FR3056634B1 - Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement - Google Patents

Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement Download PDF

Info

Publication number
FR3056634B1
FR3056634B1 FR1758748A FR1758748A FR3056634B1 FR 3056634 B1 FR3056634 B1 FR 3056634B1 FR 1758748 A FR1758748 A FR 1758748A FR 1758748 A FR1758748 A FR 1758748A FR 3056634 B1 FR3056634 B1 FR 3056634B1
Authority
FR
France
Prior art keywords
cooling air
air distribution
ring
ring assembly
assembly including
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
FR1758748A
Other languages
English (en)
Other versions
FR3056634A1 (fr
Inventor
Lucien Henri Jacques Quennehen
Sebastien Serge Francis Congratel
Clement Jean Pierre Duffau
Nicolas Paul Tableau
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 FR1758748A priority Critical patent/FR3056634B1/fr
Publication of FR3056634A1 publication Critical patent/FR3056634A1/fr
Application granted granted Critical
Publication of FR3056634B1 publication Critical patent/FR3056634B1/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
    • 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
    • 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
    • F01D25/005—Selecting particular materials
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • 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
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/644—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins for adjusting the position or the alignment, e.g. wedges or eccenters
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/75—Shape given by its similarity to a letter, e.g. T-shaped
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • 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
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/502—Thermal properties
    • F05D2300/5021—Expansivity
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/502—Thermal properties
    • F05D2300/5021—Expansivity
    • F05D2300/50212—Expansivity dissimilar
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6033—Ceramic matrix composites [CMC]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

La présente invention concerne un ensemble d'anneau de turbine comprenant une pluralité de secteurs d'anneau (110) et une structure de support d'anneau (13), l'ensemble d'anneau comprenant en outre, pour chaque secteur d'anneau, un élément de répartition (150) de l'air de refroidissement fixé à la structure de support d'anneau (13) et positionné dans une première cavité (151) délimitée entre l'anneau de turbine et la structure de support d'anneau.
FR1758748A 2016-09-27 2017-09-21 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement Active FR3056634B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1758748A FR3056634B1 (fr) 2016-09-27 2017-09-21 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1601411A FR3056632B1 (fr) 2016-09-27 2016-09-27 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement
FR1601411 2016-09-27
FR1758748A FR3056634B1 (fr) 2016-09-27 2017-09-21 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement

Publications (2)

Publication Number Publication Date
FR3056634A1 FR3056634A1 (fr) 2018-03-30
FR3056634B1 true FR3056634B1 (fr) 2021-04-23

Family

ID=58162644

Family Applications (3)

Application Number Title Priority Date Filing Date
FR1601411A Active FR3056632B1 (fr) 2016-09-27 2016-09-27 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement
FR1758748A Active FR3056634B1 (fr) 2016-09-27 2017-09-21 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement
FR1758747A Active FR3056633B1 (fr) 2016-09-27 2017-09-21 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement

Family Applications Before (1)

Application Number Title Priority Date Filing Date
FR1601411A Active FR3056632B1 (fr) 2016-09-27 2016-09-27 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement

Family Applications After (1)

Application Number Title Priority Date Filing Date
FR1758747A Active FR3056633B1 (fr) 2016-09-27 2017-09-21 Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement

Country Status (3)

