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FR3003301B1 - Anneau de turbine pour turbomachine - Google Patents

Anneau de turbine pour turbomachine Download PDF

Info

Publication number
FR3003301B1
FR3003301B1 FR1352257A FR1352257A FR3003301B1 FR 3003301 B1 FR3003301 B1 FR 3003301B1 FR 1352257 A FR1352257 A FR 1352257A FR 1352257 A FR1352257 A FR 1352257A FR 3003301 B1 FR3003301 B1 FR 3003301B1
Authority
FR
France
Prior art keywords
turbomachine
turbine ring
turbine
ring
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.)
Expired - Fee Related
Application number
FR1352257A
Other languages
English (en)
Other versions
FR3003301A1 (fr
Inventor
Carole Jaureguiberry
Manuel Silva
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 Helicopter Engines SAS
Original Assignee
Safran Helicopter Engines SAS
Turbomeca SA
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
Priority to FR1352257A priority Critical patent/FR3003301B1/fr
Application filed by Safran Helicopter Engines SAS, Turbomeca SA filed Critical Safran Helicopter Engines SAS
Priority to JP2015562286A priority patent/JP6453252B2/ja
Priority to PCT/FR2014/050579 priority patent/WO2014140493A1/fr
Priority to US14/774,417 priority patent/US10138734B2/en
Priority to KR1020157028005A priority patent/KR102199586B1/ko
Priority to EP14720173.5A priority patent/EP2971609B1/fr
Priority to CA2904951A priority patent/CA2904951C/fr
Priority to RU2015143679A priority patent/RU2653710C2/ru
Priority to PL14720173T priority patent/PL2971609T3/pl
Priority to CN201480014008.1A priority patent/CN105189937B/zh
Publication of FR3003301A1 publication Critical patent/FR3003301A1/fr
Application granted granted Critical
Publication of FR3003301B1 publication Critical patent/FR3003301B1/fr
Expired - Fee Related 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • 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
    • 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
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • 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
    • F05D2240/00—Components
    • F05D2240/40—Use of a multiplicity of similar components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1352257A 2013-03-14 2013-03-14 Anneau de turbine pour turbomachine Expired - Fee Related FR3003301B1 (fr)

Priority Applications (10)

Application Number Priority Date Filing Date Title
FR1352257A FR3003301B1 (fr) 2013-03-14 2013-03-14 Anneau de turbine pour turbomachine
PL14720173T PL2971609T3 (pl) 2013-03-14 2014-03-13 Pierścień turbiny do maszyny wirowej
US14/774,417 US10138734B2 (en) 2013-03-14 2014-03-13 Turbine ring for a turbomachine
KR1020157028005A KR102199586B1 (ko) 2013-03-14 2014-03-13 터보기계를 위한 터빈 링
EP14720173.5A EP2971609B1 (fr) 2013-03-14 2014-03-13 Anneau de turbine pour turbomachine
CA2904951A CA2904951C (fr) 2013-03-14 2014-03-13 Anneau de turbine pour turbomachine
JP2015562286A JP6453252B2 (ja) 2013-03-14 2014-03-13 ターボ機械のタービンリング
PCT/FR2014/050579 WO2014140493A1 (fr) 2013-03-14 2014-03-13 Anneau de turbine pour turbomachine
CN201480014008.1A CN105189937B (zh) 2013-03-14 2014-03-13 涡轮发动机的涡轮环以及涡轮发动机
RU2015143679A RU2653710C2 (ru) 2013-03-14 2014-03-13 Кольцо турбины для турбомашины

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1352257A FR3003301B1 (fr) 2013-03-14 2013-03-14 Anneau de turbine pour turbomachine
FR1352257 2013-03-14

Publications (2)

Publication Number Publication Date
FR3003301A1 FR3003301A1 (fr) 2014-09-19
FR3003301B1 true FR3003301B1 (fr) 2018-01-05

Family

ID=48289407

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1352257A Expired - Fee Related FR3003301B1 (fr) 2013-03-14 2013-03-14 Anneau de turbine pour turbomachine

Country Status (10)

Country Link
US (1) US10138734B2 (fr)
EP (1) EP2971609B1 (fr)
JP (1) JP6453252B2 (fr)
KR (1) KR102199586B1 (fr)
CN (1) CN105189937B (fr)
CA (1) CA2904951C (fr)
FR (1) FR3003301B1 (fr)
PL (1) PL2971609T3 (fr)
RU (1) RU2653710C2 (fr)
WO (1) WO2014140493A1 (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10400896B2 (en) * 2014-08-28 2019-09-03 United Technologies Corporation Dual-ended brush seal assembly and method of manufacture
FR3036436B1 (fr) 2015-05-22 2020-01-24 Safran Ceramics Ensemble d'anneau de turbine avec maintien par brides
CN105386797B (zh) * 2015-12-29 2017-06-16 中国航空工业集团公司沈阳发动机设计研究所 一种涡轮静子结构
US11466700B2 (en) 2017-02-28 2022-10-11 Unison Industries, Llc Fan casing and mount bracket for oil cooler
FR3064023B1 (fr) * 2017-03-16 2019-09-13 Safran Aircraft Engines Ensemble d'anneau de turbine
FR3064022B1 (fr) * 2017-03-16 2019-09-13 Safran Aircraft Engines Ensemble d'anneau de turbine
US10533446B2 (en) 2017-05-15 2020-01-14 United Technologies Corporation Alternative W-seal groove arrangement
US10753222B2 (en) * 2017-09-11 2020-08-25 Raytheon Technologies Corporation Gas turbine engine blade outer air seal
FR3076852B1 (fr) * 2018-01-16 2020-01-31 Safran Aircraft Engines Anneau de turbomachine
US10920600B2 (en) * 2018-09-05 2021-02-16 Raytheon Technologies Corporation Integrated seal and wear liner
FR3086327B1 (fr) 2018-09-25 2020-12-04 Safran Aircraft Engines Ensemble pour une turbine de turbomachine
RU199280U1 (ru) * 2019-03-07 2020-08-25 Публичное акционерное общество "МОТОР СИЧ" Корпус подвески турбовинтового двигателя
FR3093536B1 (fr) * 2019-03-08 2021-02-19 Safran Aircraft Engines Rotor pour une turbine contrarotative de turbomachine
FR3096731B1 (fr) * 2019-05-29 2021-05-07 Safran Aircraft Engines Ensemble pour turbomachine
FR3096725B1 (fr) * 2019-05-29 2021-05-14 Safran Helicopter Engines Module de turbomachine d’aeronef
FR3100838B1 (fr) * 2019-09-13 2021-10-01 Safran Aircraft Engines Anneau d’etancheite de turbomachine
US11466588B2 (en) * 2019-10-30 2022-10-11 Raytheon Technologies Corporation Axially rigid curved beam with squeeze damper
CN113803115B (zh) * 2020-06-16 2024-04-05 中国航发商用航空发动机有限责任公司 涡轮叶片缘板阻尼器、涡轮叶片和航空发动机
JP7369301B2 (ja) * 2020-08-13 2023-10-25 三菱重工業株式会社 静翼セグメント、及びこれを備える蒸気タービン
FR3140115B1 (fr) * 2022-09-22 2024-10-04 Safran Aircraft Engines Pièce d'amortissement des déformations d'un carter de récupération d'huile, ensemble qui le comporte et turbomachine ainsi équipée
CN117869016B (zh) * 2024-03-12 2024-05-17 中国航发四川燃气涡轮研究院 一种降低涡轮外环导热的冷却单元及其分析方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5423659A (en) * 1994-04-28 1995-06-13 United Technologies Corporation Shroud segment having a cut-back retaining hook
JP2957943B2 (ja) * 1996-02-26 1999-10-06 川崎重工業株式会社 セラミック製シュラウドを備えたタービン
US5738490A (en) 1996-05-20 1998-04-14 Pratt & Whitney Canada, Inc. Gas turbine engine shroud seals
US6237921B1 (en) 1998-09-02 2001-05-29 General Electric Company Nested bridge seal
JP2004036443A (ja) * 2002-07-02 2004-02-05 Ishikawajima Harima Heavy Ind Co Ltd ガスタービンシュラウド構造
US6942445B2 (en) * 2003-12-04 2005-09-13 Honeywell International Inc. Gas turbine cooled shroud assembly with hot gas ingestion suppression
GB2417528B (en) 2004-08-23 2008-08-06 Alstom Technology Ltd Improved rope seal for gas turbine engines
US7207771B2 (en) * 2004-10-15 2007-04-24 Pratt & Whitney Canada Corp. Turbine shroud segment seal
US7217089B2 (en) * 2005-01-14 2007-05-15 Pratt & Whitney Canada Corp. Gas turbine engine shroud sealing arrangement
JP5501611B2 (ja) * 2008-12-25 2014-05-28 三菱重工業株式会社 タービン翼およびガスタービン
GB2477825B (en) 2010-09-23 2015-04-01 Rolls Royce Plc Anti fret liner assembly
US8944687B2 (en) * 2011-08-12 2015-02-03 Ihi Corporation Radial foil bearing

Also Published As

Publication number Publication date
KR20150128882A (ko) 2015-11-18
JP2016511362A (ja) 2016-04-14
US20160024926A1 (en) 2016-01-28
KR102199586B1 (ko) 2021-01-07
JP6453252B2 (ja) 2019-01-16
FR3003301A1 (fr) 2014-09-19
RU2653710C2 (ru) 2018-05-14
CN105189937B (zh) 2018-03-30
EP2971609A1 (fr) 2016-01-20
RU2015143679A (ru) 2017-04-26
PL2971609T3 (pl) 2019-12-31
CA2904951C (fr) 2021-01-26
WO2014140493A1 (fr) 2014-09-18
CA2904951A1 (fr) 2014-09-18
RU2015143679A3 (fr) 2018-03-01
EP2971609B1 (fr) 2019-08-07
CN105189937A (zh) 2015-12-23
US10138734B2 (en) 2018-11-27

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Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

CD Change of name or company name

Owner name: SAFRAN HELICOPTER ENGINES, FR

Effective date: 20170727

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

ST Notification of lapse

Effective date: 20221105