FR1024218A - Vibration damping device for propeller blades and turbine engine fins - Google Patents
Vibration damping device for propeller blades and turbine engine finsInfo
- Publication number
- FR1024218A FR1024218A FR1024218DA FR1024218A FR 1024218 A FR1024218 A FR 1024218A FR 1024218D A FR1024218D A FR 1024218DA FR 1024218 A FR1024218 A FR 1024218A
- Authority
- FR
- France
- Prior art keywords
- turbine engine
- vibration damping
- damping device
- propeller blades
- fins
- 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
Links
- 238000013016 damping Methods 0.000 title 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
- F01D5/14—Form or construction
- F01D5/16—Form or construction for counteracting blade vibration
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1024218T | 1950-09-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR1024218A true FR1024218A (en) | 1953-03-30 |
Family
ID=9578703
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1024218D Expired FR1024218A (en) | 1950-09-01 | 1950-09-01 | Vibration damping device for propeller blades and turbine engine fins |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR1024218A (en) |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2828941A (en) * | 1952-12-24 | 1958-04-01 | United Aircraft Corp | Blade damping means |
| US2933286A (en) * | 1954-09-15 | 1960-04-19 | Gen Electric | Damping turbine buckets |
| US2984453A (en) * | 1957-03-25 | 1961-05-16 | Westinghouse Electric Corp | Vibration damper for blading in elastic fluid apparatus |
| FR2465067A1 (en) * | 1979-09-15 | 1981-03-20 | Rolls Royce | DEVICE FOR DAMPING THE VIBRATIONS OF THE BLADES OF A TURBINE |
| FR2544381A1 (en) * | 1983-04-14 | 1984-10-19 | Gen Electric | ROTATING COMPONENT COMPRISING AUBES WITH MODIFIED TAVE D'ARONDE |
| US4776763A (en) * | 1987-12-02 | 1988-10-11 | Sundstrand Corporation | Mechanical damping of turbine wheel blades |
| FR2712631A1 (en) * | 1993-11-19 | 1995-05-24 | Gen Electric | Blade root for axial flow compressors and turbines |
| US5498137A (en) * | 1995-02-17 | 1996-03-12 | United Technologies Corporation | Turbine engine rotor blade vibration damping device |
| US5558497A (en) * | 1995-07-31 | 1996-09-24 | United Technologies Corporation | Airfoil vibration damping device |
| US5820343A (en) * | 1995-07-31 | 1998-10-13 | United Technologies Corporation | Airfoil vibration damping device |
| EP1640562A1 (en) * | 2004-09-23 | 2006-03-29 | Siemens Aktiengesellschaft | Frequency tuning method of a turbine blade and turbine blade |
| EP1892377A1 (en) * | 2006-08-16 | 2008-02-27 | Siemens Aktiengesellschaft | Turbomachine blade |
| WO2012095067A1 (en) * | 2010-11-16 | 2012-07-19 | Mtu Aero Engines Gmbh | Turbomachine blade having a tuning element |
| EP2484870A1 (en) * | 2011-02-08 | 2012-08-08 | MTU Aero Engines GmbH | Blade of a turbomachine with damping element and method of designing a turbomachine |
| EP2806105A1 (en) * | 2013-05-23 | 2014-11-26 | MTU Aero Engines GmbH | Blade of a turbomachine having an impulse body |
| EP2806106A1 (en) * | 2013-05-23 | 2014-11-26 | MTU Aero Engines GmbH | Blade of a turbomachine having an impulse body |
| FR3040194A1 (en) * | 2015-08-21 | 2017-02-24 | Snecma | INSTRUMED VEIN OF TURBOMACHINE |
