MX161033A - Mejoras en sellos de lengueta y su metodo de fabricacion - Google Patents
Mejoras en sellos de lengueta y su metodo de fabricacionInfo
- Publication number
- MX161033A MX161033A MX203595A MX20359584A MX161033A MX 161033 A MX161033 A MX 161033A MX 203595 A MX203595 A MX 203595A MX 20359584 A MX20359584 A MX 20359584A MX 161033 A MX161033 A MX 161033A
- Authority
- MX
- Mexico
- Prior art keywords
- stamps
- tag
- manufacturing
- tag stamps
- Prior art date
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
-
- 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
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
- F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
-
- 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
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Gasket Seals (AREA)
- Sealing Devices (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/558,401 US4524980A (en) | 1983-12-05 | 1983-12-05 | Intersecting feather seals for interlocking gas turbine vanes |
Publications (1)
Publication Number | Publication Date |
---|---|
MX161033A true MX161033A (es) | 1990-07-11 |
Family
ID=24229399
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX203595A MX161033A (es) | 1983-12-05 | 1984-12-05 | Mejoras en sellos de lengueta y su metodo de fabricacion |
Country Status (8)
Country | Link |
---|---|
US (1) | US4524980A (es) |
EP (1) | EP0147354B1 (es) |
JP (1) | JPH0730684B2 (es) |
KR (1) | KR930007444B1 (es) |
BR (1) | BR8406182A (es) |
DE (2) | DE3462537D1 (es) |
IL (1) | IL73713A (es) |
MX (1) | MX161033A (es) |
Families Citing this family (51)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4749333A (en) * | 1986-05-12 | 1988-06-07 | The United States Of America As Represented By The Secretary Of The Air Force | Vane platform sealing and retention means |
US4767260A (en) * | 1986-11-07 | 1988-08-30 | United Technologies Corporation | Stator vane platform cooling means |
JPH03213602A (ja) * | 1990-01-08 | 1991-09-19 | General Electric Co <Ge> | ガスタービンエンジンの当接セグメントを連結する自己冷却式ジョイント連結構造 |
US5074748A (en) * | 1990-07-30 | 1991-12-24 | General Electric Company | Seal assembly for segmented turbine engine structures |
US5167488A (en) * | 1991-07-03 | 1992-12-01 | General Electric Company | Clearance control assembly having a thermally-controlled one-piece cylindrical housing for radially positioning shroud segments |
CA2070511C (en) * | 1991-07-22 | 2001-08-21 | Steven Milo Toborg | Turbine nozzle support |
US5188507A (en) * | 1991-11-27 | 1993-02-23 | General Electric Company | Low-pressure turbine shroud |
DE4215440A1 (de) * | 1992-05-11 | 1993-11-18 | Mtu Muenchen Gmbh | Einrichtung zur Bauteilabdichtung, insbesondere bei Turbomaschinen |
US5228835A (en) * | 1992-11-24 | 1993-07-20 | United Technologies Corporation | Gas turbine blade seal |
GB2296295A (en) * | 1994-12-23 | 1996-06-26 | Rolls Royce Plc | Sealing arrangement for a gas turbine engine |
FR2732416B1 (fr) * | 1995-03-29 | 1997-04-30 | Snecma | Agencement de raccordement de deux secteurs angulaires de turbomachine et joint concu pour servir dans cet agencement |
US5738490A (en) * | 1996-05-20 | 1998-04-14 | Pratt & Whitney Canada, Inc. | Gas turbine engine shroud seals |
US5709530A (en) * | 1996-09-04 | 1998-01-20 | United Technologies Corporation | Gas turbine vane seal |
US5868398A (en) * | 1997-05-20 | 1999-02-09 | United Technologies Corporation | Gas turbine stator vane seal |
JP3462732B2 (ja) * | 1997-10-21 | 2003-11-05 | 三菱重工業株式会社 | ガスタービン静翼のダブルクロスシール装置 |
US6162014A (en) * | 1998-09-22 | 2000-12-19 | General Electric Company | Turbine spline seal and turbine assembly containing such spline seal |
US6273683B1 (en) * | 1999-02-05 | 2001-08-14 | Siemens Westinghouse Power Corporation | Turbine blade platform seal |
US6343912B1 (en) * | 1999-12-07 | 2002-02-05 | General Electric Company | Gas turbine or jet engine stator vane frame |
GB0108398D0 (en) * | 2001-04-04 | 2001-05-23 | Siemens Ag | Seal element for sealing a gap and combustion turbine having a seal element |
US6971844B2 (en) * | 2003-05-29 | 2005-12-06 | General Electric Company | Horizontal joint sealing system for steam turbine diaphragm assemblies |
FR2869943B1 (fr) * | 2004-05-04 | 2006-07-28 | Snecma Moteurs Sa | Ensemble a anneau fixe d'une turbine a gaz |
EP1828545A2 (en) | 2004-12-01 | 2007-09-05 | United Technologies Corporation | Annular turbine ring rotor |
US7575415B2 (en) * | 2005-11-10 | 2009-08-18 | General Electric Company | Methods and apparatus for assembling turbine engines |
US7625174B2 (en) * | 2005-12-16 | 2009-12-01 | General Electric Company | Methods and apparatus for assembling gas turbine engine stator assemblies |
DE502006008991D1 (de) * | 2006-01-10 | 2011-04-14 | Siemens Ag | Verfahren zur Vorbereitung von Turbinenschaufeln mit einer Abdeckleiste mit Steckverbindung für eine anschließende Behandlung, sowie Turbinenschaufel dafür |
EP1991762B1 (de) * | 2006-03-06 | 2015-03-11 | Alstom Technology Ltd | Gasturbine mit ringförmigem hitzeschild und abgewinkelten dichtungsstreifen |
US7779866B2 (en) * | 2006-07-21 | 2010-08-24 | General Electric Company | Segmented trapped vortex cavity |
US7527472B2 (en) * | 2006-08-24 | 2009-05-05 | Siemens Energy, Inc. | Thermally sprayed conformal seal |
US7762780B2 (en) * | 2007-01-25 | 2010-07-27 | Siemens Energy, Inc. | Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies |
WO2009000802A2 (de) * | 2007-06-28 | 2008-12-31 | Alstom Technology Ltd | Leitschaufel für eine gasturbine |
US8182208B2 (en) * | 2007-07-10 | 2012-05-22 | United Technologies Corp. | Gas turbine systems involving feather seals |
US8308428B2 (en) * | 2007-10-09 | 2012-11-13 | United Technologies Corporation | Seal assembly retention feature and assembly method |
US8240985B2 (en) * | 2008-04-29 | 2012-08-14 | Pratt & Whitney Canada Corp. | Shroud segment arrangement for gas turbine engines |
US8727710B2 (en) | 2011-01-24 | 2014-05-20 | United Technologies Corporation | Mateface cooling feather seal assembly |
RU2536443C2 (ru) | 2011-07-01 | 2014-12-27 | Альстом Текнолоджи Лтд | Направляющая лопатка турбины |
GB201117084D0 (en) | 2011-10-05 | 2011-11-16 | Rolls Royce Plc | Strip seals |
EP2644834A1 (de) * | 2012-03-29 | 2013-10-02 | Siemens Aktiengesellschaft | Turbinenschaufel sowie zugehöriges Verfahren zum Herstellen einer Turbinenschaufel |
US10072517B2 (en) * | 2013-03-08 | 2018-09-11 | United Technologies Corporation | Gas turbine engine component having variable width feather seal slot |
EP3092372B1 (en) | 2014-01-08 | 2019-06-19 | United Technologies Corporation | Clamping seal for jet engine mid-turbine frame |
EP3099903B1 (en) | 2014-01-28 | 2020-04-22 | United Technologies Corporation | Seal for jet engine mid-turbine frame |
US10196913B1 (en) | 2014-12-17 | 2019-02-05 | United Technologies Corporation | Featherseal having tapered radial portion |
US10557360B2 (en) * | 2016-10-17 | 2020-02-11 | United Technologies Corporation | Vane intersegment gap sealing arrangement |
US10443420B2 (en) * | 2017-01-11 | 2019-10-15 | Rolls-Royce North American Technologies Inc. | Seal assembly for gas turbine engine components |
US10907491B2 (en) * | 2017-11-30 | 2021-02-02 | General Electric Company | Sealing system for a rotary machine and method of assembling same |
WO2019190541A1 (en) * | 2018-03-30 | 2019-10-03 | Siemens Aktiengesellschaft | Sealing arrangement between turbine shroud segments |
US10927692B2 (en) | 2018-08-06 | 2021-02-23 | General Electric Company | Turbomachinery sealing apparatus and method |
US11156116B2 (en) | 2019-04-08 | 2021-10-26 | Honeywell International Inc. | Turbine nozzle with reduced leakage feather seals |
US11111802B2 (en) * | 2019-05-01 | 2021-09-07 | Raytheon Technologies Corporation | Seal for a gas turbine engine |
US11187094B2 (en) * | 2019-08-26 | 2021-11-30 | General Electric Company | Spline for a turbine engine |
EP3789638A1 (en) * | 2019-09-05 | 2021-03-10 | Siemens Aktiengesellschaft | Seal for combustion apparatus |
US11519286B2 (en) | 2021-02-04 | 2022-12-06 | General Electric Company | Sealing assembly and sealing member therefor with spline seal retention |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3023998A (en) * | 1959-03-13 | 1962-03-06 | Jr Walter H Sanderson | Rotor blade retaining device |
US3144255A (en) * | 1961-07-14 | 1964-08-11 | Gen Electric | Sealing means utilizing leaf members |
GB1236366A (en) * | 1968-05-22 | 1971-06-23 | Westinghouse Electric Corp | Elastic fluid machine |
JPS5428696B2 (es) * | 1971-08-04 | 1979-09-18 | ||
US3728041A (en) * | 1971-10-04 | 1973-04-17 | Gen Electric | Fluidic seal for segmented nozzle diaphragm |
US3752598A (en) * | 1971-11-17 | 1973-08-14 | United Aircraft Corp | Segmented duct seal |
GB1358798A (en) * | 1972-06-09 | 1974-07-10 | Bbc Sulzer Turbomaschinen | Sealing element for a turbo-machine |
US3975114A (en) * | 1975-09-23 | 1976-08-17 | Westinghouse Electric Corporation | Seal arrangement for turbine diaphragms and the like |
US4257222A (en) * | 1977-12-21 | 1981-03-24 | United Technologies Corporation | Seal clearance control system for a gas turbine |
US4285633A (en) * | 1979-10-26 | 1981-08-25 | The United States Of America As Represented By The Secretary Of The Air Force | Broad spectrum vibration damper assembly fixed stator vanes of axial flow compressor |
-
1983
- 1983-12-05 US US06/558,401 patent/US4524980A/en not_active Expired - Lifetime
-
1984
- 1984-12-04 BR BR8406182A patent/BR8406182A/pt not_active IP Right Cessation
- 1984-12-04 DE DE8484630184T patent/DE3462537D1/de not_active Expired
- 1984-12-04 IL IL73713A patent/IL73713A/xx not_active IP Right Cessation
- 1984-12-04 DE DE198484630184T patent/DE147354T1/de active Pending
- 1984-12-04 EP EP84630184A patent/EP0147354B1/en not_active Expired
- 1984-12-05 JP JP59257299A patent/JPH0730684B2/ja not_active Expired - Lifetime
- 1984-12-05 MX MX203595A patent/MX161033A/es unknown
- 1984-12-05 KR KR1019840007665A patent/KR930007444B1/ko not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP0147354A1 (en) | 1985-07-03 |
JPS60138204A (ja) | 1985-07-22 |
KR930007444B1 (ko) | 1993-08-11 |
DE147354T1 (de) | 1986-01-30 |
IL73713A0 (en) | 1985-03-31 |
KR850004626A (ko) | 1985-07-25 |
EP0147354B1 (en) | 1987-03-04 |
JPH0730684B2 (ja) | 1995-04-10 |
BR8406182A (pt) | 1985-09-24 |
US4524980A (en) | 1985-06-25 |
DE3462537D1 (en) | 1987-04-09 |
IL73713A (en) | 1990-12-23 |
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