FR3099801B1 - Ensemble pour une turbine de turbomachine - Google Patents

Ensemble pour une turbine de turbomachine Download PDF

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Publication number
FR3099801B1
FR3099801B1 FR1909097A FR1909097A FR3099801B1 FR 3099801 B1 FR3099801 B1 FR 3099801B1 FR 1909097 A FR1909097 A FR 1909097A FR 1909097 A FR1909097 A FR 1909097A FR 3099801 B1 FR3099801 B1 FR 3099801B1
Authority
FR
France
Prior art keywords
housing
turbomachine turbine
cooling
casing
tube
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
FR1909097A
Other languages
English (en)
Other versions
FR3099801A1 (fr
Inventor
Simon Nicolas Morliere
Stéphane Pierre Guillaume Blanchard
Nicolas Jean-Marc Marcel Beauquin
Alain Dominique Gendraud
Olivier Renon
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 FR1909097A priority Critical patent/FR3099801B1/fr
Publication of FR3099801A1 publication Critical patent/FR3099801A1/fr
Application granted granted Critical
Publication of FR3099801B1 publication Critical patent/FR3099801B1/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
    • 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
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/14—Casings modified 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • 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
    • 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

Abstract

L’invention concerne un ensemble (25) pour une turbine de turbomachine comportant un carter (18) comprenant une paroi annulaire (26) autour d’un axe, et des moyens de refroidissement du carter (18), lesdits moyens de refroidissement comportant un boîtier collecteur (22) et au moins un tube (23) s’étendant circonférentiellement autour de la paroi annulaire (26) du carter (18) et relié au boîtier (22), l’au moins un tube (23) comportant des orifices d’éjection d’air de refroidissement. Figure à publier avec l’abrégé : figure n°4
FR1909097A 2019-08-09 2019-08-09 Ensemble pour une turbine de turbomachine Active FR3099801B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1909097A FR3099801B1 (fr) 2019-08-09 2019-08-09 Ensemble pour une turbine de turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1909097A FR3099801B1 (fr) 2019-08-09 2019-08-09 Ensemble pour une turbine de turbomachine
FR1909097 2019-08-09

Publications (2)

Publication Number Publication Date
FR3099801A1 FR3099801A1 (fr) 2021-02-12
FR3099801B1 true FR3099801B1 (fr) 2021-12-03

Family

ID=68807068

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1909097A Active FR3099801B1 (fr) 2019-08-09 2019-08-09 Ensemble pour une turbine de turbomachine

Country Status (1)

Country Link
FR (1) FR3099801B1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3129972A1 (fr) * 2021-12-07 2023-06-09 Safran Aircraft Engines Boîtier de distribution d’air de refroidissement
FR3137119A1 (fr) * 2022-06-22 2023-12-29 Safran Aircraft Engines Système de refroidissement amélioré pour un ensemble mobile de turbomachine
FR3137405A1 (fr) * 2022-07-04 2024-01-05 Safran Aircraft Engines Carter de turbine de turboréacteur équipé de dispositifs mobiles de fixation de tubes de refroidissement

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5399066A (en) * 1993-09-30 1995-03-21 General Electric Company Integral clearance control impingement manifold and environmental shield
FR2816352B1 (fr) * 2000-11-09 2003-01-31 Snecma Moteurs Ensemble de ventilation d'un anneau de stator
FR3021700B1 (fr) 2014-05-27 2016-07-01 Snecma Dispositif de maintien d'un tube de refroidissement pour carter de turboreacteur
US9869196B2 (en) * 2014-06-24 2018-01-16 General Electric Company Gas turbine engine spring mounted manifold

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3129972A1 (fr) * 2021-12-07 2023-06-09 Safran Aircraft Engines Boîtier de distribution d’air de refroidissement
FR3137119A1 (fr) * 2022-06-22 2023-12-29 Safran Aircraft Engines Système de refroidissement amélioré pour un ensemble mobile de turbomachine
FR3137405A1 (fr) * 2022-07-04 2024-01-05 Safran Aircraft Engines Carter de turbine de turboréacteur équipé de dispositifs mobiles de fixation de tubes de refroidissement

Also Published As

Publication number Publication date
FR3099801A1 (fr) 2021-02-12

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