PL1852639T3 - Uszczelnienia pierścieniowe do bezstykowego uszczelniania płynów w turbozespole - Google Patents
Uszczelnienia pierścieniowe do bezstykowego uszczelniania płynów w turbozespoleInfo
- Publication number
- PL1852639T3 PL1852639T3 PL07251906T PL07251906T PL1852639T3 PL 1852639 T3 PL1852639 T3 PL 1852639T3 PL 07251906 T PL07251906 T PL 07251906T PL 07251906 T PL07251906 T PL 07251906T PL 1852639 T3 PL1852639 T3 PL 1852639T3
- Authority
- PL
- Poland
- Prior art keywords
- turbomachinery
- fluids
- annular seals
- contact sealing
- sealing
- Prior art date
Links
- 239000012530 fluid Substances 0.000 title 1
- 238000007789 sealing Methods 0.000 title 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
- 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
- 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
-
- 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
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/444—Free-space packings with facing materials having honeycomb-like structure
-
- 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
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/447—Labyrinth packings
- F16J15/4472—Labyrinth packings with axial path
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
- Gasket Seals (AREA)
- Mechanical Sealing (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US74658206P | 2006-05-05 | 2006-05-05 | |
| US11/744,332 US8074998B2 (en) | 2006-05-05 | 2007-05-04 | Annular seals for non-contact sealing of fluids in turbomachinery |
| EP07251906A EP1852639B1 (en) | 2006-05-05 | 2007-05-08 | Annular seals for non-contact sealing of fluids in turbomachinery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL1852639T3 true PL1852639T3 (pl) | 2013-10-31 |
Family
ID=38330698
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL07251906T PL1852639T3 (pl) | 2006-05-05 | 2007-05-08 | Uszczelnienia pierścieniowe do bezstykowego uszczelniania płynów w turbozespole |
Country Status (4)
| Country | Link |
|---|---|
| US (3) | US8074998B2 (pl) |
| EP (1) | EP1852639B1 (pl) |
| NO (1) | NO344306B1 (pl) |
| PL (1) | PL1852639T3 (pl) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8074998B2 (en) * | 2006-05-05 | 2011-12-13 | The Texas A&M University System | Annular seals for non-contact sealing of fluids in turbomachinery |
| NO330015B1 (no) * | 2009-06-22 | 2011-02-07 | Statoil Asa | Et aksialt gasskyvekraftlager for rotorer i roterende maskineri |
| WO2012129475A2 (en) | 2011-03-24 | 2012-09-27 | Dresser-Rand Company | Interlocking hole pattern seal |
| ITCO20110068A1 (it) | 2011-12-20 | 2013-06-21 | Nuovo Pignone Spa | Metodo e tenuta a nido d'ape |
| JP5931708B2 (ja) * | 2012-12-04 | 2016-06-08 | 三菱重工業株式会社 | シール装置及び回転機械 |
| US9879690B2 (en) * | 2013-06-06 | 2018-01-30 | Dresser-Rand Company | Compressor having hollow shaft |
| JP2016061252A (ja) * | 2014-09-19 | 2016-04-25 | 三菱重工業株式会社 | 回転機械 |
| WO2016137631A1 (en) * | 2015-02-23 | 2016-09-01 | Dresser-Rand Company | Non-contacting rotating member seal for a turbomachine |
| JP2017160861A (ja) * | 2016-03-10 | 2017-09-14 | 株式会社日立製作所 | ターボ機械 |
| CN107704652B (zh) * | 2017-08-29 | 2021-05-04 | 明阳智慧能源集团股份公司 | 一种风力发电机组轴承刚度计算工具 |
| US10533568B2 (en) * | 2017-10-30 | 2020-01-14 | Daikin Applied Americas Inc. | Centrifugal compressor with seal bearing |
| JP6783257B2 (ja) * | 2018-01-31 | 2020-11-11 | 三菱重工業株式会社 | 軸流回転機械 |
Family Cites Families (42)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1823310A (en) * | 1929-05-23 | 1931-09-15 | Westinghouse Electric & Mfg Co | Elastic fluid turbine |
| US3146992A (en) * | 1962-12-10 | 1964-09-01 | Gen Electric | Turbine shroud support structure |
| US3365172A (en) * | 1966-11-02 | 1968-01-23 | Gen Electric | Air cooled shroud seal |
| US3589475A (en) * | 1969-01-02 | 1971-06-29 | Gen Electric | Vibration damping means |
| US3649033A (en) * | 1969-12-24 | 1972-03-14 | Nippon Denso Co | Honeycomb rotor-sealing device and method of manufacture |
| US3603599A (en) * | 1970-05-06 | 1971-09-07 | Gen Motors Corp | Cooled seal |
| US4218066A (en) * | 1976-03-23 | 1980-08-19 | United Technologies Corporation | Rotary seal |
| US4053254A (en) * | 1976-03-26 | 1977-10-11 | United Technologies Corporation | Turbine case cooling system |
| US4063742A (en) * | 1976-08-18 | 1977-12-20 | Kentucky Metals, Inc. | Abradable fluid seal for aircraft gas turbines |
| GB2017228B (en) * | 1977-07-14 | 1982-05-06 | Pratt & Witney Aircraft Of Can | Shroud for a turbine rotor |
| US4162077A (en) * | 1977-12-28 | 1979-07-24 | United Technologies Corporation | Wide channel seal |
| US4242042A (en) * | 1978-05-16 | 1980-12-30 | United Technologies Corporation | Temperature control of engine case for clearance control |