Country Link
US (3) US10428688B2 (fr)
FR (3) FR3056632B1 (fr)
GB (3) GB2556216B (fr)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3033825B1 (fr) * 2015-03-16 2018-09-07 Safran Aircraft Engines Ensemble d'anneau de turbine en materiau composite a matrice ceramique
FR3055146B1 (fr) * 2016-08-19 2020-05-29 Safran Aircraft Engines Ensemble d'anneau de turbine
FR3055147B1 (fr) * 2016-08-19 2020-05-29 Safran Aircraft Engines Ensemble d'anneau de turbine
FR3055148B1 (fr) * 2016-08-19 2020-06-05 Safran Aircraft Engines Ensemble d'anneau de turbine
FR3056637B1 (fr) * 2016-09-27 2018-10-19 Safran Aircraft Engines Ensemble d'anneau de turbine avec calage a froid
US10577976B2 (en) * 2017-10-30 2020-03-03 United Technologies Corporation Mounting assembly with rotatable and/or translatable retainer pins
US10704408B2 (en) * 2018-05-03 2020-07-07 Rolls-Royce North American Technologies Inc. Dual response blade track system
FR3081927B1 (fr) * 2018-05-30 2020-11-20 Safran Aircraft Engines Dispositif de refroidissement d'un carter de turbomachine
US10858949B2 (en) 2018-09-12 2020-12-08 Rolls-Royce Corporation Multi-piece carrier assembly for mounting ceramic matrix composite seal segments
FR3086327B1 (fr) 2018-09-25 2020-12-04 Safran Aircraft Engines Ensemble pour une turbine de turbomachine
FR3090732B1 (fr) * 2018-12-19 2021-01-08 Safran Aircraft Engines Ensemble d’anneau de turbine avec flasques indexés.
CN109751088A (zh) * 2019-03-25 2019-05-14 中国船舶重工集团公司第七0三研究所 一种用于船用燃气轮机的分块式涡轮外环连接结构
FR3095668B1 (fr) * 2019-05-03 2021-04-09 Safran Aircraft Engines Ensemble d’anneau de turbine monté sur entretoise
FR3108367B1 (fr) * 2020-03-20 2023-07-21 Safran Aircraft Engines Ensemble de turbine et turbomachine munie d’un tel ensemble
FR3108672B1 (fr) * 2020-03-24 2023-06-02 Safran Aircraft Engines Ensemble d'anneau de turbine
US11208911B2 (en) * 2020-04-23 2021-12-28 Rolls-Royce Plc Turbine shroud ring segments with ceramic matrix composite components
US11220928B1 (en) 2020-08-24 2022-01-11 Rolls-Royce Corporation Turbine shroud assembly with ceramic matrix composite components and cooling features
US11208896B1 (en) 2020-10-20 2021-12-28 Rolls-Royce Corporation Turbine shroud having ceramic matrix composite component mounted with cooled pin
FR3121469B1 (fr) 2021-03-30 2023-06-23 Safran Aircraft Engines Ensemble d’anneau de turbine pour une turbomachine
US11761351B2 (en) * 2021-05-25 2023-09-19 Rolls-Royce Corporation Turbine shroud assembly with radially located ceramic matrix composite shroud segments
FR3139292A1 (fr) * 2022-09-01 2024-03-08 Safran Aircraft Engines Ensemble d’anneau de turbine à rattrapage de jeux intégré
US11773751B1 (en) 2022-11-29 2023-10-03 Rolls-Royce Corporation Ceramic matrix composite blade track segment with pin-locating threaded insert
US11713694B1 (en) 2022-11-30 2023-08-01 Rolls-Royce Corporation Ceramic matrix composite blade track segment with two-piece carrier
US11840936B1 (en) 2022-11-30 2023-12-12 Rolls-Royce Corporation Ceramic matrix composite blade track segment with pin-locating shim kit
US11732604B1 (en) 2022-12-01 2023-08-22 Rolls-Royce Corporation Ceramic matrix composite blade track segment with integrated cooling passages
US11885225B1 (en) 2023-01-25 2024-01-30 Rolls-Royce Corporation Turbine blade track with ceramic matrix composite segments having attachment flange draft angles

Family Cites Families (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4303371A (en) 1978-06-05 1981-12-01 General Electric Company Shroud support with impingement baffle
US6702550B2 (en) * 2002-01-16 2004-03-09 General Electric Company Turbine shroud segment and shroud assembly
US6877952B2 (en) * 2002-09-09 2005-04-12 Florida Turbine Technologies, Inc Passive clearance control
US6997673B2 (en) * 2003-12-11 2006-02-14 Honeywell International, Inc. Gas turbine high temperature turbine blade outer air seal assembly
US7494317B2 (en) * 2005-06-23 2009-02-24 Siemens Energy, Inc. Ring seal attachment system
FR2887601B1 (fr) 2005-06-24 2007-10-05 Snecma Moteurs Sa Piece mecanique et procede de fabrication d'une telle piece
US7278820B2 (en) * 2005-10-04 2007-10-09 Siemens Power Generation, Inc. Ring seal system with reduced cooling requirements
US20070107216A1 (en) * 2005-10-31 2007-05-17 General Electric Company Mim method for coating turbine shroud
US7726936B2 (en) * 2006-07-25 2010-06-01 Siemens Energy, Inc. Turbine engine ring seal
US7722317B2 (en) * 2007-01-25 2010-05-25 Siemens Energy, Inc. CMC to metal attachment mechanism
GB0703827D0 (en) * 2007-02-28 2007-04-11 Rolls Royce Plc Rotor seal segment
BRPI1013342A8 (pt) 2009-03-09 2016-09-20 Sme Conjunto de anel de turbina
US9175579B2 (en) * 2011-12-15 2015-11-03 General Electric Company Low-ductility turbine shroud
US9726043B2 (en) * 2011-12-15 2017-08-08 General Electric Company Mounting apparatus for low-ductility turbine shroud
CA2806401A1 (fr) * 2012-02-22 2013-08-22 General Electric Company Enveloppe de turbine a faible ductilite
EP2728255A1 (fr) * 2012-10-31 2014-05-07 Alstom Technology Ltd Agencement de segment de gaz chaud
WO2015023576A1 (fr) * 2013-08-15 2015-02-19 United Technologies Corporation Panneau de protection et cadre à cet effet
CN106460543B (zh) * 2014-06-12 2018-12-21 通用电气公司 多件式护罩悬挂器组件
CN106460560B (zh) * 2014-06-12 2018-11-13 通用电气公司 护罩吊架组件
BR112016028858A2 (pt) * 2014-06-12 2017-08-22 Gen Electric ?conjuntos de suspensor e tubo base?
US9587517B2 (en) * 2014-12-29 2017-03-07 Rolls-Royce North American Technologies, Inc. Blade track assembly with turbine tip clearance control
US9874104B2 (en) 2015-02-27 2018-01-23 General Electric Company Method and system for a ceramic matrix composite shroud hanger assembly
FR3033825B1 (fr) * 2015-03-16 2018-09-07 Safran Aircraft Engines Ensemble d'anneau de turbine en materiau composite a matrice ceramique
FR3034132B1 (fr) * 2015-03-23 2018-06-15 Safran Ceramics Ensemble d'anneau de turbine comprenant une pluralite de secteurs d'anneau en materiau composite a matrice ceramique
FR3036432B1 (fr) * 2015-05-22 2019-04-19 Safran Ceramics Ensemble d'anneau de turbine avec maintien axial
FR3036435B1 (fr) * 2015-05-22 2020-01-24 Safran Ceramics Ensemble d'anneau de turbine
US10385718B2 (en) * 2015-06-29 2019-08-20 Rolls-Royce North American Technologies, Inc. Turbine shroud segment with side perimeter seal
CA2936977A1 (fr) * 2015-07-24 2017-01-24 Rolls-Royce Corporation Un segment de joint destine a une turbine a gaz
US9926799B2 (en) * 2015-10-12 2018-03-27 United Technologies Corporation Gas turbine engine components, blade outer air seal assemblies, and blade outer air seal segments thereof
FR3045715B1 (fr) * 2015-12-18 2018-01-26 Safran Aircraft Engines Ensemble d'anneau de turbine avec maintien a froid et a chaud
FR3048016B1 (fr) * 2016-02-18 2018-03-16 Safran Ceramics Secteur d'anneau de turbine avec barriere environnementale dopee par un element electriquement conducteur
FR3068071B1 (fr) * 2017-06-26 2019-11-08 Safran Aircraft Engines Ensemble pour la liaison par palonnier entre un carter de turbine et un element annulaire de turbomachine

Also Published As

Publication number Publication date
GB2556217B (en) 2021-09-15
FR3056634A1 (fr) 2018-03-30
US10415426B2 (en) 2019-09-17
GB201719103D0 (en) 2018-01-03
US10415427B2 (en) 2019-09-17
GB2556217A (en) 2018-05-23
US20180087400A1 (en) 2018-03-29
FR3056633A1 (fr) 2018-03-30
FR3056632A1 (fr) 2018-03-30
GB201715651D0 (en) 2017-11-08
US10428688B2 (en) 2019-10-01
GB2556193A (en) 2018-05-23
GB2556193B (en) 2021-03-17
GB2556216B (en) 2021-08-11
FR3056633B1 (fr) 2021-04-23
US20180087401A1 (en) 2018-03-29
GB2556216A (en) 2018-05-23
FR3056632B1 (fr) 2020-06-05
US20180087399A1 (en) 2018-03-29
GB201719002D0 (en) 2018-01-03

Similar Documents

Publication Publication Date Title
FR3056633B1 (fr) Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement
FR3036432B1 (fr) Ensemble d'anneau de turbine avec maintien axial
USD855740S1 (en) Lens with reticle
FR3036436B1 (fr) Ensemble d'anneau de turbine avec maintien par brides
FR3055147B1 (fr) Ensemble d'anneau de turbine
USD856460S1 (en) Lens with reticle
FR3033826B1 (fr) Ensemble d'anneau de turbine comprenant une pluralite de secteurs d'anneau en materiau composite a matrice ceramique
USD870923S1 (en) Vessel for a candle
EP4273370A3 (fr) Ensemble d'anneau de turbine permettant une dilatation thermique différentielle
USD792603S1 (en) Rig for electrophoresis gel casting
USD902467S1 (en) Light fixture
CL2017003251A1 (es) Carrete
FR3020399B1 (fr) Ensemble modulaire pour une turbomachine
BR112016002648A2 (pt) pá de estator de turbomáquina
FR3058460B1 (fr) Ensemble de raccordement pour le refroidissement d'une turbine de turbomachine
MA55080A (fr) Anticorps anti-mertk à affinité élevée et utilisations associées
FR3029355B1 (fr) Generateur thermoelectrique
USD752558S1 (en) Jacket for speaker
ES2575028T3 (es) Unión atornillada de la tapa de una abertura de acceso en una superficie sustentadora de una aeronave
USD816865S1 (en) Cassette support base for electrophoresis gel casting
JP2019207083A5 (fr)
JP2021062522A5 (fr)
BR102015030534B8 (pt) Guindaste
TWD196684S (zh) 口腔保健用具的跟蹤模組（一）
USD923727S1 (en) Lacrosse ball

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20180518

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8