JPS5855360B2 - ブレ−ドプラットホ−ムの振動減衰装置 - Google Patents
ブレ−ドプラットホ−ムの振動減衰装置Info
- Publication number
- JPS5855360B2 JPS5855360B2 JP50013486A JP1348675A JPS5855360B2 JP S5855360 B2 JPS5855360 B2 JP S5855360B2 JP 50013486 A JP50013486 A JP 50013486A JP 1348675 A JP1348675 A JP 1348675A JP S5855360 B2 JPS5855360 B2 JP S5855360B2
- Authority
- JP
- Japan
- Prior art keywords
- damping device
- blade platform
- vibration damping
- platform
- blade
- 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
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
-
- 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
-
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration damping features
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US473680A US3881844A (en) | 1974-05-28 | 1974-05-28 | Blade platform vibration dampers |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS50153305A JPS50153305A (enFirst) | 1975-12-10 |
| JPS5855360B2 true JPS5855360B2 (ja) | 1983-12-09 |
Family
ID=23880555
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP50013486A Expired JPS5855360B2 (ja) | 1974-05-28 | 1975-02-03 | ブレ−ドプラットホ−ムの振動減衰装置 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3881844A (enFirst) |
| JP (1) | JPS5855360B2 (enFirst) |
| CA (1) | CA1013259A (enFirst) |
| DE (1) | DE2503513C2 (enFirst) |
| FR (1) | FR2275641A1 (enFirst) |
| GB (1) | GB1491557A (enFirst) |
| IT (1) | IT1031364B (enFirst) |
Families Citing this family (36)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA1114301A (en) * | 1979-06-27 | 1981-12-15 | Ivor J. Roberts | Locking device for blade mounting |
| FR2474095B1 (fr) * | 1980-01-17 | 1986-02-28 | Rolls Royce | Dispositif amortisseur de vibrations pour aubes mobiles de moteur a turbine a gaz |
| US4347040A (en) * | 1980-10-02 | 1982-08-31 | United Technologies Corporation | Blade to blade vibration damper |
| USRE32339E (en) * | 1980-10-02 | 1987-01-27 | United Technologies Corporation | Blade to blade vibration damper |
| GB2119026B (en) * | 1981-03-25 | 1984-06-20 | Rolls Royce | Aerofoil blade mounting |
| US4355957A (en) * | 1981-06-18 | 1982-10-26 | United Technologies Corporation | Blade damper |
| US4482297A (en) * | 1981-11-16 | 1984-11-13 | Terry Corporation | Bladed rotor assembly |
| GB2122691B (en) * | 1982-06-17 | 1985-05-01 | Rolls Royce | Mounting of aerofoil blades |
| US4767247A (en) * | 1987-02-24 | 1988-08-30 | Westinghouse Electric Corp. | Apparatus and method for preventing relative blade motion in steam turbine |
| GB2236809B (en) * | 1989-09-22 | 1994-03-16 | Rolls Royce Plc | Improvements in or relating to gas turbine engines |
| FR2674569A1 (fr) * | 1991-03-27 | 1992-10-02 | Snecma | Disque ailete monobloc avec amortissement des vibrations pour turbomachine. |
| FR2716931B1 (fr) * | 1994-03-03 | 1996-04-05 | Snecma | Système d'équilibrage et d'amortissement d'un dique de turbomachine. |
| DE4436729A1 (de) * | 1994-10-14 | 1996-04-18 | Abb Management Ag | Beschaufelter Rotor |
| JPH10325302A (ja) * | 1997-05-26 | 1998-12-08 | Ishikawajima Harima Heavy Ind Co Ltd | 動翼の制振構造 |
| US6494679B1 (en) * | 1999-08-05 | 2002-12-17 | General Electric Company | Apparatus and method for rotor damping |
| US6482533B2 (en) * | 2001-03-05 | 2002-11-19 | The Boeing Company | Article having imbedded cavity |
| US6901821B2 (en) * | 2001-11-20 | 2005-06-07 | United Technologies Corporation | Stator damper anti-rotation assembly |
| US6736602B2 (en) * | 2002-07-31 | 2004-05-18 | United Technologies Corporation | Hollow fan hub under blade bumper |
| EP1703080A1 (de) * | 2005-03-03 | 2006-09-20 | ALSTOM Technology Ltd | Rotierende Maschine |
| US8177502B2 (en) * | 2008-11-25 | 2012-05-15 | General Electric Company | Vane with reduced stress |
| US20100126018A1 (en) * | 2008-11-25 | 2010-05-27 | General Electric Company | Method of manufacturing a vane with reduced stress |
| JP5743072B2 (ja) * | 2011-03-25 | 2015-07-01 | 三菱日立パワーシステムズ株式会社 | タービン動翼の固定構造及びタービン動翼の脱着方法 |
| JP5579112B2 (ja) * | 2011-03-28 | 2014-08-27 | 三菱重工業株式会社 | タービン動翼の固定構造及び翼根バネの脱着方法 |
| EP2573327A1 (en) * | 2011-09-20 | 2013-03-27 | Siemens Aktiengesellschaft | Damping wire, corresponding rotor blade stage, steam turbine and producing method |
| RU2526129C2 (ru) * | 2012-09-10 | 2014-08-20 | Открытое акционерное общество "Омское моторостроительное конструкторское бюро" (ОАО ОМБК) | Рабочее колесо осевой турбомашины гтд |
| EP2806106A1 (de) | 2013-05-23 | 2014-11-26 | MTU Aero Engines GmbH | Turbomaschinenschaufel mit einem Impulskörper |
| US9765625B2 (en) * | 2013-05-23 | 2017-09-19 | MTU Aero Engines AG | Turbomachine blade |
| US20170067349A1 (en) * | 2015-09-03 | 2017-03-09 | General Electric Company | Damper pin for a turbine blade |
| US10584597B2 (en) | 2015-09-03 | 2020-03-10 | General Electric Company | Variable cross-section damper pin for a turbine blade |
| US10472975B2 (en) | 2015-09-03 | 2019-11-12 | General Electric Company | Damper pin having elongated bodies for damping adjacent turbine blades |
| US10443408B2 (en) * | 2015-09-03 | 2019-10-15 | General Electric Company | Damper pin for a turbine blade |
| US10385701B2 (en) | 2015-09-03 | 2019-08-20 | General Electric Company | Damper pin for a turbine blade |
| DE102016205997A1 (de) * | 2016-04-11 | 2017-10-12 | MTU Aero Engines AG | Leitschaufelsegment |
| US11208903B1 (en) | 2020-11-20 | 2021-12-28 | Solar Turbines Incorporated | Stiffness coupling and vibration damping for turbine blade shroud |
| US11976565B2 (en) * | 2022-07-27 | 2024-05-07 | Ge Infrastructure Technology Llc | Nested damper pin and vibration dampening system for turbine nozzle or blade |
| US12371998B2 (en) | 2023-06-29 | 2025-07-29 | Ge Infrastructure Technology Llc | Nested damper pin and vibration dampening system for turbine nozzle or blade |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1856786A (en) * | 1931-10-16 | 1932-05-03 | Gen Electric | Bucket wheel and like rotating member |
| US2840299A (en) * | 1952-09-22 | 1958-06-24 | Thompson Prod Inc | Axial flow compressor rotor |
| US2873088A (en) * | 1953-05-21 | 1959-02-10 | Gen Electric | Lightweight rotor construction |
-
1974
- 1974-05-28 US US473680A patent/US3881844A/en not_active Expired - Lifetime
-
1975
- 1975-01-24 GB GB3166/75A patent/GB1491557A/en not_active Expired
- 1975-01-29 DE DE2503513A patent/DE2503513C2/de not_active Expired
- 1975-01-31 IT IT19839/75A patent/IT1031364B/it active
- 1975-02-03 CA CA219,259A patent/CA1013259A/en not_active Expired
- 1975-02-03 JP JP50013486A patent/JPS5855360B2/ja not_active Expired
- 1975-05-28 FR FR7516712A patent/FR2275641A1/fr active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| GB1491557A (en) | 1977-11-09 |
| DE2503513C2 (de) | 1983-09-22 |
| IT1031364B (it) | 1979-04-30 |
| CA1013259A (en) | 1977-07-05 |
| DE2503513A1 (de) | 1975-12-11 |
| JPS50153305A (enFirst) | 1975-12-10 |
| FR2275641B1 (enFirst) | 1980-01-25 |
| US3881844A (en) | 1975-05-06 |
| FR2275641A1 (fr) | 1976-01-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS5855360B2 (ja) | ブレ−ドプラットホ−ムの振動減衰装置 | |
| JP3779760B2 (ja) | 軸流タービンエンジン用ロータ組立体 | |
| US5201850A (en) | Rotor tip shroud damper including damper wires | |
| KR101359788B1 (ko) | 터빈 버킷용 댐핑 시스템 | |
| JP2877837B2 (ja) | 軸流回転機用静翼アセンブリ及びこれに用いるスプリング | |
| US10344711B2 (en) | System and method of alleviating blade flutter | |
| US5681142A (en) | Damping means for a stator assembly of a gas turbine engine | |
| JP5965616B2 (ja) | タービンブレード組合せダンパ及びシールピン並びに関連する方法 | |
| US8157507B1 (en) | Damped stator assembly | |
| JP2002147203A (ja) | ターボ機械用の流体案内部材の列 | |
| JPS58107802A (ja) | ロ−タブレ−ドの振動エネルギ減衰装置 | |
| JP5681384B2 (ja) | タービンエンジン用のロータブレード | |
| US8087881B1 (en) | Damped stator assembly | |
| JPH1082301A (ja) | タービンブレードのダンパ及びシール | |
| JP2013537953A (ja) | ブレード配列、及び当該ブレード配列を具備するガスタービン | |
| JP2000511982A (ja) | タービン・ブレードのダンパ及びシール | |
| JP2005163789A (ja) | 軸流タービンの羽根のための振動減衰装置 | |
| US11421534B2 (en) | Damping device | |
| US3451654A (en) | Blade vibration damping | |
| US5215432A (en) | Stator vane damper | |
| US11346233B2 (en) | Damping device | |
| JPH0477121B2 (enFirst) | ||
| KR100584798B1 (ko) | 반경방향 진동 감쇠 댐퍼 | |
| JPH0411722B2 (enFirst) | ||
| JP6955021B2 (ja) | 向上した耐フラッタ性を備えるスナバ化翼 |