FR3104198B1 - Agencement de limitation de survitesse d’une turbine - Google Patents
Agencement de limitation de survitesse d’une turbine Download PDFInfo
- Publication number
- FR3104198B1 FR3104198B1 FR1913743A FR1913743A FR3104198B1 FR 3104198 B1 FR3104198 B1 FR 3104198B1 FR 1913743 A FR1913743 A FR 1913743A FR 1913743 A FR1913743 A FR 1913743A FR 3104198 B1 FR3104198 B1 FR 3104198B1
- Authority
- FR
- France
- Prior art keywords
- wiper
- carrying
- friction face
- downstream
- upstream
- 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
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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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/006—Arrangements of brakes
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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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
-
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
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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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
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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
- 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
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- 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/02—Purpose of the control system to control rotational speed (n)
- F05D2270/021—Purpose of the control system to control rotational speed (n) to prevent overspeed
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Abstract
L’invention concerne un limiteur de survitesse de turbine de turbomachine, cette turbine comprenant un disque tournant autour d’un axe longitudinal (AX) et portant des aubes rotatives (11), et un distributeur (13) portant des aubes fixes (12), chaque aube rotative (11) comportant une extrémité libre terminée par un talon (19) portant au moins une léchette (23), chaque aube directrice (12) comportant une plateforme (29) radialement externe par laquelle elle est solidarisée à un élément de carter (9). Chaque plateforme (29) a une extrémité amont comportant une face de frottement (36) située en vis-à-vis de la léchette (23), la léchette (23) venant en appui sur la face de frottement (36) en cas de déplacement vers l’aval (AV) du disque tournant. La face de frottement (36) comporte une portion amont cylindrique radialement au même niveau ou plus éloignée qu’une extrémité libre de la léchette (23), et une portion aval conique inclinée selon une orientation qui s’éloigne de l’axe longitudinal (AX) de l’aval (AV) vers l’amont (AM). Figure pour l’abrégé : Figure 3
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1913743A FR3104198B1 (fr) | 2019-12-04 | 2019-12-04 | Agencement de limitation de survitesse d’une turbine |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1913743A FR3104198B1 (fr) | 2019-12-04 | 2019-12-04 | Agencement de limitation de survitesse d’une turbine |
| FR1913743 | 2019-12-04 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3104198A1 FR3104198A1 (fr) | 2021-06-11 |
| FR3104198B1 true FR3104198B1 (fr) | 2022-07-22 |
Family
ID=69700121
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1913743A Active FR3104198B1 (fr) | 2019-12-04 | 2019-12-04 | Agencement de limitation de survitesse d’une turbine |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR3104198B1 (fr) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3154137B1 (fr) * | 2023-10-11 | 2025-10-03 | Safran Aircraft Engines | Turbomachine comportant un dispositif de limitation de survitesse |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2977909B1 (fr) * | 2011-07-12 | 2016-07-15 | Snecma | Aube de rotor pour une turbomachine |
| DE102011086775A1 (de) * | 2011-07-20 | 2013-01-24 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung eines Einlaufbelags, Einlaufsystem, Strömungsmaschine sowie Leitschaufel |
| FR3075863B1 (fr) * | 2017-12-22 | 2019-11-22 | Safran Aircraft Engines | Turbine de turbomachine comportant un dispositif de limitation de survitesse |
-
2019
- 2019-12-04 FR FR1913743A patent/FR3104198B1/fr active Active
Also Published As
| Publication number | Publication date |
|---|---|
| FR3104198A1 (fr) | 2021-06-11 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PLFP | Fee payment |
Year of fee payment: 2 |
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| PLSC | Publication of the preliminary search report |
Effective date: 20210611 |
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| PLFP | Fee payment |
Year of fee payment: 3 |
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| PLFP | Fee payment |
Year of fee payment: 4 |
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| PLFP | Fee payment |
Year of fee payment: 5 |
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| PLFP | Fee payment |
Year of fee payment: 6 |
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| PLFP | Fee payment |
Year of fee payment: 7 |