FR3064669B1 - Dispositif d'etancheite d'une turbomachine a revetement abradable - Google Patents
Dispositif d'etancheite d'une turbomachine a revetement abradable Download PDFInfo
- Publication number
- FR3064669B1 FR3064669B1 FR1752801A FR1752801A FR3064669B1 FR 3064669 B1 FR3064669 B1 FR 3064669B1 FR 1752801 A FR1752801 A FR 1752801A FR 1752801 A FR1752801 A FR 1752801A FR 3064669 B1 FR3064669 B1 FR 3064669B1
- Authority
- FR
- France
- Prior art keywords
- strips
- sealing device
- faces
- turbomachine
- abradable coating
- 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
- 239000011248 coating agent Substances 0.000 title abstract 2
- 238000000576 coating method Methods 0.000 title abstract 2
- 238000007789 sealing Methods 0.000 title abstract 2
- 238000005219 brazing Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 229910000679 solder Inorganic materials 0.000 abstract 1
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
-
- 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
- F01D11/127—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 a deformable or crushable structure, e.g. honeycomb
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
- F05D2230/237—Brazing
-
- 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
- F05D2230/50—Building or constructing in particular ways
- F05D2230/51—Building or constructing in particular ways in a modular way, e.g. using several identical or complementary parts or features
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/28—Three-dimensional patterned
- F05D2250/283—Three-dimensional patterned honeycomb
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Est concerné un dispositif d'étanchéité d'un étage mobile de rotor de turbomachine, comprenant un revêtement (46) en matière abradable qui est adapté à coopérer avec des léchettes (40) d'aubes et qui comprend des feuillards (60a,60b) s'étendant suivant des directions d'allongement parallèles le long desquelles les feuillards présentent chacun des créneaux (62) et des redans (64) successifs ayant des faces (56,58) s'étendant parallèlement à ladite direction d'allongement. Deux feuillards adjacents sont fixés entre eux par des brasures à l'endroit de dites faces (56,58) en regard deux à deux de créneaux et redans respectifs. Entre certaines au moins desdites faces en regard les brasures (54) s'étendent sur une partie seulement de la hauteur (H) des feuillards.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1752801A FR3064669B1 (fr) | 2017-03-31 | 2017-03-31 | Dispositif d'etancheite d'une turbomachine a revetement abradable |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1752801 | 2017-03-31 | ||
FR1752801A FR3064669B1 (fr) | 2017-03-31 | 2017-03-31 | Dispositif d'etancheite d'une turbomachine a revetement abradable |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3064669A1 FR3064669A1 (fr) | 2018-10-05 |
FR3064669B1 true FR3064669B1 (fr) | 2020-11-13 |
Family
ID=59745983
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1752801A Active FR3064669B1 (fr) | 2017-03-31 | 2017-03-31 | Dispositif d'etancheite d'une turbomachine a revetement abradable |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3064669B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3112165B1 (fr) | 2020-07-01 | 2022-07-15 | Safran Aircraft Engines | Dispositif abradable d’étanchéité |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1097210B (it) * | 1977-07-29 | 1985-08-26 | Rolls Royce | Perfezionamenti relativi a strutture a nido a'api |
FR2552159B1 (fr) * | 1983-09-21 | 1987-07-10 | Snecma | Dispositif de liaison et d'etancheite de secteurs d'aubes de stator de turbine |
FR3028882B1 (fr) * | 2014-11-20 | 2021-05-28 | Snecma | Procede de realisation d'un revetement abradable multicouches avec structure tubulaire integree, et revetement abradable obtenu par un tel procede |
-
2017
- 2017-03-31 FR FR1752801A patent/FR3064669B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3064669A1 (fr) | 2018-10-05 |
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PLFP | Fee payment |
Year of fee payment: 2 |
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Effective date: 20181005 |
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Year of fee payment: 8 |