AU4448100A - Honeycomb sealing preferably for steam turbine - Google Patents
Honeycomb sealing preferably for steam turbineInfo
- Publication number
- AU4448100A AU4448100A AU44481/00A AU4448100A AU4448100A AU 4448100 A AU4448100 A AU 4448100A AU 44481/00 A AU44481/00 A AU 44481/00A AU 4448100 A AU4448100 A AU 4448100A AU 4448100 A AU4448100 A AU 4448100A
- Authority
- AU
- Australia
- Prior art keywords
- steam turbine
- sealing preferably
- honeycomb sealing
- honeycomb
- 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.)
- Abandoned
Links
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- 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
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
-
- 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
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/28—Three-dimensional patterned
- F05D2250/283—Three-dimensional patterned honeycomb
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UA99031824 | 1999-03-31 | ||
UA99031824 | 1999-03-31 | ||
PCT/UA2000/000011 WO2000058607A1 (en) | 1999-03-31 | 2000-03-31 | Honeycomb sealing preferably for steam turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
AU4448100A true AU4448100A (en) | 2000-10-16 |
Family
ID=21689350
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU44481/00A Abandoned AU4448100A (en) | 1999-03-31 | 2000-03-31 | Honeycomb sealing preferably for steam turbine |
Country Status (3)
Country | Link |
---|---|
AU (1) | AU4448100A (en) |
RU (1) | RU2150627C1 (en) |
WO (1) | WO2000058607A1 (en) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6547522B2 (en) * | 2001-06-18 | 2003-04-15 | General Electric Company | Spring-backed abradable seal for turbomachinery |
DE102005002270A1 (en) * | 2005-01-18 | 2006-07-20 | Mtu Aero Engines Gmbh | engine |
FR2922589B1 (en) * | 2007-10-22 | 2009-12-04 | Snecma | CONTROL OF THE AUBES SET IN A HIGH-PRESSURE TURBINE TURBINE |
RU2362887C1 (en) * | 2008-08-06 | 2009-07-27 | Александр Степанович Лисянский | Labyrinth over-strip sealing for steam turbine |
US20130017072A1 (en) * | 2011-07-14 | 2013-01-17 | General Electric Company | Pattern-abradable/abrasive coatings for steam turbine stationary component surfaces |
DE102012200883B4 (en) | 2012-01-23 | 2015-12-03 | MTU Aero Engines AG | Dynamic-seal assembly |
DE102012201050B4 (en) * | 2012-01-25 | 2017-11-30 | MTU Aero Engines AG | Sealing arrangement, method and turbomachine |
JP2014020509A (en) * | 2012-07-20 | 2014-02-03 | Toshiba Corp | Seal device, axial flow turbine, and power-generating plant |
FR3007065B1 (en) * | 2013-06-14 | 2017-11-10 | Snecma | ABRADABLE RING FOR TURBOMACHINE |
RU2531312C1 (en) * | 2013-07-16 | 2014-10-20 | Открытое акционерное общество "Научно-производственное объдинение "Сатурн" | Production of cellular filler |
FR3073890B1 (en) * | 2017-11-21 | 2021-01-22 | Safran Aircraft Engines | ABRADABLE LABYRINTH SEAL, ESPECIALLY FOR AIRCRAFT TURBINE |
RU190835U1 (en) * | 2019-02-07 | 2019-07-15 | Сергей Владимирович Ушинин | CELLULAR PRIVAL SEAL OF STEAM TURBINE |
RU2719751C2 (en) * | 2019-12-14 | 2020-04-23 | Акционерное Общество "Ротек" | Honeycomb seal of turbomachine |
RU195872U1 (en) * | 2019-12-18 | 2020-02-07 | Акционерное Общество "Ротек" | CELLULAR TURBO SEAL |
RU2756879C2 (en) * | 2020-12-17 | 2021-10-06 | Акционерное Общество "Ротек" | Turbomachine radial clearance seal |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3867060A (en) * | 1973-09-27 | 1975-02-18 | Gen Electric | Shroud assembly |
FR2552159B1 (en) * | 1983-09-21 | 1987-07-10 | Snecma | DEVICE FOR CONNECTING AND SEALING TURBINE STATOR BLADE SECTIONS |
SU1182224A1 (en) | 1984-04-05 | 1985-09-30 | Предприятие П/Я Р-6977 | Shaft labyrinth packing |
FR2583493B1 (en) * | 1985-06-14 | 1989-06-30 | Alsthom Atlantique | ALVEOLE PRODUCT FOR TURBOMACHINE SEALING |
EP0536575B1 (en) * | 1991-10-08 | 1995-04-05 | Asea Brown Boveri Ag | Shroud band for axial flow turbine |
JP3477347B2 (en) * | 1997-07-30 | 2003-12-10 | 三菱重工業株式会社 | Gas turbine interstage seal device |
-
1999
- 1999-10-27 RU RU99122620A patent/RU2150627C1/en active
-
2000
- 2000-03-31 WO PCT/UA2000/000011 patent/WO2000058607A1/en active Application Filing
- 2000-03-31 AU AU44481/00A patent/AU4448100A/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
RU2150627C1 (en) | 2000-06-10 |
WO2000058607A1 (en) | 2000-10-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MK6 | Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase |