FR3096105B1 - rotor de turbomachine à gaz à masselotte - Google Patents

rotor de turbomachine à gaz à masselotte Download PDF

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Publication number
FR3096105B1
FR3096105B1 FR1905128A FR1905128A FR3096105B1 FR 3096105 B1 FR3096105 B1 FR 3096105B1 FR 1905128 A FR1905128 A FR 1905128A FR 1905128 A FR1905128 A FR 1905128A FR 3096105 B1 FR3096105 B1 FR 3096105B1
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine rotor
flyweight
disc
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.)
Active
Application number
FR1905128A
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English (en)
Other versions
FR3096105A1 (fr
Inventor
Thomas Nolwenn Emmanuel Delahaye
Blaise Bergon
Laurent Jablonski
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
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1905128A priority Critical patent/FR3096105B1/fr
Publication of FR3096105A1 publication Critical patent/FR3096105A1/fr
Application granted granted Critical
Publication of FR3096105B1 publication Critical patent/FR3096105B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Est concerné un rotor de turbomachine à gaz pour aéronef, comprenant un disque (48) et au moins une masselotte (85) d'équilibrage du disque. Le disque présente une partie saillante vers l’amont définissant une virole annulaire (79) festonnée présentant ainsi une alternance de dents (81) saillante vers l’amont et de creux (83) vers l’aval. La masselotte (85) d'équilibrage s’étend dans un dit creux et est fixée à la virole annulaire. Figure à publier avec l’abrégé : Figure 5
FR1905128A 2019-05-16 2019-05-16 rotor de turbomachine à gaz à masselotte Active FR3096105B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1905128A FR3096105B1 (fr) 2019-05-16 2019-05-16 rotor de turbomachine à gaz à masselotte

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1905128 2019-05-16
FR1905128A FR3096105B1 (fr) 2019-05-16 2019-05-16 rotor de turbomachine à gaz à masselotte

Publications (2)

Publication Number Publication Date
FR3096105A1 FR3096105A1 (fr) 2020-11-20
FR3096105B1 true FR3096105B1 (fr) 2021-11-05

Family

ID=67660325

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1905128A Active FR3096105B1 (fr) 2019-05-16 2019-05-16 rotor de turbomachine à gaz à masselotte

Country Status (1)

Country Link
FR (1) FR3096105B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118391298B (zh) * 2024-06-28 2024-09-06 中国航发四川燃气涡轮研究院 一种带配重的低压压气机出口双重封严结构

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2358545A1 (fr) * 1976-07-16 1978-02-10 Snecma Perfectionnements aux dispositifs d'equilibrage de rotors
FR2885196B1 (fr) * 2005-04-29 2007-06-29 Snecma Moteurs Sa Dispositif d'equilibrage d'un rotor de turbomachine
US8506253B2 (en) * 2009-08-19 2013-08-13 Pratt & Whitney Canada Corp. Balancing apparatus for rotor assembly
PL2808486T3 (pl) * 2013-05-27 2017-11-30 MTU Aero Engines AG Element wyważający do układu łopatek wirujących
EP3091179B1 (fr) * 2015-05-07 2021-06-30 MTU Aero Engines AG Système de rotor pour une turbomachine et compresseur
DE102017207283A1 (de) * 2017-04-28 2018-10-31 Rolls-Royce Deutschland Ltd & Co Kg Rotoranordnung mit Wuchtelement und Verfahren zur Montage eines Wuchtelements

Also Published As

Publication number Publication date
FR3096105A1 (fr) 2020-11-20

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