FR3129175B1 - Module de turbomachine avec un dispositif de limitation d’amplitude et turbomachine correpondante - Google Patents

Module de turbomachine avec un dispositif de limitation d’amplitude et turbomachine correpondante Download PDF

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Publication number
FR3129175B1
FR3129175B1 FR2112051A FR2112051A FR3129175B1 FR 3129175 B1 FR3129175 B1 FR 3129175B1 FR 2112051 A FR2112051 A FR 2112051A FR 2112051 A FR2112051 A FR 2112051A FR 3129175 B1 FR3129175 B1 FR 3129175B1
Authority
FR
France
Prior art keywords
stator
rotor
turbomachine
longitudinal axis
limiting device
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
FR2112051A
Other languages
English (en)
Other versions
FR3129175A1 (fr
Inventor
Thomas Giraudeau
Robin Leynaud
Alban François Louis
Olivier Formica
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 FR2112051A priority Critical patent/FR3129175B1/fr
Publication of FR3129175A1 publication Critical patent/FR3129175A1/fr
Application granted granted Critical
Publication of FR3129175B1 publication Critical patent/FR3129175B1/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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/08—Restoring position
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • 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
    • F05D2240/00—Components
    • F05D2240/50—Bearings
    • F05D2240/54—Radial bearings
    • 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
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/31—Retaining bolts or nuts
    • F05D2260/311—Retaining bolts or nuts of the frangible or shear type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L’invention concerne une module de turbomachine ayant un axe longitudinal (X), comprenant : - un stator centré sur l’axe longitudinal,- un rotor (3) comprenant un disque (12) et une pluralité d’aubes (13) portées par le disque, le rotor étant entraîné en rotation autour de l’axe longitudinal par un arbre (5) supporté par le stator via un palier (20), et- un dispositif de limitation d’amplitude (35) radiale du rotor par rapport au stator. Selon l’invention, le dispositif de limitation comprend une virole annulaire (36) rapportée et reliée de manière amovible au stator, la virole annulaire s’étendant radialement autour d’une partie du disque et comprenant une première portion (41) statorique située en amont du palier, ladite première portion (41) étant à distance et en regard d’une deuxième portion (42 ; 12a) rotorique solidaire en rotation du disque, laquelle est configurée pour venir en butée radialement contre la première portion en cas de déplacement radial du rotor. Figure d’abrégé : Figure 2
FR2112051A 2021-11-15 2021-11-15 Module de turbomachine avec un dispositif de limitation d’amplitude et turbomachine correpondante Active FR3129175B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2112051A FR3129175B1 (fr) 2021-11-15 2021-11-15 Module de turbomachine avec un dispositif de limitation d’amplitude et turbomachine correpondante

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2112051A FR3129175B1 (fr) 2021-11-15 2021-11-15 Module de turbomachine avec un dispositif de limitation d’amplitude et turbomachine correpondante
FR2112051 2021-11-15

Publications (2)

Publication Number Publication Date
FR3129175A1 FR3129175A1 (fr) 2023-05-19
FR3129175B1 true FR3129175B1 (fr) 2023-10-27

Family

ID=79602215

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2112051A Active FR3129175B1 (fr) 2021-11-15 2021-11-15 Module de turbomachine avec un dispositif de limitation d’amplitude et turbomachine correpondante

Country Status (1)

Country Link
FR (1) FR3129175B1 (fr)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL6900762A (fr) 1968-01-26 1969-07-29
GB2109481B (en) * 1981-11-12 1985-03-13 Rolls Royce Gas turbine engine and shaft
US6312215B1 (en) * 2000-02-15 2001-11-06 United Technologies Corporation Turbine engine windmilling brake
FR2965298B1 (fr) * 2010-09-28 2012-09-28 Snecma Moteur a turbine a gaz comprenant des moyens de retention axiale d'une soufflante dudit moteur
CN103775212B (zh) * 2012-10-25 2016-11-23 中航商用航空发动机有限责任公司 一种航空发动机的风扇失效制动装置
GB2550397B (en) * 2016-05-19 2018-11-21 Derwent Aviation Consulting Ltd A turbo machine comprising a compressor system
FR3071546B1 (fr) * 2017-09-25 2019-09-13 Safran Aircraft Engines Retention axiale de l'arbre de soufflante dans un moteur a turbine a gaz

Also Published As

Publication number Publication date
FR3129175A1 (fr) 2023-05-19

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