FI960920A - Arrangements cause damping of vibrations at the wings of a gas turbine or the like - Google Patents
Arrangements cause damping of vibrations at the wings of a gas turbine or the like Download PDFInfo
- Publication number
- FI960920A FI960920A FI960920A FI960920A FI960920A FI 960920 A FI960920 A FI 960920A FI 960920 A FI960920 A FI 960920A FI 960920 A FI960920 A FI 960920A FI 960920 A FI960920 A FI 960920A
- Authority
- FI
- Finland
- Prior art keywords
- gas turbine
- vibrations
- wings
- turbine
- cause damping
- Prior art date
Links
- 238000013016 damping Methods 0.000 title abstract 2
- 238000002485 combustion reaction Methods 0.000 abstract 1
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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/24—Blade-to-blade connections, e.g. for damping vibrations using wire or the like
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The arrangement for damping the blade vibrations in a turbine 1 which interacts with a gaseous medium, for example a gas turbine, the turbine in the turbocharger of an internal combustion engine or the like, by utilizing a relatively rigid wire unit or the like 4, which can be fitted in through 3 and connects the blades 2 and comprises two or more annular elements 4a-4k which are arranged in such a manner in relation to one another that the joining point between the ends 4', 4'' in each element is located in essentially different places in relation to the circumference of the wire unit or the like 4. Said annular elements 4c-4k are at least in part arranged within one another. <IMAGE>
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FI960920A FI100821B (en) | 1996-02-28 | 1996-02-28 | Arrangement for damping vibrations of a gas turbine or similar blades |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FI960920A FI100821B (en) | 1996-02-28 | 1996-02-28 | Arrangement for damping vibrations of a gas turbine or similar blades |
Publications (3)
Publication Number | Publication Date |
---|---|
FI960920A0 FI960920A0 (en) | 1996-02-28 |
FI960920A true FI960920A (en) | 1997-08-29 |
FI100821B FI100821B (en) | 1998-02-27 |
Family
ID=8545544
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FI960920A FI100821B (en) | 1996-02-28 | 1996-02-28 | Arrangement for damping vibrations of a gas turbine or similar blades |
Country Status (1)
Country | Link |
---|---|
FI (1) | FI100821B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2019057655A1 (en) * | 2017-09-20 | 2019-03-28 | Sulzer Turbo Services Venlo B.V. | Assembly of vane units |
-
1996
- 1996-02-28 FI FI960920A patent/FI100821B/en active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2019057655A1 (en) * | 2017-09-20 | 2019-03-28 | Sulzer Turbo Services Venlo B.V. | Assembly of vane units |
US11428106B2 (en) | 2017-09-20 | 2022-08-30 | Sulzer Management Ag | Assembly of vane units |
Also Published As
Publication number | Publication date |
---|---|
FI960920A0 (en) | 1996-02-28 |
FI100821B (en) | 1998-02-27 |
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