CN101652809A - 一种阻尼消音结构的制造方法,由该方法获取的阻尼消音结构及使用该结构的衬垫 - Google Patents
一种阻尼消音结构的制造方法,由该方法获取的阻尼消音结构及使用该结构的衬垫 Download PDFInfo
- Publication number
- CN101652809A CN101652809A CN200880011435A CN200880011435A CN101652809A CN 101652809 A CN101652809 A CN 101652809A CN 200880011435 A CN200880011435 A CN 200880011435A CN 200880011435 A CN200880011435 A CN 200880011435A CN 101652809 A CN101652809 A CN 101652809A
- Authority
- CN
- China
- Prior art keywords
- viscose glue
- damping noise
- porous layer
- reducing structure
- noise
- 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.)
- Granted
Links
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- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 239000004831 Hot glue Substances 0.000 description 1
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Images
Classifications
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/172—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects
-
- 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
-
- 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
- F02C7/24—Heat or noise insulation
-
- 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
- F05D2300/70—Treatment or modification of materials
- F05D2300/702—Reinforcement
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
- Y10T156/1056—Perforating lamina
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Laminated Bodies (AREA)
- Building Environments (AREA)
Abstract
Description
Claims (8)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0754275A FR2914773B1 (fr) | 2007-04-04 | 2007-04-04 | Procede de realisation d'une structure acoustiquement resistive, structure acoustiquement resistive ainsi obtenue et revetement utilisant une telle structure |
FR0754275 | 2007-04-04 | ||
PCT/FR2008/050561 WO2008135702A2 (fr) | 2007-04-04 | 2008-03-28 | Procede de realisation d'une structure acoustiquement resistive, structure acoustiquement resistive ainsi obtenue et revetement utilisant une telle structure |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101652809A true CN101652809A (zh) | 2010-02-17 |
CN101652809B CN101652809B (zh) | 2012-10-03 |
Family
ID=38669406
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2008800114359A Expired - Fee Related CN101652809B (zh) | 2007-04-04 | 2008-03-28 | 一种阻尼消音结构的制造方法,由该方法获取的阻尼消音结构及使用该结构的衬垫 |
Country Status (9)
Country | Link |
---|---|
US (1) | US7946385B2 (zh) |
EP (1) | EP2132730B1 (zh) |
JP (1) | JP5177587B2 (zh) |
CN (1) | CN101652809B (zh) |
BR (1) | BRPI0809177A2 (zh) |
CA (1) | CA2682306C (zh) |
FR (1) | FR2914773B1 (zh) |
RU (1) | RU2470383C2 (zh) |
WO (1) | WO2008135702A2 (zh) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102883872A (zh) * | 2010-03-02 | 2013-01-16 | 吉凯恩航空服务有限公司 | 无缝声衬垫 |
CN104564353A (zh) * | 2013-10-17 | 2015-04-29 | 罗尔公司 | 具有倾斜芯的声音结构面板 |
CN107438881A (zh) * | 2015-04-10 | 2017-12-05 | Mra***有限公司 | 声衬和建构声衬的方法 |
CN107664069A (zh) * | 2016-07-28 | 2018-02-06 | 波音公司 | 衬垫组件、发动机壳体及其组装方法 |
CN108725748A (zh) * | 2017-04-25 | 2018-11-02 | 空中客车运营简化股份公司 | 声学处理面板及飞行器 |
CN108759948A (zh) * | 2018-08-31 | 2018-11-06 | 四川菲罗米特仪表有限公司 | 一种气体超声流量计的内置整流器 |
CN109630272A (zh) * | 2018-11-02 | 2019-04-16 | 中国航空工业集团公司西安飞机设计研究所 | 一种减低飞机噪音的方法及消音衬垫 |
CN110573328A (zh) * | 2017-05-01 | 2019-12-13 | 赫克赛尔公司 | 封堵的隔音蜂窝体 |
CN110815901A (zh) * | 2019-10-17 | 2020-02-21 | 成都飞机工业(集团)有限责任公司 | 一种蜂窝夹芯复合材料声衬壁板通孔率控制方法 |
CN111373470A (zh) * | 2017-09-06 | 2020-07-03 | 赛峰短舱公司 | 用于制造用于吸音板的蜂窝芯体的方法 |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008104716A2 (fr) * | 2007-02-20 | 2008-09-04 | Airbus France | Procede de realisation d ' un revetement pour le traitement acoustique et revetement ainsi obtenu |
JP5762284B2 (ja) * | 2008-05-22 | 2015-08-12 | スリーエム イノベイティブ プロパティズ カンパニー | メッシュ層を含む多層吸音構造物 |
