DE602004001306D1 - Äussere Luftabdichtungsanordnung - Google Patents
Äussere LuftabdichtungsanordnungInfo
- Publication number
- DE602004001306D1 DE602004001306D1 DE602004001306T DE602004001306T DE602004001306D1 DE 602004001306 D1 DE602004001306 D1 DE 602004001306D1 DE 602004001306 T DE602004001306 T DE 602004001306T DE 602004001306 T DE602004001306 T DE 602004001306T DE 602004001306 D1 DE602004001306 D1 DE 602004001306D1
- Authority
- DE
- Germany
- Prior art keywords
- external air
- sealing arrangement
- air sealing
- arrangement
- external
- 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.)
- Expired - Lifetime
Links
- 238000007789 sealing Methods 0.000 title 1
Classifications
-
- 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
- F16J15/441—Free-space packings with floating ring
- F16J15/442—Free-space packings with floating ring segmented
-
- 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
- F01D11/005—Sealing means between non relatively rotating elements
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US671291 | 2003-09-25 | ||
US10/671,291 US20050067788A1 (en) | 2003-09-25 | 2003-09-25 | Outer air seal assembly |
Publications (2)
Publication Number | Publication Date |
---|---|
DE602004001306D1 true DE602004001306D1 (de) | 2006-08-03 |
DE602004001306T2 DE602004001306T2 (de) | 2007-06-06 |
Family
ID=34194844
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602004001306T Expired - Lifetime DE602004001306T2 (de) | 2003-09-25 | 2004-08-03 | Äussere Luftabdichtungsanordnung |
Country Status (3)
Country | Link |
---|---|
US (1) | US20050067788A1 (de) |
EP (1) | EP1519010B1 (de) |
DE (1) | DE602004001306T2 (de) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004037356B4 (de) | 2004-07-30 | 2017-11-23 | Ansaldo Energia Ip Uk Limited | Wandstruktur zur Begrenzung eines Heißgaspfads |
US7665955B2 (en) * | 2006-08-17 | 2010-02-23 | Siemens Energy, Inc. | Vortex cooled turbine blade outer air seal for a turbine engine |
US7670108B2 (en) * | 2006-11-21 | 2010-03-02 | Siemens Energy, Inc. | Air seal unit adapted to be positioned adjacent blade structure in a gas turbine |
US8740224B2 (en) * | 2012-02-28 | 2014-06-03 | General Electric Company | Seal assembly for a turbomachine |
US20160194979A1 (en) * | 2013-09-06 | 2016-07-07 | United Technologies Corporation | Canted boas intersegment geometry |
US10180082B2 (en) * | 2014-06-05 | 2019-01-15 | Rolls-Royce Corporation | Fan case |
US10907651B2 (en) * | 2016-01-12 | 2021-02-02 | Rolls-Royce Corporation | Fan track liner subassembly angled upturn joint |
US11156117B2 (en) * | 2016-04-25 | 2021-10-26 | Raytheon Technologies Corporation | Seal arc segment with sloped circumferential sides |
GB2553565B (en) * | 2016-09-09 | 2019-04-10 | Rolls Royce Plc | Air riding seal arrangement |
FR3092867B1 (fr) * | 2019-02-19 | 2021-08-13 | Safran Aircraft Engines | Partie de turbomachine pour aeronef a languettes d’etancheite |
US11156116B2 (en) | 2019-04-08 | 2021-10-26 | Honeywell International Inc. | Turbine nozzle with reduced leakage feather seals |
US11125096B2 (en) * | 2019-05-03 | 2021-09-21 | Raytheon Technologies Corporation | CMC boas arrangement |
US11098612B2 (en) | 2019-11-18 | 2021-08-24 | Raytheon Technologies Corporation | Blade outer air seal including cooling trench |
US11384654B2 (en) | 2019-11-18 | 2022-07-12 | Raytheon Technologies Corporation | Mateface for blade outer air seals in a gas turbine engine |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2262382A (en) * | 1938-07-25 | 1941-11-11 | Hermes Patentverwertungs Gmbh | Labyrinth packing |
GB1493913A (en) * | 1975-06-04 | 1977-11-30 | Gen Motors Corp | Turbomachine stator interstage seal |
US3970318A (en) * | 1975-09-26 | 1976-07-20 | General Electric Company | Sealing means for a segmented ring |
CA1063139A (en) * | 1976-03-09 | 1979-09-25 | Westinghouse Electric Corporation | Variable radius springback wavy seal |
US4131388A (en) * | 1977-05-26 | 1978-12-26 | United Technologies Corporation | Outer air seal |
GB2092243B (en) * | 1981-01-31 | 1984-12-05 | Rolls Royce | Non-contacting gas seal |
JPS5877973A (ja) * | 1981-11-04 | 1983-05-11 | Hitachi Ltd | ラビリンス装置 |
US4557412A (en) * | 1983-12-05 | 1985-12-10 | United Technologies Corporation | Intersecting feather seals and construction thereof |
US4650394A (en) * | 1984-11-13 | 1987-03-17 | United Technologies Corporation | Coolable seal assembly for a gas turbine engine |
US5092735A (en) * | 1990-07-02 | 1992-03-03 | The United States Of America As Represented By The Secretary Of The Air Force | Blade outer air seal cooling system |
US5374161A (en) * | 1993-12-13 | 1994-12-20 | United Technologies Corporation | Blade outer air seal cooling enhanced with inter-segment film slot |
EP1260678B1 (de) * | 1997-09-15 | 2004-07-07 | ALSTOM Technology Ltd | Segmentanordnung für Plattformen |
JP3999395B2 (ja) * | 1999-03-03 | 2007-10-31 | 三菱重工業株式会社 | ガスタービン分割環 |
GB2356022B (en) * | 1999-11-02 | 2003-12-10 | Rolls Royce Plc | Gas turbine engines |
DE19963371A1 (de) * | 1999-12-28 | 2001-07-12 | Alstom Power Schweiz Ag Baden | Gekühltes Hitzeschild |
JP4719370B2 (ja) * | 2001-03-30 | 2011-07-06 | イーグル・エンジニアリング・エアロスペース株式会社 | ブラシシール装置 |
US6726448B2 (en) * | 2002-05-15 | 2004-04-27 | General Electric Company | Ceramic turbine shroud |
-
2003
- 2003-09-25 US US10/671,291 patent/US20050067788A1/en not_active Abandoned
-
2004
- 2004-08-03 EP EP04077224A patent/EP1519010B1/de not_active Expired - Lifetime
- 2004-08-03 DE DE602004001306T patent/DE602004001306T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1519010B1 (de) | 2006-06-21 |
US20050067788A1 (en) | 2005-03-31 |
EP1519010A1 (de) | 2005-03-30 |
DE602004001306T2 (de) | 2007-06-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |