DE50206992D1 - Device for sealing turbomachinery - Google Patents
Device for sealing turbomachineryInfo
- Publication number
- DE50206992D1 DE50206992D1 DE50206992T DE50206992T DE50206992D1 DE 50206992 D1 DE50206992 D1 DE 50206992D1 DE 50206992 T DE50206992 T DE 50206992T DE 50206992 T DE50206992 T DE 50206992T DE 50206992 D1 DE50206992 D1 DE 50206992D1
- Authority
- DE
- Germany
- Prior art keywords
- bore
- turbomachinery
- sealing
- 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.)
- Expired - Lifetime
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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The seal device has a heat-elastic inner ring (3) fitted to the blade foot (14) of a turbine blade (1) provided with a dovetail seal (4) cooperating with a labyrinth (5) of the rotor (17). The cooling flow through the turbine blade communicates with a flow channel provided by a bore (15) extending through the inner ring to the dovetail seal, leading to a further flow channel provided by a radial bore (7) or a diagonal bore.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE50206992T DE50206992D1 (en) | 2002-04-02 | 2002-09-19 | Device for sealing turbomachinery |
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 |
DE50206992T DE50206992D1 (en) | 2002-04-02 | 2002-09-19 | Device for sealing turbomachinery |
Publications (1)
Publication Number | Publication Date |
---|---|
DE50206992D1 true DE50206992D1 (en) | 2006-07-06 |
Family
ID=27816113
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE50206992T Expired - Lifetime DE50206992D1 (en) | 2002-04-02 | 2002-09-19 | Device for sealing turbomachinery |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1350925B1 (en) |
AT (1) | ATE328191T1 (en) |
CA (1) | CA2421600C (en) |
DE (1) | DE50206992D1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE202007004292U1 (en) * | 2007-03-23 | 2008-07-31 | Ghh-Rand Schraubenkompressoren Gmbh | Seal for shaft seals |
RU2549397C1 (en) * | 2013-12-30 | 2015-04-27 | Открытое акционерное общество "Авиадвигатель" | High temperature gas turbine |
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 |
Family Cites Families (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 |
US6065928A (en) * | 1998-07-22 | 2000-05-23 | General Electric Company | Turbine nozzle having purge air circuit |
-
2002
- 2002-09-19 AT AT02020928T patent/ATE328191T1/en not_active IP Right Cessation
- 2002-09-19 DE DE50206992T patent/DE50206992D1/en not_active Expired - Lifetime
- 2002-09-19 EP EP02020928A patent/EP1350925B1/en not_active Expired - Lifetime
-
2003
- 2003-03-06 CA CA002421600A patent/CA2421600C/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CA2421600A1 (en) | 2003-10-02 |
ATE328191T1 (en) | 2006-06-15 |
CA2421600C (en) | 2008-05-06 |
EP1350925A2 (en) | 2003-10-08 |
EP1350925A3 (en) | 2005-03-09 |
EP1350925B1 (en) | 2006-05-31 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ATE551497T1 (en) | GAS TURBINE | |
PL1774140T3 (en) | Steam turbine, and method for the operation of a steam turbine | |
DE50312282D1 (en) | gas turbine | |
DK1609996T3 (en) | Scooters, especially for an axial fan | |
ATE396328T1 (en) | TURBOCHARGER WITH ADJUSTABLE GUIDE VANES | |
RU2004117218A (en) | GAS TURBINE STATOR | |
EP1096108A3 (en) | Stationary flowpath components for gas turbine engines | |
ATE547591T1 (en) | GUIDE VANE FOR AN AXIAL FLOW TURBO MACHINE AND ASSOCIATED GUIDE VANE ARRANGEMENT | |
ATE409279T1 (en) | TURBINES WITH A SLIDE FOR THE FLOW OF FOREIGN BODY | |
NO20082659L (en) | Radial compressor rotor | |
DE502005003367D1 (en) | ND OF A COOLING PHASE | |
EP1731717A3 (en) | Seal assembly for sealing space between stator and rotor in a gas turbine | |
FR2851010B1 (en) | DEVICE FOR VENTILATION OF A HIGH PRESSURE TURBINE ROTOR OF A TURBOMACHINE | |
EP1731766A3 (en) | Stator disc for turbomolecular pump | |
ATE392388T1 (en) | FILLING MACHINE OF ROTARY DESIGN | |
DE50206992D1 (en) | Device for sealing turbomachinery | |
EP2143881A3 (en) | Labyrinth seal for turbine blade dovetail root and corresponding sealing method | |
WO2018140130A3 (en) | Method and system for a gas turbine engine with a stage two blade cooling delivery circuit | |
ATE482326T1 (en) | FLOW MACHINE WITH A SPIRAL CHANNEL PROVIDED IN THE MIDDLE PART OF THE HOUSING | |
DE502004001950D1 (en) | Tool for machining | |
NO20035021L (en) | Device for circulating a sealing gas for mechanical dry seals in a centrifugal compressor at times when the machine is stationary and under pressure | |
DE502005005350D1 (en) | Mounting arrangement of a tube on a peripheral surface | |
DE10347842A1 (en) | Compressor and turbine wheel for a secondary air delivery unit is constituted as a single component with compressor and turbine blades | |
DK1336807T3 (en) | Sealing head for supplying a heat-carrying medium | |
DE50309583D1 (en) | External rotor motor with seal |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: MAN DIESEL & TURBO SE, 86153 AUGSBURG, DE |