FR2358545A1 - Perfectionnements aux dispositifs d'equilibrage de rotors - Google Patents
Perfectionnements aux dispositifs d'equilibrage de rotorsInfo
- Publication number
- FR2358545A1 FR2358545A1 FR7622779A FR7622779A FR2358545A1 FR 2358545 A1 FR2358545 A1 FR 2358545A1 FR 7622779 A FR7622779 A FR 7622779A FR 7622779 A FR7622779 A FR 7622779A FR 2358545 A1 FR2358545 A1 FR 2358545A1
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- balancing
- disc
- fixing grooves
- groove
- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
- F16F15/34—Fastening arrangements therefor
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/027—Arrangements for balancing
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/30—Compensating imbalance
- G01M1/32—Compensating imbalance by adding material to the body to be tested, e.g. by correcting-weights
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- General Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Rotor de machine axiale, notamment de compresseur axial, à disque porteur, aubes amovibles et masselottes d'équilibrage. Le pourtour du disque comportant des rainures à parois en contre-dépouille dans lesquelles sont insérés les pieds prismatiques des aubes, les masselottes comportent aussi des pieds prismatiques en vue de leur insertion dans des espaces de rainures non occupés par les pieds d'aubes. Compresseurs pour turbo-réacteurs.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7622779A FR2358545A1 (fr) | 1976-07-16 | 1976-07-16 | Perfectionnements aux dispositifs d'equilibrage de rotors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7622779A FR2358545A1 (fr) | 1976-07-16 | 1976-07-16 | Perfectionnements aux dispositifs d'equilibrage de rotors |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2358545A1 true FR2358545A1 (fr) | 1978-02-10 |
FR2358545B1 FR2358545B1 (fr) | 1978-12-15 |
Family
ID=9176152
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7622779A Granted FR2358545A1 (fr) | 1976-07-16 | 1976-07-16 | Perfectionnements aux dispositifs d'equilibrage de rotors |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2358545A1 (fr) |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4470756A (en) * | 1982-04-08 | 1984-09-11 | S.N.E.C.M.A. | Device for axial securing of blade feet of a gas turbine disk |
FR2545873A1 (fr) * | 1983-05-09 | 1984-11-16 | Gen Electric | Dispositif d'equilibrage pour aube en queue d'aronde de rotor |
US4685863A (en) * | 1979-06-27 | 1987-08-11 | United Technologies Corporation | Turbine rotor assembly |
JPH01147103A (ja) * | 1987-10-27 | 1989-06-08 | United Technol Corp <Utc> | ガスタービンロータのバランシング装置 |
US4846628A (en) * | 1988-12-23 | 1989-07-11 | United Technologies Corporation | Rotor assembly for a turbomachine |
US4940389A (en) * | 1987-12-19 | 1990-07-10 | Mtu Motoren- Und Turbinen-Union Munich Gmbh | Assembly of rotor blades in a rotor disc for a compressor or a turbine |
FR2645902A1 (fr) * | 1989-04-17 | 1990-10-19 | Gen Electric | Masselotte d'equilibrage sans boulons pour des rotors de turbine |
US5112193A (en) * | 1990-09-11 | 1992-05-12 | Pratt & Whitney Canada | Fan blade axial retention device |
EP1239059A2 (fr) * | 2001-03-07 | 2002-09-11 | General Electric Company | Usinage chimique des aubes d'un moteur à turbine à gaz |
EP1808573A1 (fr) * | 2006-01-13 | 2007-07-18 | Snecma | Masselotte d'équilibrage, disque de rotor en étant équipe, rotor et moteur d'aéronef les comportant |
US7252481B2 (en) * | 2004-05-14 | 2007-08-07 | Pratt & Whitney Canada Corp. | Natural frequency tuning of gas turbine engine blades |
US9145772B2 (en) | 2012-01-31 | 2015-09-29 | United Technologies Corporation | Compressor disk bleed air scallops |
FR3021689A1 (fr) * | 2014-05-28 | 2015-12-04 | Snecma | Disque de turbomachine et procede pour son equilibrage |
US9404367B2 (en) | 2012-11-21 | 2016-08-02 | Solar Turbines Incorporated | Gas turbine engine compressor rotor assembly and balancing system |
EP2253800A3 (fr) * | 2009-05-19 | 2017-05-17 | Rolls-Royce plc | Rotor équilibré pour moteur de turbine |
EP3611338A3 (fr) * | 2018-08-14 | 2020-03-18 | United Technologies Corporation | Système de poids d'équilibrage de rotor en queue d'aronde |
FR3096105A1 (fr) * | 2019-05-16 | 2020-11-20 | Safran Aircraft Engines | rotor de turbomachine à gaz à masselotte |
CN112160794A (zh) * | 2020-09-18 | 2021-01-01 | 中国航发四川燃气涡轮研究院 | 定位组件及其涡轮盘或压气机盘、航空发动机 |
CN113915163A (zh) * | 2021-10-12 | 2022-01-11 | 浙江意动科技股份有限公司 | 一种压气机转子叶片连接结构 |
-
1976
- 1976-07-16 FR FR7622779A patent/FR2358545A1/fr active Granted
Non-Patent Citations (1)
Title |
---|
NEANT * |
Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4685863A (en) * | 1979-06-27 | 1987-08-11 | United Technologies Corporation | Turbine rotor assembly |
US4470756A (en) * | 1982-04-08 | 1984-09-11 | S.N.E.C.M.A. | Device for axial securing of blade feet of a gas turbine disk |
FR2545873A1 (fr) * | 1983-05-09 | 1984-11-16 | Gen Electric | Dispositif d'equilibrage pour aube en queue d'aronde de rotor |
JPH01147103A (ja) * | 1987-10-27 | 1989-06-08 | United Technol Corp <Utc> | ガスタービンロータのバランシング装置 |
US4940389A (en) * | 1987-12-19 | 1990-07-10 | Mtu Motoren- Und Turbinen-Union Munich Gmbh | Assembly of rotor blades in a rotor disc for a compressor or a turbine |
US4846628A (en) * | 1988-12-23 | 1989-07-11 | United Technologies Corporation | Rotor assembly for a turbomachine |
FR2645902A1 (fr) * | 1989-04-17 | 1990-10-19 | Gen Electric | Masselotte d'equilibrage sans boulons pour des rotors de turbine |
US5112193A (en) * | 1990-09-11 | 1992-05-12 | Pratt & Whitney Canada | Fan blade axial retention device |
EP1239059A2 (fr) * | 2001-03-07 | 2002-09-11 | General Electric Company | Usinage chimique des aubes d'un moteur à turbine à gaz |
EP1239059A3 (fr) * | 2001-03-07 | 2003-08-27 | General Electric Company | Usinage chimique des aubes d'un moteur à turbine à gaz |
US7252481B2 (en) * | 2004-05-14 | 2007-08-07 | Pratt & Whitney Canada Corp. | Natural frequency tuning of gas turbine engine blades |
EP1808573A1 (fr) * | 2006-01-13 | 2007-07-18 | Snecma | Masselotte d'équilibrage, disque de rotor en étant équipe, rotor et moteur d'aéronef les comportant |
US7753651B2 (en) | 2006-01-13 | 2010-07-13 | Snecma | Balancing flyweight, rotor disk equipped therewith, rotor and aircraft engine comprising them |
FR2896289A1 (fr) * | 2006-01-13 | 2007-07-20 | Snecma Sa | Masselotte d'equilibrage, disque de rotor en etant equipe, rotor et moteur d'aeronef les comportant |
EP2253800A3 (fr) * | 2009-05-19 | 2017-05-17 | Rolls-Royce plc | Rotor équilibré pour moteur de turbine |
US9145772B2 (en) | 2012-01-31 | 2015-09-29 | United Technologies Corporation | Compressor disk bleed air scallops |
US9404367B2 (en) | 2012-11-21 | 2016-08-02 | Solar Turbines Incorporated | Gas turbine engine compressor rotor assembly and balancing system |
FR3021689A1 (fr) * | 2014-05-28 | 2015-12-04 | Snecma | Disque de turbomachine et procede pour son equilibrage |
EP3611338A3 (fr) * | 2018-08-14 | 2020-03-18 | United Technologies Corporation | Système de poids d'équilibrage de rotor en queue d'aronde |
US10883370B2 (en) | 2018-08-14 | 2021-01-05 | Raytheon Technologies Corporation | Dovetail weight system for rotor balance |
FR3096105A1 (fr) * | 2019-05-16 | 2020-11-20 | Safran Aircraft Engines | rotor de turbomachine à gaz à masselotte |
CN112160794A (zh) * | 2020-09-18 | 2021-01-01 | 中国航发四川燃气涡轮研究院 | 定位组件及其涡轮盘或压气机盘、航空发动机 |
CN112160794B (zh) * | 2020-09-18 | 2023-02-17 | 中国航发四川燃气涡轮研究院 | 定位组件及其涡轮盘或压气机盘、航空发动机 |
CN113915163A (zh) * | 2021-10-12 | 2022-01-11 | 浙江意动科技股份有限公司 | 一种压气机转子叶片连接结构 |
Also Published As
Publication number | Publication date |
---|---|
FR2358545B1 (fr) | 1978-12-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |