FR3004748B1 - AIRCRAFT ENGINE BLADE OR BLADE AND METHOD AND SYSTEM FOR CONTROLLING DEFECTS IN COMPOSITES BY PARTICLES HAVING FERROMAGNETIC PROPERTIES - Google Patents
AIRCRAFT ENGINE BLADE OR BLADE AND METHOD AND SYSTEM FOR CONTROLLING DEFECTS IN COMPOSITES BY PARTICLES HAVING FERROMAGNETIC PROPERTIESInfo
- Publication number
- FR3004748B1 FR3004748B1 FR1353574A FR1353574A FR3004748B1 FR 3004748 B1 FR3004748 B1 FR 3004748B1 FR 1353574 A FR1353574 A FR 1353574A FR 1353574 A FR1353574 A FR 1353574A FR 3004748 B1 FR3004748 B1 FR 3004748B1
- Authority
- FR
- France
- Prior art keywords
- blade
- composites
- particles
- aircraft engine
- ferromagnetic properties
- 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
- 239000002131 composite material Substances 0.000 title 1
- 230000005294 ferromagnetic effect Effects 0.000 title 1
- 239000002245 particle Substances 0.000 title 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/005—Repairing methods or devices
-
- 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
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/507—Magnetic properties
-
- 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1353574A FR3004748B1 (en) | 2013-04-19 | 2013-04-19 | AIRCRAFT ENGINE BLADE OR BLADE AND METHOD AND SYSTEM FOR CONTROLLING DEFECTS IN COMPOSITES BY PARTICLES HAVING FERROMAGNETIC PROPERTIES |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1353574A FR3004748B1 (en) | 2013-04-19 | 2013-04-19 | AIRCRAFT ENGINE BLADE OR BLADE AND METHOD AND SYSTEM FOR CONTROLLING DEFECTS IN COMPOSITES BY PARTICLES HAVING FERROMAGNETIC PROPERTIES |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3004748A1 FR3004748A1 (en) | 2014-10-24 |
FR3004748B1 true FR3004748B1 (en) | 2015-04-10 |
Family
ID=48570400
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1353574A Active FR3004748B1 (en) | 2013-04-19 | 2013-04-19 | AIRCRAFT ENGINE BLADE OR BLADE AND METHOD AND SYSTEM FOR CONTROLLING DEFECTS IN COMPOSITES BY PARTICLES HAVING FERROMAGNETIC PROPERTIES |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3004748B1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201511686D0 (en) | 2015-07-03 | 2015-08-19 | Rolls Royce Plc | Composite component |
FR3132322B1 (en) * | 2022-02-03 | 2023-12-22 | Safran Aircraft Engines | Composite blade for an aircraft turbomachine fan comprising means for measuring internal deformations |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2861143B1 (en) * | 2003-10-20 | 2006-01-20 | Snecma Moteurs | TURBOMACHINE BLADE, IN PARTICULAR BLADE OF BLOWER AND METHOD OF MANUFACTURING THE SAME |
FR2951222B1 (en) * | 2009-10-09 | 2013-01-11 | Snecma | DAMPING A ROTATING PIECE BY PASSIVE OR SEMI-PASSIVE DISSIPATIVE PIEZOELECTRIC DEVICE |
FR2961847B1 (en) * | 2010-06-25 | 2012-08-17 | Snecma | AUBES MOBILE WHEEL IN COMPOSITE MATERIAL FOR A TURBINE GAS TURBINE ENGINE WITH A WAVEBASE / TIGHTENING DISC |
US8397580B2 (en) * | 2010-09-16 | 2013-03-19 | The Boeing Company | Multi-ferroic structural health monitoring systems and methods |
-
2013
- 2013-04-19 FR FR1353574A patent/FR3004748B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3004748A1 (en) | 2014-10-24 |
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Legal Events
Date | Code | Title | Description |
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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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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |