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 PDFInfo
- 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
Links
- 238000001816 cooling Methods 0.000 title abstract 2
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical group FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
Classifications
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- 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.
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 |
FR1758747A Active FR3056633B1 (fr) | 2016-09-27 | 2017-09-21 | 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 |
Family Applications Before (2)
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 |
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) | GB2556193B (fr) |
Families Citing this family (28)
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 |
JP2024010701A (ja) * | 2022-07-13 | 2024-01-25 | 本田技研工業株式会社 | ラジアルタービンノズル及びその組立方法 |
FR3139292B1 (fr) * | 2022-09-01 | 2024-08-30 | 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 |
US12031443B2 (en) | 2022-11-29 | 2024-07-09 | Rolls-Royce Corporation | Ceramic matrix composite blade track segment with attachment flange cooling chambers |
US11840936B1 (en) | 2022-11-30 | 2023-12-12 | Rolls-Royce Corporation | Ceramic matrix composite blade track segment with pin-locating shim kit |
US11713694B1 (en) | 2022-11-30 | 2023-08-01 | Rolls-Royce Corporation | Ceramic matrix composite blade track segment with two-piece carrier |
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)
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 |
RU2522264C2 (ru) | 2009-03-09 | 2014-07-10 | Снекма | Сборка обоймы турбины |
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 |
BR112016028858A2 (pt) * | 2014-06-12 | 2017-08-22 | Gen Electric | ?conjuntos de suspensor e tubo base? |
JP6363232B2 (ja) * | 2014-06-12 | 2018-07-25 | ゼネラル・エレクトリック・カンパニイ | シュラウドハンガーアセンブリ |
EP3155230B1 (fr) * | 2014-06-12 | 2022-06-01 | General Electric Company | Ensemble de suspension de carénage à multiples pièces |
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 |
US10641120B2 (en) * | 2015-07-24 | 2020-05-05 | Rolls-Royce Corporation | Seal segment for a gas turbine engine |
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 |
-
2016
- 2016-09-27 FR FR1601411A patent/FR3056632B1/fr active Active
-
2017
- 2017-09-21 FR FR1758747A patent/FR3056633B1/fr active Active
- 2017-09-21 FR FR1758748A patent/FR3056634B1/fr active Active
- 2017-09-27 GB GB1715651.4A patent/GB2556193B/en active Active
- 2017-09-27 GB GB1719002.6A patent/GB2556216B/en active Active
- 2017-09-27 GB GB1719103.2A patent/GB2556217B/en active Active
- 2017-09-27 US US15/717,039 patent/US10428688B2/en active Active
- 2017-11-20 US US15/818,121 patent/US10415427B2/en active Active
- 2017-11-20 US US15/818,039 patent/US10415426B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20180087400A1 (en) | 2018-03-29 |
US10428688B2 (en) | 2019-10-01 |
FR3056632B1 (fr) | 2020-06-05 |
GB2556217B (en) | 2021-09-15 |
FR3056633A1 (fr) | 2018-03-30 |
GB2556193B (en) | 2021-03-17 |
GB2556216A (en) | 2018-05-23 |
GB2556193A (en) | 2018-05-23 |
FR3056634A1 (fr) | 2018-03-30 |
US20180087401A1 (en) | 2018-03-29 |
GB2556216B (en) | 2021-08-11 |
GB201719103D0 (en) | 2018-01-03 |
FR3056632A1 (fr) | 2018-03-30 |
US10415426B2 (en) | 2019-09-17 |
FR3056633B1 (fr) | 2021-04-23 |
GB2556217A (en) | 2018-05-23 |
GB201719002D0 (en) | 2018-01-03 |
US10415427B2 (en) | 2019-09-17 |
GB201715651D0 (en) | 2017-11-08 |
US20180087399A1 (en) | 2018-03-29 |
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