EP1350925A3 - Sealing device in turbo machines - Google Patents
Sealing device in turbo machines Download PDFInfo
- Publication number
- EP1350925A3 EP1350925A3 EP02020928A EP02020928A EP1350925A3 EP 1350925 A3 EP1350925 A3 EP 1350925A3 EP 02020928 A EP02020928 A EP 02020928A EP 02020928 A EP02020928 A EP 02020928A EP 1350925 A3 EP1350925 A3 EP 1350925A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- sealing device
- bore
- turbo machines
- inner ring
- flow channel
- 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.)
- Granted
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
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
- F01D11/025—Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10214624A DE10214624C1 (en) | 2001-10-29 | 2002-04-02 | Seal device for turbomachine has heat elastic inner ring fitted to blade foot provided with cooled dovetail seal cooperating with rotor labyrinth |
DE10214624 | 2002-04-02 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1350925A2 EP1350925A2 (en) | 2003-10-08 |
EP1350925A3 true EP1350925A3 (en) | 2005-03-09 |
EP1350925B1 EP1350925B1 (en) | 2006-05-31 |
Family
ID=27816113
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP02020928A Expired - Lifetime EP1350925B1 (en) | 2002-04-02 | 2002-09-19 | Sealing device in turbo machines |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1350925B1 (en) |
AT (1) | ATE328191T1 (en) |
CA (1) | CA2421600C (en) |
DE (1) | DE50206992D1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2549397C1 (en) * | 2013-12-30 | 2015-04-27 | Открытое акционерное общество "Авиадвигатель" | High temperature gas turbine |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE202007004292U1 (en) * | 2007-03-23 | 2008-07-31 | Ghh-Rand Schraubenkompressoren Gmbh | Seal for shaft seals |
CN114087028B (en) * | 2021-11-12 | 2023-09-08 | 中国航发沈阳发动机研究所 | Be suitable for adjustable stator inner ring bleed air structure |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5217348A (en) * | 1992-09-24 | 1993-06-08 | United Technologies Corporation | Turbine vane assembly with integrally cast cooling fluid nozzle |
US5273396A (en) * | 1992-06-22 | 1993-12-28 | General Electric Company | Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud |
US5749701A (en) * | 1996-10-28 | 1998-05-12 | General Electric Company | Interstage seal assembly for a turbine |
EP0974733A2 (en) * | 1998-07-22 | 2000-01-26 | General Electric Company | Turbine nozzle having purge air circuit |
-
2002
- 2002-09-19 DE DE50206992T patent/DE50206992D1/en not_active Expired - Lifetime
- 2002-09-19 EP EP02020928A patent/EP1350925B1/en not_active Expired - Lifetime
- 2002-09-19 AT AT02020928T patent/ATE328191T1/en not_active IP Right Cessation
-
2003
- 2003-03-06 CA CA002421600A patent/CA2421600C/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5273396A (en) * | 1992-06-22 | 1993-12-28 | General Electric Company | Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud |
US5217348A (en) * | 1992-09-24 | 1993-06-08 | United Technologies Corporation | Turbine vane assembly with integrally cast cooling fluid nozzle |
US5749701A (en) * | 1996-10-28 | 1998-05-12 | General Electric Company | Interstage seal assembly for a turbine |
EP0974733A2 (en) * | 1998-07-22 | 2000-01-26 | General Electric Company | Turbine nozzle having purge air circuit |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2549397C1 (en) * | 2013-12-30 | 2015-04-27 | Открытое акционерное общество "Авиадвигатель" | High temperature gas turbine |
Also Published As
Publication number | Publication date |
---|---|
CA2421600A1 (en) | 2003-10-02 |
EP1350925B1 (en) | 2006-05-31 |
DE50206992D1 (en) | 2006-07-06 |
ATE328191T1 (en) | 2006-06-15 |
CA2421600C (en) | 2008-05-06 |
EP1350925A2 (en) | 2003-10-08 |
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