FR3108141B1 - Aube de compresseur de turbomachine, compresseur et turbomachine munis de celle-ci - Google Patents
Aube de compresseur de turbomachine, compresseur et turbomachine munis de celle-ci Download PDFInfo
- Publication number
- FR3108141B1 FR3108141B1 FR2002353A FR2002353A FR3108141B1 FR 3108141 B1 FR3108141 B1 FR 3108141B1 FR 2002353 A FR2002353 A FR 2002353A FR 2002353 A FR2002353 A FR 2002353A FR 3108141 B1 FR3108141 B1 FR 3108141B1
- Authority
- FR
- France
- Prior art keywords
- thickness
- turbomachine
- compressor
- percentage
- blade
- 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
- 241000795424 Epia Species 0.000 abstract 1
- 238000011144 upstream manufacturing Methods 0.000 abstract 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
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- 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
- F05D2220/321—Application in turbines in gas turbines for a special turbine stage
- F05D2220/3216—Application in turbines in gas turbines for a special turbine stage for a special compressor stage
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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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
L’invention concerne une aube de compresseur de turbomachine, dont une épaisseur (EP) est définie dans la section d’aube par la distance entre un premier point de l’intrados et un deuxième point de l’extrados sur un premier segment perpendiculaire à la corde (AF), l’épaisseur (EP) suivant une courbe (CC) convexe d’épaisseur en fonction du pourcentage (PAF) de corde, la courbe (CC) passant par une épaisseur maximale (Emax) pour une valeur déterminée (XEmax) du pourcentage (PAF), caractérisée en ce que la courbe (CC) d’épaisseur passe par un point intermédiaire (I) de bombement amont, défini par le fait que : le pourcentage (IA) pris au point intermédiaire (I) est compris entre 5 % et 25 % et est inférieur à la valeur déterminée (XEmax), l’épaisseur (EPIA) prise au point intermédiaire (I) est comprise entre 75 % et 85 % de l’épaisseur maximale (Emax). Figure pour l'abrégé : figure 2
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2002353A FR3108141B1 (fr) | 2020-03-10 | 2020-03-10 | Aube de compresseur de turbomachine, compresseur et turbomachine munis de celle-ci |
BE20215105A BE1028097B1 (fr) | 2020-03-10 | 2021-02-17 | Aube de compresseur de turbomachine, compresseur et turbomachine munis de celle-ci |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2002353 | 2020-03-10 | ||
FR2002353A FR3108141B1 (fr) | 2020-03-10 | 2020-03-10 | Aube de compresseur de turbomachine, compresseur et turbomachine munis de celle-ci |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3108141A1 FR3108141A1 (fr) | 2021-09-17 |
FR3108141B1 true FR3108141B1 (fr) | 2022-08-12 |
Family
ID=70457004
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2002353A Active FR3108141B1 (fr) | 2020-03-10 | 2020-03-10 | Aube de compresseur de turbomachine, compresseur et turbomachine munis de celle-ci |
Country Status (2)
Country | Link |
---|---|
BE (1) | BE1028097B1 (fr) |
FR (1) | FR3108141B1 (fr) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE29825097U1 (de) * | 1997-06-24 | 2005-03-24 | Siemens Ag | Verdichterschaufel und Verwendung einer Verdichterschaufel |
US7497664B2 (en) * | 2005-08-16 | 2009-03-03 | General Electric Company | Methods and apparatus for reducing vibrations induced to airfoils |
GB201003084D0 (en) * | 2010-02-24 | 2010-04-14 | Rolls Royce Plc | An aerofoil |
DE102010027588A1 (de) * | 2010-07-19 | 2012-01-19 | Rolls-Royce Deutschland Ltd & Co Kg | Fan-Nachleitradschaufel eines Turbofantriebwerks |
-
2020
- 2020-03-10 FR FR2002353A patent/FR3108141B1/fr active Active
-
2021
- 2021-02-17 BE BE20215105A patent/BE1028097B1/fr active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
FR3108141A1 (fr) | 2021-09-17 |
BE1028097A1 (fr) | 2021-09-20 |
BE1028097B1 (fr) | 2022-01-26 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20210917 |
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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 |