FR3117156B1 - Aube pour soufflante de turbomachine d’aéronef comportant un moyen de transmission d’une pluralité de données à distance - Google Patents
Aube pour soufflante de turbomachine d’aéronef comportant un moyen de transmission d’une pluralité de données à distance Download PDFInfo
- Publication number
- FR3117156B1 FR3117156B1 FR2012846A FR2012846A FR3117156B1 FR 3117156 B1 FR3117156 B1 FR 3117156B1 FR 2012846 A FR2012846 A FR 2012846A FR 2012846 A FR2012846 A FR 2012846A FR 3117156 B1 FR3117156 B1 FR 3117156B1
- Authority
- FR
- France
- Prior art keywords
- blade
- transmitting
- remote data
- aircraft turbomachine
- turbomachine fan
- 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
- 230000005540 biological transmission Effects 0.000 abstract 2
- 239000002131 composite material Substances 0.000 abstract 2
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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- 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
- F05D2260/80—Diagnostics
-
- 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
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/334—Vibration measurements
-
- 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
-
- 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)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Cette aube (9, 10) pour soufflante (4) de turbomachine (3) d’aéronef, réalisée en matériau composite, comprend un moyen de transmission configuré pour transmettre à distance (14) une pluralité de données, le moyen de transmission (14) étant localisé dans le matériau composite. Figure pour l’abrégé : Fig 2
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2012846A FR3117156B1 (fr) | 2020-12-08 | 2020-12-08 | Aube pour soufflante de turbomachine d’aéronef comportant un moyen de transmission d’une pluralité de données à distance |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2012846 | 2020-12-08 | ||
FR2012846A FR3117156B1 (fr) | 2020-12-08 | 2020-12-08 | Aube pour soufflante de turbomachine d’aéronef comportant un moyen de transmission d’une pluralité de données à distance |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3117156A1 FR3117156A1 (fr) | 2022-06-10 |
FR3117156B1 true FR3117156B1 (fr) | 2023-09-15 |
Family
ID=75339838
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2012846A Active FR3117156B1 (fr) | 2020-12-08 | 2020-12-08 | Aube pour soufflante de turbomachine d’aéronef comportant un moyen de transmission d’une pluralité de données à distance |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3117156B1 (fr) |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201001000D0 (en) * | 2010-01-22 | 2010-03-10 | Rolls Royce Plc | Method of forming a hollow component with an internal structure |
FR2956206B1 (fr) * | 2010-02-10 | 2012-10-05 | Snecma | Stimulateur vibratoire pour le controle d'une aube d'une roue aubagee d'une turbomachine |
GB201417781D0 (en) * | 2014-10-08 | 2014-11-19 | Rolls Royce Plc | Composite component |
US10938328B2 (en) * | 2016-06-22 | 2021-03-02 | General Electric Company | Harvesting energy from composite aircraft engine components |
US11050011B2 (en) * | 2017-12-18 | 2021-06-29 | Raytheon Technologies Corporation | Sensor assembly for gas turbine engines |
-
2020
- 2020-12-08 FR FR2012846A patent/FR3117156B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3117156A1 (fr) | 2022-06-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20220610 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |