CN101899995A - 用于间隙控制的系统和方法 - Google Patents
用于间隙控制的系统和方法 Download PDFInfo
- Publication number
- CN101899995A CN101899995A CN201010197284XA CN201010197284A CN101899995A CN 101899995 A CN101899995 A CN 101899995A CN 201010197284X A CN201010197284X A CN 201010197284XA CN 201010197284 A CN201010197284 A CN 201010197284A CN 101899995 A CN101899995 A CN 101899995A
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- Prior art keywords
- gap
- guard shield
- turbine
- magnet
- removable guard
- 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.)
- Pending
Links
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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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/22—Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
-
- 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
- F05D2260/00—Function
- F05D2260/50—Kinematic linkage, i.e. transmission of position
- F05D2260/52—Kinematic linkage, i.e. transmission of position involving springs
-
- 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
- F05D2270/00—Control
- F05D2270/60—Control system actuates means
- F05D2270/62—Electrical actuators
-
- 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
- F05D2300/507—Magnetic properties
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/472195 | 2009-05-26 | ||
| US12/472,195 US8186945B2 (en) | 2009-05-26 | 2009-05-26 | System and method for clearance control |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101899995A true CN101899995A (zh) | 2010-12-01 |
Family
ID=43028726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201010197284XA Pending CN101899995A (zh) | 2009-05-26 | 2010-05-26 | 用于间隙控制的系统和方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8186945B2 (enExample) |
| JP (1) | JP2010276019A (enExample) |
| CN (1) | CN101899995A (enExample) |
| CH (1) | CH701149A2 (enExample) |
| DE (1) | DE102010016995A1 (enExample) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102230397A (zh) * | 2011-07-09 | 2011-11-02 | 潍坊雷诺特动力设备有限公司 | 蒸汽动力装置的汽封系统 |
| CN103375193A (zh) * | 2012-04-18 | 2013-10-30 | 通用电气公司 | 用于避免涡轮摩擦的定子密封件 |
| CN103429850A (zh) * | 2011-01-28 | 2013-12-04 | 斯奈克玛 | 涡轮发动机级 |
| CN103511003A (zh) * | 2012-06-28 | 2014-01-15 | 中航商用航空发动机有限责任公司 | 控制系统 |
| CN105587342A (zh) * | 2014-10-22 | 2016-05-18 | A.S.En.安萨尔多开发能源有限责任公司 | 具有可移动的末端的涡轮转子叶片 |
| CN106164417A (zh) * | 2014-02-25 | 2016-11-23 | 西门子股份公司 | 用于由主动液压间隙调节操作燃气轮机的方法 |
| CN109139129A (zh) * | 2017-06-27 | 2019-01-04 | 通用电气公司 | 间隙控制装置 |
| CN110939517A (zh) * | 2018-09-24 | 2020-03-31 | 通用电气公司 | 包壳主动间隙控制结构 |
| CN113757174A (zh) * | 2021-11-08 | 2021-12-07 | 中国航发上海商用航空发动机制造有限责任公司 | 一种机匣、压气机及压气机试验方法 |
| CN114592927A (zh) * | 2020-12-04 | 2022-06-07 | 通用电气公司 | 具有压电致动器的快速响应主动间隙控制系统 |
| CN114607474A (zh) * | 2022-03-21 | 2022-06-10 | 中国联合重型燃气轮机技术有限公司 | 静叶间隙控制系统和具有其的燃气轮机 |
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| CA2607700A1 (en) * | 2006-11-03 | 2008-05-03 | General Electric Company | Mechanical sealing system and method for rotary machines |
| US20100327534A1 (en) * | 2009-06-26 | 2010-12-30 | General Electric Company | Magnetic brush seal system |
| US8342798B2 (en) * | 2009-07-28 | 2013-01-01 | General Electric Company | System and method for clearance control in a rotary machine |
| FR2971543B1 (fr) * | 2011-02-11 | 2013-03-08 | Snecma | Procede de pilotage de jeu en sommet d'aubes de rotor de turbine |
| US8944756B2 (en) * | 2011-07-15 | 2015-02-03 | United Technologies Corporation | Blade outer air seal assembly |
| GB2494137B (en) * | 2011-08-31 | 2016-02-17 | Rolls Royce Plc | A rotor casing liner comprising multiple sections |
| US8985938B2 (en) * | 2011-12-13 | 2015-03-24 | United Technologies Corporation | Fan blade tip clearance control via Z-bands |
| US9228447B2 (en) * | 2012-02-14 | 2016-01-05 | United Technologies Corporation | Adjustable blade outer air seal apparatus |
| US9121302B2 (en) * | 2012-07-12 | 2015-09-01 | Hamilton Sundstrand Corporation | Radial compressor blade clearance control system |
| DE102012213016A1 (de) * | 2012-07-25 | 2014-01-30 | Siemens Aktiengesellschaft | Verfahren zur Minimierung des Spalts zwischen einem Läufer und einem Gehäuse |
| US9309776B2 (en) * | 2012-09-11 | 2016-04-12 | General Electric Company | Replaceable seals for turbine engine components and methods for installing the same |
| US20140161612A1 (en) * | 2012-12-07 | 2014-06-12 | General Electric Company | Tip shroud monitoring system, method, and controller |
| US9458731B2 (en) | 2013-03-13 | 2016-10-04 | General Electric Company | Turbine shroud cooling system |
| WO2014186002A2 (en) * | 2013-04-12 | 2014-11-20 | United Technologies Corporation | Rapid response clearance control system with spring assist for gas turbine engine |
| US9476318B2 (en) | 2013-09-03 | 2016-10-25 | General Electric Company | Systems and methods to monitor a rotating component |
| WO2015038906A1 (en) * | 2013-09-12 | 2015-03-19 | United Technologies Corporation | Blade tip clearance control system including boas support |
| US9488063B2 (en) * | 2013-09-12 | 2016-11-08 | General Electric Company | Clearance control system for a rotary machine and method of controlling a clearance |
| US9488060B2 (en) * | 2013-10-09 | 2016-11-08 | General Electric Company | Systems and methods for dynamically sealing a turbine engine |
| US9587511B2 (en) * | 2013-12-13 | 2017-03-07 | General Electric Company | Turbomachine cold clearance adjustment |
| US10364694B2 (en) * | 2013-12-17 | 2019-07-30 | United Technologies Corporation | Turbomachine blade clearance control system |
| US9567865B2 (en) * | 2014-04-08 | 2017-02-14 | Hamilton Sundstrand Corporation | Turbomachine blade clearance control system |
| US9708980B2 (en) | 2014-06-05 | 2017-07-18 | General Electric Company | Apparatus and system for compressor clearance control |
| FR3024751B1 (fr) * | 2014-08-05 | 2019-07-19 | Safran Aircraft Engines | Unite de commande pour le pilotage d'un jeu entre des sommets d'aubes et un anneau de turbine |
| US9810091B2 (en) * | 2014-08-12 | 2017-11-07 | United Technologies Corporation | Smart active clearance control between a rotor blade and a shroud |
| BE1022471B1 (fr) * | 2014-10-10 | 2016-04-15 | Techspace Aero S.A. | Carter externe de compresseur de turbomachine axiale avec joint d'etancheite |
| US9970315B2 (en) * | 2015-02-12 | 2018-05-15 | Hamilton Sundstrand Corporation | Movable vane control system |
| CN209033764U (zh) * | 2015-04-06 | 2019-06-28 | 特灵国际有限公司 | 螺杆压缩机中的主动间隙管理 |
| GB201507881D0 (en) * | 2015-05-08 | 2015-06-24 | Rolls Royce Plc | Turbine tip clearance |
| US9771821B1 (en) * | 2015-06-15 | 2017-09-26 | Florida Turbine Technologies, Inc. | Turbine interstage seal with self-balancing capability |
| US9995799B2 (en) * | 2015-07-14 | 2018-06-12 | The Boeing Company | System and method for magnetic characterization of induction heating wires |
| FR3040069B1 (fr) * | 2015-08-11 | 2017-09-01 | Snecma | Procede de detection d'une augmentation du regime d'une turbine basse pression d'un reacteur d'un aeronef au cours d'une phase de croisiere et dispositif et procede de regulation du debit d'air de refroidissement d'une turbine basse pression associes |
| FR3040070B1 (fr) * | 2015-08-11 | 2019-05-10 | Safran Aircraft Engines | Procede de detection d'une commande de poussee ascensionnelle d'un aeronef et dispositif et procede de regulation du debit d'air de refroidissement d'une turbine basse pression associes |
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| RU168262U1 (ru) * | 2016-01-22 | 2017-01-25 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" | Устройство регулирования радиального зазора надроторного пространства |
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| US10161258B2 (en) * | 2016-03-16 | 2018-12-25 | United Technologies Corporation | Boas rail shield |
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| KR102011370B1 (ko) * | 2018-03-20 | 2019-08-16 | 두산중공업 주식회사 | 가스 터빈 및 가스 터빈 제어 방법 |
| KR102087667B1 (ko) * | 2018-09-20 | 2020-03-11 | 두산중공업 주식회사 | 자력을 이용한 블레이드 고정 구조 및 이를 포함하는 가스터빈 |
| KR102113326B1 (ko) * | 2018-10-01 | 2020-05-21 | 두산중공업 주식회사 | 블레이드 일체형 탄성체를 이용한 블레이드 고정 구조 및 이를 포함하는 가스터빈 |
