FR2959535B1 - Carter de turbomachine - Google Patents

Carter de turbomachine

Info

Publication number
FR2959535B1
FR2959535B1 FR1053339A FR1053339A FR2959535B1 FR 2959535 B1 FR2959535 B1 FR 2959535B1 FR 1053339 A FR1053339 A FR 1053339A FR 1053339 A FR1053339 A FR 1053339A FR 2959535 B1 FR2959535 B1 FR 2959535B1
Authority
FR
France
Prior art keywords
turbomachine housing
rotating
waves
standing waves
frequency
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
FR1053339A
Other languages
English (en)
Other versions
FR2959535A1 (fr
Inventor
Bruno Froissart
Francois Maurice Garcin
Delphine Hermance Maxime Parent
Vincent Roy
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 FR1053339A priority Critical patent/FR2959535B1/fr
Priority to US13/096,294 priority patent/US8684671B2/en
Publication of FR2959535A1 publication Critical patent/FR2959535A1/fr
Application granted granted Critical
Publication of FR2959535B1 publication Critical patent/FR2959535B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04—Antivibration arrangements
    • F01D25/06—Antivibration arrangements for preventing blade vibration
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F05D2240/11—Shroud seal segments
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Carter (52) de turbomachine, formant une enveloppe annulaire continue s'étendant sur 360° autour d'une roue à aubes et servant de support à la propagation d'ondes tournantes, chaque onde tournante étant générée par deux ondes stationnaires de même fréquence et le carter comprenant au moins un raidisseur longitudinal (50) sur sa périphérie externe dimensionné et positionné de manière à séparer en fréquence les deux ondes stationnaires (54, 56) d'au moins une onde tournante donnée.
FR1053339A 2010-04-29 2010-04-29 Carter de turbomachine Active FR2959535B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1053339A FR2959535B1 (fr) 2010-04-29 2010-04-29 Carter de turbomachine
US13/096,294 US8684671B2 (en) 2010-04-29 2011-04-28 Turbomachine casing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1053339A FR2959535B1 (fr) 2010-04-29 2010-04-29 Carter de turbomachine

Publications (2)

Publication Number Publication Date
FR2959535A1 FR2959535A1 (fr) 2011-11-04
FR2959535B1 true FR2959535B1 (fr) 2014-04-18

Family

ID=43127608

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1053339A Active FR2959535B1 (fr) 2010-04-29 2010-04-29 Carter de turbomachine

Country Status (2)

Country Link
US (1) US8684671B2 (fr)
FR (1) FR2959535B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9498850B2 (en) 2012-03-27 2016-11-22 Pratt & Whitney Canada Corp. Structural case for aircraft gas turbine engine
FR2991405B1 (fr) * 2012-05-29 2017-02-10 Snecma Ensemble d'un compresseur comportant un organe de rupture
CA2986589C (fr) 2015-05-22 2022-11-22 Nike Innovate C.V. Collants d'entrainement comportant des zones de compression concues au prealable et des motifs de structure integres
FR3052804B1 (fr) * 2016-06-16 2018-05-25 Safran Aircraft Engines Roue aubagee volontairement desaccordee
US10808574B2 (en) 2016-09-13 2020-10-20 General Electric Company Turbomachine stator travelling wave inhibitor
US10422348B2 (en) * 2017-01-10 2019-09-24 General Electric Company Unsymmetrical turbofan abradable grind for reduced rub loads

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1502903A (en) * 1923-02-27 1924-07-29 Gen Electric Steam-turbine rotor and method of avoiding wave phenomena therein
US3319929A (en) * 1964-12-31 1967-05-16 Gen Electric Vibration damping means
US3589475A (en) * 1969-01-02 1971-06-29 Gen Electric Vibration damping means
US4728255A (en) * 1985-02-25 1988-03-01 General Electric Company Removable stiffening disk
US6195982B1 (en) * 1998-12-30 2001-03-06 United Technologies Corporation Apparatus and method of active flutter control
JP2007500298A (ja) * 2003-07-29 2007-01-11 プラット　アンド　ホイットニー　カナダ　コーポレイション ターボファンケースと製造方法
FR2930590B1 (fr) * 2008-04-23 2013-05-31 Snecma Carter de turbomachine comportant un dispositif empechant une instabilite lors d'un contact entre le carter et le rotor
US8251637B2 (en) * 2008-05-16 2012-08-28 General Electric Company Systems and methods for modifying modal vibration associated with a turbine

Also Published As

Publication number Publication date
FR2959535A1 (fr) 2011-11-04
US8684671B2 (en) 2014-04-01
US20110274540A1 (en) 2011-11-10

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