keywords
- segment
- upstream
- wall
- pressure turbine
- housing
- Prior art date
Links
- 238000011144 upstream manufacturing Methods 0.000 claims abstract description 32
- 238000006073 displacement reaction Methods 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000012876 topography Methods 0.000 claims 1
- 125000006850 spacer group Chemical group 0.000 abstract 4
- 239000007789 gas Substances 0.000 description 15
- 230000014759 maintenance of location Effects 0.000 description 8
- 238000005452 bending Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000003993 interaction Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 241000435574 Popa Species 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000002788 crimping Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 239000002574 poison Substances 0.000 description 1
- 231100000614 poison Toxicity 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
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
- 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
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/60—Assembly methods
- F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
- F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation
-
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0100059A FR2819010B1 (fr) | 2001-01-04 | 2001-01-04 | Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux |
| PCT/FR2002/000011 WO2002053876A1 (fr) | 2001-01-04 | 2002-01-03 | Secteur d"entretoise de support d"anneau de stator de la turbine haute pression d"une turbomachine avec rattrapage de jeux |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| UA73345C2 true UA73345C2 (uk) | 2005-07-15 |
Family
ID=8858504
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| UA2002097182A UA73345C2 (uk) | 2001-01-04 | 2002-03-01 | Проміжний сегмент для утримання статорного кільця турбіни високого тиску в турбомашині, виконаний з можливістю корекції величини зазорів |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US6726446B2 (fr) |
| EP (1) | EP1225309B1 (fr) |
| JP (1) | JP4021768B2 (fr) |
| KR (1) | KR100829154B1 (fr) |
| CA (1) | CA2400151C (fr) |
| DE (1) | DE60204489T2 (fr) |
| FR (1) | FR2819010B1 (fr) |
| RU (1) | RU2289699C2 (fr) |
| UA (1) | UA73345C2 (fr) |
| WO (1) | WO2002053876A1 (fr) |
Families Citing this family (50)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2816352B1 (fr) * | 2000-11-09 | 2003-01-31 | Snecma Moteurs | Ensemble de ventilation d'un anneau de stator |
| US8641045B2 (en) * | 2003-05-01 | 2014-02-04 | Advanced Technologies Group, Inc. | Seal with stacked sealing elements |
| US7108479B2 (en) * | 2003-06-19 | 2006-09-19 | General Electric Company | Methods and apparatus for supplying cooling fluid to turbine nozzles |
| FI116958B (fi) * | 2003-07-01 | 2006-04-13 | Nokia Corp | Hallintasolmujen määrittäminen laitteenhallintajärjestelmässä |
| US20050091984A1 (en) * | 2003-11-03 | 2005-05-05 | Robert Czachor | Heat shield for gas turbine engine |
| FR2867224B1 (fr) | 2004-03-04 | 2006-05-19 | Snecma Moteurs | Dispositif de maintien axial de secteur d'entretoise pour anneau d'une turbine haute-pression de turbomachine |
| US7494317B2 (en) * | 2005-06-23 | 2009-02-24 | Siemens Energy, Inc. | Ring seal attachment system |
| US7448846B2 (en) * | 2005-08-06 | 2008-11-11 | General Electric Company | Thermally compliant turbine shroud mounting |
| US20070249823A1 (en) * | 2006-04-20 | 2007-10-25 | Chemagis Ltd. | Process for preparing gemcitabine and associated intermediates |
| US7607885B2 (en) * | 2006-07-31 | 2009-10-27 | General Electric Company | Methods and apparatus for operating gas turbine engines |
| US7665962B1 (en) | 2007-01-26 | 2010-02-23 | Florida Turbine Technologies, Inc. | Segmented ring for an industrial gas turbine |
| US7597533B1 (en) | 2007-01-26 | 2009-10-06 | Florida Turbine Technologies, Inc. | BOAS with multi-metering diffusion cooling |
| FR2913051B1 (fr) * | 2007-02-28 | 2011-06-10 | Snecma | Etage de turbine dans une turbomachine |
| KR100789311B1 (ko) * | 2007-03-08 | 2007-12-28 | 한전케이피에스 주식회사 | 저압 터빈용 하부 그랜드 하우징 위치 조절 장치 |
| FR2921410B1 (fr) * | 2007-09-24 | 2010-03-12 | Snecma | Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des moyens permettant sa prehension |
| US7762509B2 (en) * | 2007-10-18 | 2010-07-27 | United Technologies Corp. | Gas turbine engine systems involving rotatable annular supports |
| FR2923527B1 (fr) * | 2007-11-13 | 2013-12-27 | Snecma | Etage de turbine ou de compresseur, en particulier de turbomachine |
| FR2931872B1 (fr) * | 2008-05-28 | 2010-08-20 | Snecma | Turbine haute pression d'une turbomachine avec montage ameliore du boitier de pilotage des jeux radiaux d'aubes mobiles. |
| FR2935430B1 (fr) * | 2008-08-26 | 2012-03-09 | Snecma | Turbine haute-pression de turbomachine amelioree, secteur de distributeur et moteur d'aeronef associes |
| FR2941488B1 (fr) * | 2009-01-28 | 2011-09-16 | Snecma | Anneau de turbine a encoche anti-rotation |
| FR2942845B1 (fr) * | 2009-03-09 | 2011-04-01 | Snecma | Ensemble d'anneau de turbine |
| BRPI1013342A8 (pt) * | 2009-03-09 | 2016-09-20 | Sme | Conjunto de anel de turbina |
| JP5384983B2 (ja) * | 2009-03-27 | 2014-01-08 | 本田技研工業株式会社 | タービンシュラウド |
| US8342798B2 (en) * | 2009-07-28 | 2013-01-01 | General Electric Company | System and method for clearance control in a rotary machine |
| US8740552B2 (en) * | 2010-05-28 | 2014-06-03 | General Electric Company | Low-ductility turbine shroud and mounting apparatus |
| JP5751950B2 (ja) * | 2011-06-20 | 2015-07-22 | 三菱日立パワーシステムズ株式会社 | ガスタービン及びガスタービンの補修方法 |
| US9080458B2 (en) | 2011-08-23 | 2015-07-14 | United Technologies Corporation | Blade outer air seal with multi impingement plate assembly |
| US9726043B2 (en) | 2011-12-15 | 2017-08-08 | General Electric Company | Mounting apparatus for low-ductility turbine shroud |
| US9051849B2 (en) | 2012-02-13 | 2015-06-09 | United Technologies Corporation | Anti-rotation stator segments |
| FR2989724B1 (fr) * | 2012-04-20 | 2015-12-25 | Snecma | Etage de turbine pour une turbomachine |
| EP2841720B1 (fr) * | 2012-04-27 | 2020-08-19 | General Electric Company | Système et procédé pour limiter le mouvement axial entre un étrier et un ensemble carénage dans un ensemble turbine |
| EP2997234B1 (fr) | 2013-05-17 | 2020-05-27 | General Electric Company | Système de support d'anneau d'étancheité cmc d'une turbine à gaz |
| JP6529013B2 (ja) | 2013-12-12 | 2019-06-12 | ゼネラル・エレクトリック・カンパニイ | Cmcシュラウド支持システム |
| US10577963B2 (en) * | 2014-01-20 | 2020-03-03 | United Technologies Corporation | Retention clip for a blade outer air seal |
| CN106460543B (zh) * | 2014-06-12 | 2018-12-21 | 通用电气公司 | 多件式护罩悬挂器组件 |
| US10400619B2 (en) | 2014-06-12 | 2019-09-03 | General Electric Company | Shroud hanger assembly |
| EP3155236A1 (fr) | 2014-06-12 | 2017-04-19 | General Electric Company | Ensemble de suspension de carénage |
| FR3024883B1 (fr) * | 2014-08-14 | 2016-08-05 | Snecma | Module de turbomachine |
| US9874104B2 (en) | 2015-02-27 | 2018-01-23 | General Electric Company | Method and system for a ceramic matrix composite shroud hanger assembly |
| US10392950B2 (en) * | 2015-05-07 | 2019-08-27 | General Electric Company | Turbine band anti-chording flanges |
| US9915153B2 (en) * | 2015-05-11 | 2018-03-13 | General Electric Company | Turbine shroud segment assembly with expansion joints |
| US10436071B2 (en) | 2016-04-15 | 2019-10-08 | United Technologies Corporation | Blade outer air seal having retention snap ring |
| GB201708746D0 (en) * | 2017-06-01 | 2017-07-19 | Rolls Royce Plc | Clearance control arrangement |
| FR3082872B1 (fr) * | 2018-06-25 | 2021-06-04 | Safran Aircraft Engines | Dispositif de refroidissement d'un carter de turbomachine |
| US10934876B2 (en) * | 2018-07-18 | 2021-03-02 | Raytheon Technologies Corporation | Blade outer air seal AFT hook retainer |