| US9765625B2 (en) | 2013-05-23 | 2017-09-19 | MTU Aero Engines AG | Turbomachine blade |
| US20210123347A1 (en) * | 2019-10-23 | 2021-04-29 | Rolls-Royce Corporation | Gas turbine engine blades with airfoil plugs for selected tuning |
-
1950
- 1950-09-01 FR FR1024218D patent/FR1024218A/en not_active Expired
Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2828941A (en) * | 1952-12-24 | 1958-04-01 | United Aircraft Corp | Blade damping means |
| US2933286A (en) * | 1954-09-15 | 1960-04-19 | Gen Electric | Damping turbine buckets |
| US2984453A (en) * | 1957-03-25 | 1961-05-16 | Westinghouse Electric Corp | Vibration damper for blading in elastic fluid apparatus |
| FR2465067A1 (en) * | 1979-09-15 | 1981-03-20 | Rolls Royce | DEVICE FOR DAMPING THE VIBRATIONS OF THE BLADES OF A TURBINE |
| FR2544381A1 (en) * | 1983-04-14 | 1984-10-19 | Gen Electric | ROTATING COMPONENT COMPRISING AUBES WITH MODIFIED TAVE D'ARONDE |
| US4776763A (en) * | 1987-12-02 | 1988-10-11 | Sundstrand Corporation | Mechanical damping of turbine wheel blades |
| DE3840730A1 (en) * | 1987-12-02 | 1989-06-15 | Sundstrand Corp | DAMPED TURBINE WHEEL |
| FR2712631A1 (en) * | 1993-11-19 | 1995-05-24 | Gen Electric | Blade root for axial flow compressors and turbines |
| US5498137A (en) * | 1995-02-17 | 1996-03-12 | United Technologies Corporation | Turbine engine rotor blade vibration damping device |
| US5558497A (en) * | 1995-07-31 | 1996-09-24 | United Technologies Corporation | Airfoil vibration damping device |
| US5820343A (en) * | 1995-07-31 | 1998-10-13 | United Technologies Corporation | Airfoil vibration damping device |
| EP1640562A1 (en) * | 2004-09-23 | 2006-03-29 | Siemens Aktiengesellschaft | Frequency tuning method of a turbine blade and turbine blade |
| EP1892377A1 (en) * | 2006-08-16 | 2008-02-27 | Siemens Aktiengesellschaft | Turbomachine blade |
| WO2012095067A1 (en) * | 2010-11-16 | 2012-07-19 | Mtu Aero Engines Gmbh | Turbomachine blade having a tuning element |
| US9371733B2 (en) | 2010-11-16 | 2016-06-21 | Mtu Aero Engines Gmbh | Rotor blade arrangement for a turbo machine |
| EP2484870A1 (en) * | 2011-02-08 | 2012-08-08 | MTU Aero Engines GmbH | Blade of a turbomachine with damping element and method of designing a turbomachine |
| EP2806105A1 (en) * | 2013-05-23 | 2014-11-26 | MTU Aero Engines GmbH | Blade of a turbomachine having an impulse body |
| EP2806106A1 (en) * | 2013-05-23 | 2014-11-26 | MTU Aero Engines GmbH | Blade of a turbomachine having an impulse body |
| US9765625B2 (en) | 2013-05-23 | 2017-09-19 | MTU Aero Engines AG | Turbomachine blade |
| US9840916B2 (en) | 2013-05-23 | 2017-12-12 | MTU Aero Engines AG | Turbomachine blade |
| FR3040194A1 (en) * | 2015-08-21 | 2017-02-24 | Snecma | INSTRUMED VEIN OF TURBOMACHINE |
| US10513945B2 (en) | 2015-08-21 | 2019-12-24 | Safran Aircraft Engines | Instrumented flow passage of a turbine engine |
| US20210123347A1 (en) * | 2019-10-23 | 2021-04-29 | Rolls-Royce Corporation | Gas turbine engine blades with airfoil plugs for selected tuning |
| US11220913B2 (en) * | 2019-10-23 | 2022-01-11 | Rolls-Royce Corporation | Gas turbine engine blades with airfoil plugs for selected tuning |
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