FR2912780B1 - Revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe - Google Patents
Revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexeInfo
- Publication number
- FR2912780B1 FR2912780B1 FR0753357A FR0753357A FR2912780B1 FR 2912780 B1 FR2912780 B1 FR 2912780B1 FR 0753357 A FR0753357 A FR 0753357A FR 0753357 A FR0753357 A FR 0753357A FR 2912780 B1 FR2912780 B1 FR 2912780B1
- Authority
- FR
- France
- Prior art keywords
- coating
- complex shape
- acoustic treatment
- alveolar structure
- treatment incorporating
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0286—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- 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
- F05D2250/282—Three-dimensional patterned cubic pattern
-
- 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
-
- 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
- F05D2250/30—Arrangement of components
- F05D2250/32—Arrangement of components according to their shape
-
- 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
- F05D2250/70—Shape
- F05D2250/71—Shape curved
-
- 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)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0753357A FR2912780B1 (fr) | 2007-02-20 | 2007-02-20 | Revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe |
US12/527,984 US20100089690A1 (en) | 2007-02-20 | 2008-02-14 | Method for making an acoustic treatment coating and coating thus obtained |
JP2009549456A JP2010519445A (ja) | 2007-02-20 | 2008-02-14 | 複雑な形状の、セル状構造を備える吸音処理被覆材の製作方法及びそのようにして得られる吸音処理被覆材 |
CA2678476A CA2678476A1 (fr) | 2007-02-20 | 2008-02-14 | Procede de realisation d'un revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe et revetement pour le traitement acoustique ainsiobtenu |
CN200880005569A CN101636575A (zh) | 2007-02-20 | 2008-02-14 | 一种消音衬垫的实施方法及用此方法获得的衬垫 |
EP08762096A EP2140120A2 (fr) | 2007-02-20 | 2008-02-14 | Procede de realisation d'un revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe et revetement pour le traitement acoustique ainsi obtenu |
BRPI0807276-0A BRPI0807276A2 (pt) | 2007-02-20 | 2008-02-14 | "processo de realização de um revestimento para o tratamento acústico aplicado no nível de uma superfície a tratar de uma aeronave, revestimento para o tratamento acústico, e nacela de aeronave" |
RU2009134984/06A RU2455510C2 (ru) | 2007-02-20 | 2008-02-14 | Способ выполнения покрытия для акустической обработки, включающее ячеистую структуру сложной формы, и покрытие для акустической обработки, полученное таким образом |
PCT/FR2008/050248 WO2008104716A2 (fr) | 2007-02-20 | 2008-02-14 | Procede de realisation d ' un revetement pour le traitement acoustique et revetement ainsi obtenu |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0753357A FR2912780B1 (fr) | 2007-02-20 | 2007-02-20 | Revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2912780A1 FR2912780A1 (fr) | 2008-08-22 |
FR2912780B1 true FR2912780B1 (fr) | 2012-03-02 |
Family
ID=38596572
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0753357A Active FR2912780B1 (fr) | 2007-02-20 | 2007-02-20 | Revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe |
Country Status (2)
Country | Link |
---|---|
CN (1) | CN101636575A (fr) |
FR (1) | FR2912780B1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2966801B1 (fr) * | 2010-10-29 | 2012-11-02 | Aircelle Sa | Structure de bord d'attaque notamment pour entree d'air de nacelle de moteur d'aeronef |
FR2971613B1 (fr) * | 2011-02-10 | 2013-03-15 | Airbus Operations Sas | Panneau pour le traitement acoustique comprenant une jonction entre deux parties et procede de reparation d'un panneau pour le traitement acoustique |
FR2983835B1 (fr) | 2011-12-13 | 2014-02-21 | Airbus Operations Sas | Procede de realisation d'un panneau pour le traitement acoustique |
FR2984429B1 (fr) * | 2011-12-16 | 2014-02-14 | Snecma | Bandes d'amortissement de vibrations a evacuation de fluides, pour protection acoustique de carter de soufflante de turbomachine d'aeronef |
US10851713B2 (en) * | 2017-08-29 | 2020-12-01 | Mra Systems, Llc. | Acoustic liner having internal structure |
CN112984768B (zh) * | 2021-03-17 | 2024-08-30 | 马鞍山迈安特航空制造有限公司 | 降噪结构 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2024380A (en) * | 1978-04-29 | 1980-01-09 | Rolls Royce | Acoustic linings for fluid flow ducts |
US4452335A (en) * | 1982-05-03 | 1984-06-05 | United Technologies Corporation | Sound absorbing structure for a gas turbine engine |
FR2820716B1 (fr) * | 2001-02-15 | 2003-05-30 | Eads Airbus Sa | Procede de degivrage par circulation forcee d'un fluide, d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre |
GB0119608D0 (en) * | 2001-08-11 | 2001-10-03 | Rolls Royce Plc | A guide vane assembly |
DE202004002363U1 (de) * | 2004-02-13 | 2004-04-22 | Deutsche Bahn Ag | Leichtmetallprofil mit integrierten Bodenblech zur Gestaltung einer akustisch optimierten Beugungskante |
DE102004053383A1 (de) * | 2004-11-02 | 2006-05-04 | Eads Deutschland Gmbh | Akustischer Absorber für Flugtriebwerke |
-
2007
- 2007-02-20 FR FR0753357A patent/FR2912780B1/fr active Active
-
2008
- 2008-02-14 CN CN200880005569A patent/CN101636575A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
FR2912780A1 (fr) | 2008-08-22 |
CN101636575A (zh) | 2010-01-27 |
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Legal Events
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CA | Change of address |
Effective date: 20110916 |
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CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
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CJ | Change in legal form |
Effective date: 20110916 |
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TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
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