FR3071538B1 - Aube de rotor pour une turbomachine - Google Patents
Aube de rotor pour une turbomachine Download PDFInfo
- Publication number
- FR3071538B1 FR3071538B1 FR1758929A FR1758929A FR3071538B1 FR 3071538 B1 FR3071538 B1 FR 3071538B1 FR 1758929 A FR1758929 A FR 1758929A FR 1758929 A FR1758929 A FR 1758929A FR 3071538 B1 FR3071538 B1 FR 3071538B1
- Authority
- FR
- France
- Prior art keywords
- heel
- axis
- sealing lip
- turbomachine
- radially outer
- 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
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
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
-
- 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
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
-
- 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
- F01D11/22—Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- 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
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade
-
- 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
- F05D2240/55—Seals
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Un aspect de l'invention concerne une aube de rotor de turbomachine comportant une extrémité radialement externe munie d'un talon, le talon étant pourvu d'au moins une léchette d'étanchéité (3), la ou chaque léchette d'étanchéité (3) faisant saillie du talon suivant un premier axe (z), le premier axe (z) étant à +/- 15° selon une direction radiale, et s'étendant suivant un deuxième axe (x), sensiblement perpendiculaire au premier axe (z), entre une première extrémité extrados et une deuxième extrémité intrados, la ou chaque léchette d'étanchéité (3) présentant un premier côté amont et un deuxième côté aval ainsi qu'une surface radialement externe, l'aube étant caractérisée en ce que la ou chaque léchette d'étanchéité (3) comporte une base (7) fixée au talon et un embout (8) imbriqué de manière amovible avec la base (7).
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1758929A FR3071538B1 (fr) | 2017-09-27 | 2017-09-27 | Aube de rotor pour une turbomachine |
US16/651,052 US11333031B2 (en) | 2017-09-27 | 2018-09-17 | Rotor blade for a turbomachine |
PCT/FR2018/052273 WO2019063909A1 (fr) | 2017-09-27 | 2018-09-17 | Aube de rotor pour une turbomachine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1758929A FR3071538B1 (fr) | 2017-09-27 | 2017-09-27 | Aube de rotor pour une turbomachine |
FR1758929 | 2017-09-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3071538A1 FR3071538A1 (fr) | 2019-03-29 |
FR3071538B1 true FR3071538B1 (fr) | 2020-09-04 |
Family
ID=60202224
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1758929A Active FR3071538B1 (fr) | 2017-09-27 | 2017-09-27 | Aube de rotor pour une turbomachine |
Country Status (3)
Country | Link |
---|---|
US (1) | US11333031B2 (fr) |
FR (1) | FR3071538B1 (fr) |
WO (1) | WO2019063909A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102626244B1 (ko) * | 2019-07-30 | 2024-01-17 | 지멘스 에너지, 인코포레이티드 | 고온 가스 터빈 컴포넌트들을 보수하기 위한 시스템 및 방법 |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3053505A (en) * | 1958-06-11 | 1962-09-11 | Gen Motors Corp | Pinned blade shrouding |
FR2511908A1 (fr) | 1981-08-26 | 1983-03-04 | Snecma | Procede de brasage-diffusion destine aux pieces en superalliages |
US5234318A (en) * | 1993-01-22 | 1993-08-10 | Brandon Ronald E | Clip-on radial tip seals for steam and gas turbines |
US6926495B2 (en) * | 2003-09-12 | 2005-08-09 | Siemens Westinghouse Power Corporation | Turbine blade tip clearance control device |
US8753093B2 (en) * | 2010-10-19 | 2014-06-17 | General Electric Company | Bonded turbine bucket tip shroud and related method |
FR2977909B1 (fr) | 2011-07-12 | 2016-07-15 | Snecma | Aube de rotor pour une turbomachine |
US9163519B2 (en) * | 2011-07-28 | 2015-10-20 | General Electric Company | Cap for ceramic blade tip shroud |
FR2980234B1 (fr) | 2011-09-16 | 2016-08-19 | Snecma | Aube pour turbomachine avec lechettes d'etancheite |
US20140255194A1 (en) * | 2012-12-21 | 2014-09-11 | General Electric Company | Tip shrouds of turbine rotor blades and methods of manufacture related thereto |
WO2014137457A1 (fr) * | 2013-03-08 | 2014-09-12 | Uskert Richard C | Procédé de formation d'un ensemble aile portante composite de moteur à turbine à gaz et ensemble aile portante correspondante |
US9771870B2 (en) * | 2014-03-04 | 2017-09-26 | Rolls-Royce North American Technologies Inc. | Sealing features for a gas turbine engine |
FR3027622B1 (fr) * | 2014-10-28 | 2018-11-09 | Safran Aircraft Engines | Aube de rotor a pilotage de jeu actif, ensemble tournant et son procede de fonctionnement |
KR101643900B1 (ko) * | 2015-06-05 | 2016-07-29 | 두산중공업 주식회사 | 터빈 실링을 위한 탄성 실 |
US10544698B2 (en) * | 2016-06-20 | 2020-01-28 | United Technologies Corporation | Air seal abrasive coating and method |
US10995623B2 (en) * | 2018-04-23 | 2021-05-04 | Rolls-Royce Corporation | Ceramic matrix composite turbine blade with abrasive tip |
US10519777B2 (en) * | 2018-05-14 | 2019-12-31 | General Electric Company | Tip member for blade structure and related method to form turbomachine component |
-
2017
- 2017-09-27 FR FR1758929A patent/FR3071538B1/fr active Active
-
2018
- 2018-09-17 WO PCT/FR2018/052273 patent/WO2019063909A1/fr active Application Filing
- 2018-09-17 US US16/651,052 patent/US11333031B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
WO2019063909A1 (fr) | 2019-04-04 |
US11333031B2 (en) | 2022-05-17 |
US20200277872A1 (en) | 2020-09-03 |
FR3071538A1 (fr) | 2019-03-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLSC | Publication of the preliminary search report |
Effective date: 20190329 |
|
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 |
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PLFP | Fee payment |
Year of fee payment: 7 |