| US4545586A (en) * | 1983-04-28 | 1985-10-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Damping seal for turbomachinery |
| US4512712A (en) * | 1983-08-01 | 1985-04-23 | United Technologies Corporation | Turbine stator assembly |
| FR2570763B1 (fr) * | 1984-09-27 | 1986-11-28 | Snecma | Dispositif de controle automatique du jeu d'un joint a labyrinthe de turbomachine |
| US4897021A (en) * | 1988-06-02 | 1990-01-30 | United Technologies Corporation | Stator vane asssembly for an axial flow rotary machine |
| US5281090A (en) * | 1990-04-03 | 1994-01-25 | General Electric Co. | Thermally-tuned rotary labyrinth seal with active seal clearance control |
| US5096376A (en) * | 1990-08-29 | 1992-03-17 | General Electric Company | Low windage corrugated seal facing strip |
| IE67360B1 (en) * | 1990-09-25 | 1996-03-20 | United Technologies Corp | Apparatus and method for a stator assembly of a rotary machine |
| US5190440A (en) * | 1991-03-11 | 1993-03-02 | Dresser-Rand Company | Swirl control labyrinth seal |
| US5161943A (en) * | 1991-03-11 | 1992-11-10 | Dresser-Rand Company, A General Partnership | Swirl control labyrinth seal |
| US5215435A (en) * | 1991-10-28 | 1993-06-01 | General Electric Company | Angled cooling air bypass slots in honeycomb seals |
| US5188507A (en) * | 1991-11-27 | 1993-02-23 | General Electric Company | Low-pressure turbine shroud |
| US5201846A (en) * | 1991-11-29 | 1993-04-13 | General Electric Company | Low-pressure turbine heat shield |
| US5702050A (en) * | 1995-04-28 | 1997-12-30 | Mitsubishi Jukogyo Kabushiki Kaisha | Method of brazing a honeycomb |
| EP0911491B1 (en) * | 1997-04-30 | 2007-09-05 | Mitsubishi Heavy Industries, Ltd. | High differential pressure end rotor seal |
| JP3477347B2 (ja) * | 1997-07-30 | 2003-12-10 | 三菱重工業株式会社 | ガスタービン段間部シール装置 |
| FR2804486B1 (fr) | 2000-02-02 | 2002-05-31 | Framatome Sa | Dispositif d'etancheite peripherique d'un element rotatif |
| US6341938B1 (en) * | 2000-03-10 | 2002-01-29 | General Electric Company | Methods and apparatus for minimizing thermal gradients within turbine shrouds |
| DE10140742B4 (de) * | 2000-12-16 | 2015-02-12 | Alstom Technology Ltd. | Vorrichtung zur Dichtspaltreduzierung zwischen einer rotierenden und einer stationären Komponente innerhalb einer axial durchströmten Strömungsmaschine |
| US6652226B2 (en) * | 2001-02-09 | 2003-11-25 | General Electric Co. | Methods and apparatus for reducing seal teeth wear |
| 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 |
| US6773225B2 (en) * | 2002-05-30 | 2004-08-10 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and method of bleeding gas therefrom |
| JP4285134B2 (ja) * | 2003-07-04 | 2009-06-24 | 株式会社Ihi | シュラウドセグメント |
| GB2418957B (en) * | 2003-10-22 | 2006-07-05 | Rolls Royce Plc | A liner for a gas turbine engine casing |
| US7334984B1 (en) * | 2003-12-24 | 2008-02-26 | Heico Corporation | Turbine shroud assembly with enhanced blade containment capabilities |
| GB0408825D0 (en) * | 2004-04-20 | 2004-05-26 | Rolls Royce Plc | A rotor blade containment assembly for a gas turbine engine |
| US8011883B2 (en) * | 2004-12-29 | 2011-09-06 | United Technologies Corporation | Gas turbine engine blade tip clearance apparatus and method |
| US8074998B2 (en) * | 2006-05-05 | 2011-12-13 | The Texas A&M University System | Annular seals for non-contact sealing of fluids in turbomachinery |
| US20080080972A1 (en) * | 2006-09-29 | 2008-04-03 | General Electric Company | Stationary-rotating assemblies having surface features for enhanced containment of fluid flow, and related processes |
| US7819625B2 (en) * | 2007-05-07 | 2010-10-26 | Siemens Energy, Inc. | Abradable CMC stacked laminate ring segment for a gas turbine |
| US20090014964A1 (en) * | 2007-07-09 | 2009-01-15 | Siemens Power Generation, Inc. | Angled honeycomb seal between turbine rotors and turbine stators in a turbine engine |
-
2007
- 2007-05-04 US US11/744,332 patent/US8074998B2/en not_active Expired - Fee Related
- 2007-05-07 NO NO20072345A patent/NO344306B1/no not_active IP Right Cessation
- 2007-05-08 EP EP07251906A patent/EP1852639B1/en not_active Not-in-force
- 2007-05-08 PL PL07251906T patent/PL1852639T3/pl unknown
-
2011
- 2011-12-09 US US13/315,973 patent/US8844936B2/en not_active Expired - Fee Related
-
2013
- 2013-12-11 US US14/102,749 patent/US9127564B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| NO20072345L (no) | 2007-11-06 |
| US20070257444A1 (en) | 2007-11-08 |
| EP1852639A1 (en) | 2007-11-07 |
| US8074998B2 (en) | 2011-12-13 |
| US9127564B2 (en) | 2015-09-08 |
| EP1852639B1 (en) | 2013-04-03 |
| US20120080853A1 (en) | 2012-04-05 |
| US8844936B2 (en) | 2014-09-30 |
| US20140219787A1 (en) | 2014-08-07 |
| NO344306B1 (no) | 2019-10-28 |
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