AU2001258097A1 - Turbomachine with rotor-shroud seal structure - Google Patents
Turbomachine with rotor-shroud seal structureInfo
- Publication number
- AU2001258097A1 AU2001258097A1 AU2001258097A AU5809701A AU2001258097A1 AU 2001258097 A1 AU2001258097 A1 AU 2001258097A1 AU 2001258097 A AU2001258097 A AU 2001258097A AU 5809701 A AU5809701 A AU 5809701A AU 2001258097 A1 AU2001258097 A1 AU 2001258097A1
- Authority
- AU
- Australia
- Prior art keywords
- turbomachine
- rotor
- seal structure
- shroud seal
- shroud
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
- F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
- F04D29/326—Rotors specially for elastic fluids for axial flow pumps for axial flow fans comprising a rotating shroud
-
- 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
- F05D2240/00—Components
- F05D2240/55—Seals
- F05D2240/56—Brush seals
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Sealing Devices (AREA)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US20141600P | 2000-05-03 | 2000-05-03 | |
US60201416 | 2000-05-03 | ||
US09645773 | 2000-08-25 | ||
US09/645,773 US6471472B1 (en) | 2000-05-03 | 2000-08-25 | Turbomachine shroud fibrous tip seal |
PCT/CA2001/000641 WO2001083950A1 (en) | 2000-05-03 | 2001-05-02 | Turbomachine with rotor-shroud seal structure |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2001258097A1 true AU2001258097A1 (en) | 2001-11-12 |
Family
ID=26896723
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2001258097A Abandoned AU2001258097A1 (en) | 2000-05-03 | 2001-05-02 | Turbomachine with rotor-shroud seal structure |
Country Status (6)
Country | Link |
---|---|
US (1) | US6471472B1 (ja) |
EP (1) | EP1278943B1 (ja) |
JP (1) | JP2003532013A (ja) |
AU (1) | AU2001258097A1 (ja) |
DE (1) | DE60115416T2 (ja) |
WO (1) | WO2001083950A1 (ja) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6899339B2 (en) * | 2001-08-30 | 2005-05-31 | United Technologies Corporation | Abradable seal having improved durability |
US6874990B2 (en) * | 2003-01-29 | 2005-04-05 | Siemens Vdo Automotive Inc. | Integral tip seal in a fan-shroud structure |
US20070231128A1 (en) * | 2006-03-31 | 2007-10-04 | Caterpiller Inc. | Fan assembly |
DE102007037855A1 (de) | 2007-08-10 | 2009-02-12 | Rolls-Royce Deutschland Ltd & Co Kg | Schaufeldeckband mit Sperrstrahlerzeugung |
US9822650B2 (en) | 2011-04-28 | 2017-11-21 | Hamilton Sundstrand Corporation | Turbomachine shroud |
EP2959113B1 (en) | 2013-02-23 | 2018-10-31 | Rolls-Royce Corporation | Edge seal for gas turbine engine ceramic matrix composite component |
US20150285259A1 (en) * | 2014-04-05 | 2015-10-08 | Arthur John Wennerstrom | Filament-Wound Tip-Shrouded Axial Compressor or Fan Rotor System |
US10233764B2 (en) * | 2015-10-12 | 2019-03-19 | Rolls-Royce North American Technologies Inc. | Fabric seal and assembly for gas turbine engine |
EP3239533A1 (de) | 2016-04-29 | 2017-11-01 | STEINBEIS GMBH & CO. Für TECHNOLOGIETRANSFER | Axiale turbomaschine |
WO2018058068A1 (en) * | 2016-09-23 | 2018-03-29 | Federal-Mogul Powertrain Llc | Radial shaft seal assembly with debris exclusion member and method of construction thereof |
Family Cites Families (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2051912A5 (ja) | 1969-07-01 | 1971-04-09 | Rabouyt Denis | |
US3719365A (en) | 1971-10-18 | 1973-03-06 | Gen Motors Corp | Seal structure |
US3779341A (en) | 1972-10-16 | 1973-12-18 | Modine Mfg Co | Noise suppressive fan shroud |
US3970319A (en) | 1972-11-17 | 1976-07-20 | General Motors Corporation | Seal structure |
US3834001A (en) | 1972-11-17 | 1974-09-10 | Gen Motors Corp | Method of making a porous laminated seal element |
US3799128A (en) * | 1973-03-08 | 1974-03-26 | Gen Motors Corp | Engine cooling system radiator and fan shroud |
US4181172A (en) | 1977-07-01 | 1980-01-01 | General Motors Corporation | Fan shroud arrangement |
US4213426A (en) * | 1978-11-09 | 1980-07-22 | General Motors Corporation | Shrouding for engine mounted cooling fan |
US4247247A (en) | 1979-05-29 | 1981-01-27 | General Motors Corporation | Blade tip clearance control |
JPS5688992A (en) | 1979-12-21 | 1981-07-18 | Aisin Seiki Co Ltd | Axial fan for cooling internal combustion engine |
US4406581A (en) | 1980-12-30 | 1983-09-27 | Hayes-Albion Corp. | Shrouded fan assembly |
US4398508A (en) | 1981-02-20 | 1983-08-16 | Volvo White Truck Corporation | Engine cooling fan construction |
DE3716718A1 (de) * | 1986-05-19 | 1987-11-26 | Usui Kokusai Sangyo Kk | Blaetter fuer niedriggeschwindigkeits-propellerventilatoren |
DE8614073U1 (de) | 1986-05-24 | 1988-04-07 | Daimler-Benz Ag | Kühleinrichtung an einer Brennkraftmaschine |
US4728257A (en) | 1986-06-18 | 1988-03-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal stress minimized, two component, turbine shroud seal |
GB2212228B (en) | 1987-11-13 | 1991-08-07 | Rolls Royce Plc | Enhanced performance brush seals |
US4989886A (en) * | 1988-12-30 | 1991-02-05 | Textron Inc. | Braided filamentary sealing element |
JPH0755293Y2 (ja) | 1989-06-28 | 1995-12-20 | アイシン化工株式会社 | 熱交換器用冷却装置 |
US5106104A (en) | 1990-10-11 | 1992-04-21 | General Electric Company | Constant pressure drop multiple stage brush seal |
US5489186A (en) | 1991-08-30 | 1996-02-06 | Airflow Research And Manufacturing Corp. | Housing with recirculation control for use with banded axial-flow fans |
US5183382A (en) | 1991-09-03 | 1993-02-02 | Caterpillar Inc. | Low noise rotating fan and shroud assembly |
US5335920A (en) | 1992-08-20 | 1994-08-09 | General Electric Company | Brush seal |
US5342167A (en) | 1992-10-09 | 1994-08-30 | Airflow Research And Manufacturing Corporation | Low noise fan |
US5749584A (en) | 1992-11-19 | 1998-05-12 | General Electric Company | Combined brush seal and labyrinth seal segment for rotary machines |
US5474306A (en) | 1992-11-19 | 1995-12-12 | General Electric Co. | Woven seal and hybrid cloth-brush seals for turbine applications |
DE4310104C2 (de) * | 1993-03-27 | 1997-04-30 | Deutsche Forsch Luft Raumfahrt | Verfahren zur Reduzierung der Schallemission sowie zur Verbesserung der Luftleistung und des Wirkungsgrads bei einer axialen Strömungsmaschine und Strömungsmaschine |
GB9317083D0 (en) | 1993-08-17 | 1993-09-29 | Rolls Royce Plc | A brush seal |
US5522698A (en) | 1994-04-29 | 1996-06-04 | United Technologies Corporation | Brush seal support and vane assembly windage cover |
US5498139A (en) | 1994-11-09 | 1996-03-12 | United Technologies Corporation | Brush seal |
DE19532701C2 (de) * | 1995-09-05 | 2000-01-05 | Freudenberg Carl Fa | Lippendichtring |
US5980203A (en) | 1996-06-05 | 1999-11-09 | Atlas Compco Comptec | Spark-prevention coating for oxygen compressor shroud |
US6079945A (en) | 1997-11-10 | 2000-06-27 | Geneal Electric Company | Brush seal for high-pressure rotor applications |
DE19803502B4 (de) | 1998-01-30 | 2006-01-05 | Behr Gmbh & Co. Kg | Lüfteranordnung |
US6036437A (en) | 1998-04-03 | 2000-03-14 | General Electric Co. | Bucket cover geometry for brush seal applications |
US6053699A (en) | 1998-07-27 | 2000-04-25 | General Electric Company | Steam turbine having a brush seal assembly |
US5971400A (en) | 1998-08-10 | 1999-10-26 | General Electric Company | Seal assembly and rotary machine containing such seal assembly |
US6030175A (en) | 1998-09-23 | 2000-02-29 | General Electric Company | Hybrid seal and rotary machine containing such hybrid seal |
-
2000
- 2000-08-25 US US09/645,773 patent/US6471472B1/en not_active Expired - Fee Related
-
2001
- 2001-05-02 EP EP01931264A patent/EP1278943B1/en not_active Expired - Lifetime
- 2001-05-02 AU AU2001258097A patent/AU2001258097A1/en not_active Abandoned
- 2001-05-02 WO PCT/CA2001/000641 patent/WO2001083950A1/en active IP Right Grant
- 2001-05-02 JP JP2001580547A patent/JP2003532013A/ja active Pending
- 2001-05-02 DE DE2001615416 patent/DE60115416T2/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1278943A1 (en) | 2003-01-29 |
EP1278943B1 (en) | 2005-11-30 |
WO2001083950A1 (en) | 2001-11-08 |
US6471472B1 (en) | 2002-10-29 |
DE60115416T2 (de) | 2006-06-29 |
JP2003532013A (ja) | 2003-10-28 |
DE60115416D1 (de) | 2006-01-05 |
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