FR2358545A1 - Perfectionnements aux dispositifs d'equilibrage de rotors - Google Patents

Perfectionnements aux dispositifs d'equilibrage de rotors

Info

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
Application number
FR7622779A
Other languages
English (en)
French (fr)
Other versions
FR2358545B1 (enExample
Inventor
Claude Christian Hallinger
Jean Marc Surdi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to FR7622779A priority Critical patent/FR2358545A1/fr
Publication of FR2358545A1 publication Critical patent/FR2358545A1/fr
Application granted granted Critical
Publication of FR2358545B1 publication Critical patent/FR2358545B1/fr
Granted legal-status Critical Current

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)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7622779A 1976-07-16 1976-07-16 Perfectionnements aux dispositifs d'equilibrage de rotors Granted FR2358545A1 (fr)

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 (enExample) 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 (enExample)

Cited By (19)

* Cited by examiner, † Cited by third party
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
EP1239059A3 (en) * 2001-03-07 2003-08-27 General Electric Company Chemical milling of the blades of a gas turbine engine
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 (en) * 2009-05-19 2017-05-17 Rolls-Royce plc A balanced rotor for a turbine engine
EP3611338A3 (en) * 2018-08-14 2020-03-18 United 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
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

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Cited By (23)

* Cited by examiner, † Cited by third party
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
EP1239059A3 (en) * 2001-03-07 2003-08-27 General Electric Company Chemical milling of the blades of a gas turbine engine
US7252481B2 (en) * 2004-05-14 2007-08-07 Pratt & Whitney Canada Corp. Natural frequency tuning of gas turbine engine blades
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
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
EP2253800A3 (en) * 2009-05-19 2017-05-17 Rolls-Royce plc A balanced rotor for a turbine engine
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 (en) * 2018-08-14 2020-03-18 United Technologies Corporation Dovetail weight system for rotor balance
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 (enExample) 1978-12-15

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Legal Events

Date Code Title Description
ST Notification of lapse