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| US11208912B2 (en) | 2018-12-13 | 2021-12-28 | General Electric Company | Turbine engine with floating shrouds |
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| DE102019216891A1 (de) * | 2019-10-31 | 2021-05-06 | Rolls-Royce Deutschland Ltd & Co Kg | Statorbaugruppe mit kippbarem Trägersegment |
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| US12241375B2 (en) | 2023-03-24 | 2025-03-04 | General Electric Company | Seal support assembly for a turbine engine |
| US12215588B2 (en) | 2023-03-27 | 2025-02-04 | General Electric Company | Seal assembly for a gas turbine engine |
| US12326089B2 (en) | 2023-04-24 | 2025-06-10 | General Electric Company | Seal assembly for a gas turbine engine |
| US20250075627A1 (en) * | 2023-09-05 | 2025-03-06 | General Electric Company | Systems and methods of active clearance control in a gas turbine engine |
| US12345163B2 (en) | 2023-11-17 | 2025-07-01 | Rolls-Royce Corporation | Travel stop for a tip clearance control system |
| US12345162B2 (en) | 2023-11-17 | 2025-07-01 | Rolls-Royce Corporation | Adjustable position impeller shroud for centrifugal compressors |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20010001845A1 (en) * | 1998-12-23 | 2001-05-24 | Khalid Syed J. | Method and apparatus for use in control of clearances in a gas turbine engine |
| US20050149274A1 (en) * | 2003-12-30 | 2005-07-07 | Finnigan Peter M. | Method and system for active tip clearance control in turbines |
| US20050286995A1 (en) * | 2004-06-23 | 2005-12-29 | Tonghuo Shang | Method and system for determining gas turbine tip clearance |
| GB2440744A (en) * | 2006-08-09 | 2008-02-13 | Rolls Royce Plc | Magnetically controlled blade clearance |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5263816A (en) | 1991-09-03 | 1993-11-23 | General Motors Corporation | Turbomachine with active tip clearance control |
| GB2336408B (en) | 1998-04-17 | 2002-07-24 | Rolls Royce Plc | A seal arrangement |
| GB2363864B (en) * | 2000-06-23 | 2004-08-18 | Rolls Royce Plc | A control arrangement |
| GB0028408D0 (en) * | 2000-11-22 | 2001-01-03 | Rolls Royce Plc | Seal apparatus |
| JP4434814B2 (ja) * | 2004-03-31 | 2010-03-17 | 本田技研工業株式会社 | ガスタービン・エンジンの制御装置 |
| US20080063513A1 (en) | 2006-09-08 | 2008-03-13 | Siemens Power Generation, Inc. | Turbine blade tip gap reduction system for a turbine engine |
| GB2466404B (en) * | 2007-11-21 | 2010-10-27 | Rolls Royce Plc | Turbomachine having an apparatus to measure the clearance between a rotor blade tip and a stator liner of a stator casing |
| US8177476B2 (en) * | 2009-03-25 | 2012-05-15 | General Electric Company | Method and apparatus for clearance control |
-
2009
- 2009-05-26 US US12/472,195 patent/US8186945B2/en not_active Expired - Fee Related
-
2010
- 2010-05-18 DE DE102010016995A patent/DE102010016995A1/de not_active Withdrawn
- 2010-05-20 JP JP2010115943A patent/JP2010276019A/ja not_active Withdrawn
- 2010-05-25 CH CH00810/10A patent/CH701149A2/de not_active Application Discontinuation
- 2010-05-26 CN CN201010197284XA patent/CN101899995A/zh active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US20010001845A1 (en) * | 1998-12-23 | 2001-05-24 | Khalid Syed J. | Method and apparatus for use in control of clearances in a gas turbine engine |
| US20050149274A1 (en) * | 2003-12-30 | 2005-07-07 | Finnigan Peter M. | Method and system for active tip clearance control in turbines |
| US20050286995A1 (en) * | 2004-06-23 | 2005-12-29 | Tonghuo Shang | Method and system for determining gas turbine tip clearance |
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| CN113757174A (zh) * | 2021-11-08 | 2021-12-07 | 中国航发上海商用航空发动机制造有限责任公司 | 一种机匣、压气机及压气机试验方法 |
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Also Published As
| Publication number | Publication date |
|---|---|
| CH701149A2 (de) | 2010-11-30 |
| JP2010276019A (ja) | 2010-12-09 |
| US20100303612A1 (en) | 2010-12-02 |
| DE102010016995A1 (de) | 2010-12-02 |
| US8186945B2 (en) | 2012-05-29 |
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