CH525419A - Sealing device for turbo machines - Google Patents
Sealing device for turbo machinesInfo
- Publication number
- CH525419A CH525419A CH1878370A CH1878370A CH525419A CH 525419 A CH525419 A CH 525419A CH 1878370 A CH1878370 A CH 1878370A CH 1878370 A CH1878370 A CH 1878370A CH 525419 A CH525419 A CH 525419A
- Authority
- CH
- Switzerland
- Prior art keywords
- sealing device
- turbo machines
- turbo
- machines
- sealing
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- 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
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Devices (AREA)
- Gasket Seals (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1878370A CH525419A (en) | 1970-12-18 | 1970-12-18 | Sealing device for turbo machines |
DE2120171A DE2120171C3 (en) | 1970-12-18 | 1971-04-24 | Sealing arrangement for expansion gaps on turbo machines |
JP9895671A JPS5421883B1 (en) | 1970-12-18 | 1971-12-07 | |
US00207897A US3801220A (en) | 1970-12-18 | 1971-12-14 | Sealing element for a turbo-machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1878370A CH525419A (en) | 1970-12-18 | 1970-12-18 | Sealing device for turbo machines |
Publications (1)
Publication Number | Publication Date |
---|---|
CH525419A true CH525419A (en) | 1972-07-15 |
Family
ID=4435259
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH1878370A CH525419A (en) | 1970-12-18 | 1970-12-18 | Sealing device for turbo machines |
Country Status (4)
Country | Link |
---|---|
US (1) | US3801220A (en) |
JP (1) | JPS5421883B1 (en) |
CH (1) | CH525419A (en) |
DE (1) | DE2120171C3 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2758856A1 (en) * | 1997-01-30 | 1998-07-31 | Snecma | SEALING WITH STACKED INSERTS SLIDING IN RECEPTION SLOTS |
EP1914386A1 (en) * | 2006-10-17 | 2008-04-23 | Siemens Aktiengesellschaft | Turbine blade assembly |
WO2008074633A1 (en) | 2006-12-19 | 2008-06-26 | Alstom Technology Ltd | Turbomachine, particularly a gas turbine |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2816791C3 (en) * | 1977-05-03 | 1981-05-07 | Vereinigte Edelstahlwerke Ag (Vew), Wien | Cooled rotor for a turbine with an axial flow |
FR2404134A1 (en) * | 1977-09-23 | 1979-04-20 | Snecma | ROTOR FOR TURBOMACHINES |
CH626947A5 (en) * | 1978-03-02 | 1981-12-15 | Bbc Brown Boveri & Cie | |
JPS5896105A (en) * | 1981-12-03 | 1983-06-08 | Hitachi Ltd | Air-leakage prevention rotor at spacer top |
US4659289A (en) * | 1984-07-23 | 1987-04-21 | United Technologies Corporation | Turbine side plate assembly |
US4688988A (en) * | 1984-12-17 | 1987-08-25 | United Technologies Corporation | Coolable stator assembly for a gas turbine engine |
GB2171151B (en) * | 1985-02-20 | 1988-05-18 | Rolls Royce | Rotors for gas turbine engines |
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 |
US5374161A (en) * | 1993-12-13 | 1994-12-20 | United Technologies Corporation | Blade outer air seal cooling enhanced with inter-segment film slot |
JP2941698B2 (en) * | 1995-11-10 | 1999-08-25 | 三菱重工業株式会社 | Gas turbine rotor |
DE19654471B4 (en) * | 1996-12-27 | 2006-05-24 | Alstom | Rotor of a turbomachine |
JP3462695B2 (en) * | 1997-03-12 | 2003-11-05 | 三菱重工業株式会社 | Gas turbine blade seal plate |
DE59710924D1 (en) * | 1997-09-15 | 2003-12-04 | Alstom Switzerland Ltd | Cooling device for gas turbine components |
JP3462732B2 (en) * | 1997-10-21 | 2003-11-05 | 三菱重工業株式会社 | Double cross seal device for gas turbine vane |
DE19914227B4 (en) * | 1999-03-29 | 2007-05-10 | Alstom | Heat protection device in gas turbines |
DE50211431D1 (en) * | 2001-09-25 | 2008-02-07 | Alstom Technology Ltd | SEALING ARRANGEMENT FOR THE DENSITY PALL REDUCTION WITHIN A FLOW ROTATION MACHINE |
US6883807B2 (en) * | 2002-09-13 | 2005-04-26 | Seimens Westinghouse Power Corporation | Multidirectional turbine shim seal |
US7128522B2 (en) * | 2003-10-28 | 2006-10-31 | Pratt & Whitney Canada Corp. | Leakage control in a gas turbine engine |
US7562880B2 (en) * | 2004-02-09 | 2009-07-21 | Siemens Energy, Inc. | Seal usable between thermally movable components |
US7217081B2 (en) * | 2004-10-15 | 2007-05-15 | Siemens Power Generation, Inc. | Cooling system for a seal for turbine vane shrouds |
JP4822716B2 (en) * | 2005-02-07 | 2011-11-24 | 三菱重工業株式会社 | Gas turbine with seal structure |
US9534500B2 (en) * | 2011-04-27 | 2017-01-03 | Pratt & Whitney Canada Corp. | Seal arrangement for segmented gas turbine engine components |
RU2564741C2 (en) * | 2011-07-01 | 2015-10-10 | Альстом Текнолоджи Лтд | Turbine blade and turbine rotor |
US10822988B2 (en) * | 2015-12-21 | 2020-11-03 | Pratt & Whitney Canada Corp. | Method of sizing a cavity in a part |
US10494943B2 (en) * | 2016-02-03 | 2019-12-03 | General Electric Company | Spline seal for a gas turbine engine |
US10215043B2 (en) | 2016-02-24 | 2019-02-26 | United Technologies Corporation | Method and device for piston seal anti-rotation |
EP3438410B1 (en) | 2017-08-01 | 2021-09-29 | General Electric Company | Sealing system for a rotary machine |
US10907487B2 (en) | 2018-10-16 | 2021-02-02 | Honeywell International Inc. | Turbine shroud assemblies for gas turbine engines |
US12018567B2 (en) * | 2022-05-31 | 2024-06-25 | Pratt & Whitney Canada Corp. | Joint between gas turbine engine components with bonded fastener(s) |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2858103A (en) * | 1956-03-26 | 1958-10-28 | Westinghouse Electric Corp | Gas turbine apparatus |
-
1970
- 1970-12-18 CH CH1878370A patent/CH525419A/en not_active IP Right Cessation
-
1971
- 1971-04-24 DE DE2120171A patent/DE2120171C3/en not_active Expired
- 1971-12-07 JP JP9895671A patent/JPS5421883B1/ja active Pending
- 1971-12-14 US US00207897A patent/US3801220A/en not_active Expired - Lifetime
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2758856A1 (en) * | 1997-01-30 | 1998-07-31 | Snecma | SEALING WITH STACKED INSERTS SLIDING IN RECEPTION SLOTS |
EP0856640A1 (en) | 1997-01-30 | 1998-08-05 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Sealing consisting of stacked strip sliding freely in a slot |
US5997247A (en) * | 1997-01-30 | 1999-12-07 | Societe Nationale Detude Et De Construction De Mothers D'aviation "Snecma" | Seal of stacked thin slabs that slide within reception slots |
EP1914386A1 (en) * | 2006-10-17 | 2008-04-23 | Siemens Aktiengesellschaft | Turbine blade assembly |
WO2008046684A1 (en) | 2006-10-17 | 2008-04-24 | Siemens Aktiengesellschaft | Turbine blade assembly |
US8545181B2 (en) | 2006-10-17 | 2013-10-01 | Siemens Aktiengesellschaft | Turbine blade assembly |
WO2008074633A1 (en) | 2006-12-19 | 2008-06-26 | Alstom Technology Ltd | Turbomachine, particularly a gas turbine |
US8052382B2 (en) | 2006-12-19 | 2011-11-08 | Alstom Technology Ltd. | Turbo machine and gas turbine |
KR101426715B1 (en) | 2006-12-19 | 2014-08-06 | 알스톰 테크놀러지 리미티드 | Turbomachine, particularly a gas turbine |
Also Published As
Publication number | Publication date |
---|---|
DE2120171A1 (en) | 1972-06-22 |
DE2120171B2 (en) | 1973-06-14 |
US3801220A (en) | 1974-04-02 |
JPS5421883B1 (en) | 1979-08-02 |
DE2120171C3 (en) | 1974-01-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PL | Patent ceased |