| FR3098238B1 (fr) * | 2019-07-04 | 2021-06-18 | Safran Aircraft Engines | dispositif de refroidissement amélioré d’anneau de turbine d’aéronef |
| FR3109406B1 (fr) * | 2020-04-17 | 2022-10-07 | Safran Aircraft Engines | Dispositif de refroidissement d’un carter de turbine |
| US11788425B2 (en) * | 2021-11-05 | 2023-10-17 | General Electric Company | Gas turbine engine with clearance control system |
| CN116085067B (zh) | 2021-11-05 | 2026-05-29 | 通用电气公司 | 具有流体导管系统的燃气涡轮发动机及其操作方法 |
| DE102023104051A1 (de) * | 2023-02-17 | 2024-08-22 | MTU Aero Engines AG | Statorvorrichtung zur Anordnung innerhalb eines vorgegebenen Turbinengehäuses einer Strömungsmaschine, Verbindungssystem für eine Strömungsmaschine, sowie Strömungsmaschine |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3966354A (en) * | 1974-12-19 | 1976-06-29 | General Electric Company | Thermal actuated valve for clearance control |
| US4303371A (en) * | 1978-06-05 | 1981-12-01 | General Electric Company | Shroud support with impingement baffle |
| US5022816A (en) * | 1989-10-24 | 1991-06-11 | United Technologies Corporation | Gas turbine blade shroud support |
| US5056988A (en) * | 1990-02-12 | 1991-10-15 | General Electric Company | Blade tip clearance control apparatus using shroud segment position modulation |
| US5127793A (en) * | 1990-05-31 | 1992-07-07 | General Electric Company | Turbine shroud clearance control assembly |
| US5169287A (en) * | 1991-05-20 | 1992-12-08 | General Electric Company | Shroud cooling assembly for gas turbine engine |
| US5205708A (en) * | 1992-02-07 | 1993-04-27 | General Electric Company | High pressure turbine component interference fit up |
| RU2086792C1 (ru) * | 1994-11-24 | 1997-08-10 | Акционерное общество "Авиадвигатель" | Газотурбинный двигатель |
| FR2743603B1 (fr) * | 1996-01-11 | 1998-02-13 | Snecma | Dispositif de jonction de segments d'un distributeur circulaire a un carter de turbomachine |
| RU2136896C1 (ru) * | 1997-05-28 | 1999-09-10 | Акционерное общество "Турбомоторный завод" | Турбина |
| FR2766517B1 (fr) * | 1997-07-24 | 1999-09-03 | Snecma | Dispositif de ventilation d'un anneau de turbomachine |
| FR2780443B1 (fr) | 1998-06-25 | 2000-08-04 | Snecma | Anneau de stator de turbine haute pression d'une turbomachine |
| US6602050B1 (en) * | 1999-03-24 | 2003-08-05 | Siemens Aktiengesellschaft | Covering element and arrangement with a covering element and a support structure |
| US6435820B1 (en) * | 1999-08-25 | 2002-08-20 | General Electric Company | Shroud assembly having C-clip retainer |
-
2001
- 2001-01-04 FR FR0100059A patent/FR2819010B1/fr not_active Expired - Fee Related
-
2002
- 2002-01-03 RU RU2002123582/06A patent/RU2289699C2/ru active
- 2002-01-03 DE DE60204489T patent/DE60204489T2/de not_active Expired - Lifetime
- 2002-01-03 US US10/204,403 patent/US6726446B2/en not_active Expired - Lifetime
- 2002-01-03 EP EP02290005A patent/EP1225309B1/fr not_active Expired - Lifetime
- 2002-01-03 JP JP2002554361A patent/JP4021768B2/ja not_active Expired - Fee Related
- 2002-01-03 KR KR1020027011546A patent/KR100829154B1/ko not_active Expired - Fee Related
- 2002-01-03 WO PCT/FR2002/000011 patent/WO2002053876A1/fr not_active Ceased
- 2002-01-03 CA CA002400151A patent/CA2400151C/fr not_active Expired - Lifetime
- 2002-03-01 UA UA2002097182A patent/UA73345C2/uk unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US6726446B2 (en) | 2004-04-27 |
| CA2400151C (fr) | 2009-10-06 |
| KR100829154B1 (ko) | 2008-05-13 |
| EP1225309A1 (fr) | 2002-07-24 |
| RU2289699C2 (ru) | 2006-12-20 |
| JP4021768B2 (ja) | 2007-12-12 |
| US20030031557A1 (en) | 2003-02-13 |
| DE60204489D1 (de) | 2005-07-14 |
| EP1225309B1 (fr) | 2005-06-08 |
| KR20020075470A (ko) | 2002-10-04 |
| JP2004517246A (ja) | 2004-06-10 |
| FR2819010A1 (fr) | 2002-07-05 |
| CA2400151A1 (fr) | 2002-07-11 |
| WO2002053876A1 (fr) | 2002-07-11 |
| DE60204489T2 (de) | 2006-03-16 |
| FR2819010B1 (fr) | 2004-05-28 |
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