FR2953811B1 (fr) * | 2009-12-15 | 2012-03-16 | Airbus Operations Sas | Panneau pour une entree d'air d'une nacelle d'aeronef assurant un traitement acoustique et un traitement du givre optimises |
DE102010051583A1 (de) * | 2010-11-05 | 2012-05-10 | Progress-Werk Oberkirch Ag | Schallabsorbierendes Abschirmelement |
FR2969702B1 (fr) * | 2010-12-23 | 2014-10-10 | Ge Energy Products France Snc | Enceinte pour equipement thermique et procede de montage |
GB201121887D0 (en) | 2011-12-20 | 2012-02-01 | Rolls Royce Plc | Intake liner for a gas turbine engine |
US9651059B2 (en) * | 2012-12-27 | 2017-05-16 | United Technologies Corporation | Adhesive pattern for fan case conformable liner |
US20150267593A1 (en) * | 2013-08-28 | 2015-09-24 | The Boeing Company | System and method for forming elongated perforations in an inner barrel section of an engine |
CN104552445B (zh) * | 2013-10-21 | 2016-09-14 | 哈尔滨飞机工业集团有限责任公司 | 一种航空复合材料消音板的胶膜制孔方法 |
US10072511B2 (en) | 2014-10-02 | 2018-09-11 | Rolls-Royce North American Technologies Inc. | Engine nacelle |
GB201511454D0 (en) | 2015-06-30 | 2015-08-12 | Rolls Royce Plc | Aircraft engine nacelle |
FR3041937B1 (fr) * | 2015-10-05 | 2017-10-20 | Airbus Operations Sas | Structure compartimentee pour le traitement acoustique et le degivrage d'une nacelle d'aeronef et nacelle d'aeronef incorporant ladite structure |
GB201521075D0 (en) * | 2015-11-30 | 2016-01-13 | Short Brothers Plc | Methods, precursors and abrasive blasting masks for manufacturing noise attenuating devices |
US10443496B2 (en) * | 2016-07-18 | 2019-10-15 | The Boeing Company | Acoustic paneling |
US10720135B2 (en) | 2016-07-18 | 2020-07-21 | The Boeing Company | Acoustic panels that include multi-layer facesheets |
CN109563994B (zh) * | 2016-07-25 | 2020-12-01 | 西门子股份公司 | 具有谐振器环的燃气涡轮发动机 |
RU2720151C1 (ru) * | 2019-04-23 | 2020-04-24 | федеральное государственное бюджетное образовательное учреждение высшего образования "Пермский национальный исследовательский политехнический университет" | Способ изготовления звукопоглощающей конструкции |
FR3102882B1 (fr) * | 2019-10-31 | 2021-11-12 | Safran Nacelles | Panneau d’atténuation acoustique et ses procédés de fabrication |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
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US3329740A (en) * | 1965-07-06 | 1967-07-04 | United Shoe Machinery Corp | Thermoplastic adhesive prepared from crystallizable polyester resins and amorphous phenoxy resin |
DE3243713C2 (de) * | 1982-11-26 | 1985-05-15 | Fr. Kammerer GmbH, 7530 Pforzheim | Flachwärmetauscherplatte und Verfahren zu deren Herstellung |
US5747573A (en) * | 1994-02-07 | 1998-05-05 | H. B. Fuller Licensing & Financing, Inc. | High heat resistant hot melt adhesive |
US5604010A (en) * | 1996-01-11 | 1997-02-18 | Hartz; Dale E. | Composite honeycomb sandwich structure |
WO1998018656A1 (de) * | 1996-10-29 | 1998-05-07 | Rieter Automotive (International) Ag | Ultraleichter multifunktionaler, schallisolierender bausatz |
US6176964B1 (en) * | 1997-10-20 | 2001-01-23 | Vought Aircraft Industries, Inc. | Method of fabricating an acoustic liner |
US6190602B1 (en) * | 1998-03-13 | 2001-02-20 | Aztex, Inc. | Method of manufacturing a perforated laminate |
FR2817994B1 (fr) * | 2000-12-08 | 2003-02-28 | Eads Airbus Sa | Panneau acoustique sandwich |
FR2818581B1 (fr) * | 2000-12-21 | 2003-03-28 | Eads Airbus Sa | Procede de fabrication d'un panneau a couche d'amortissement acoustique protegee et panneau acoustique ainsi obtenu |
FR2826168B1 (fr) | 2001-06-19 | 2003-12-05 | Eads Airbus Sa | Procede de realisation d'une couche acoustiquement resistive renforcee, couche resistive ainsi obtenue et panneau utilisant une telle couche |
JP4187101B2 (ja) * | 2003-08-01 | 2008-11-26 | 河西工業株式会社 | 車両用吸音材及びその製造方法 |
DE202004018241U1 (de) * | 2004-11-24 | 2006-04-06 | Fritz Egger Gmbh & Co | Deckschicht und Paneel mit schallabsorbierenden Eigenschaften |
US7484593B2 (en) * | 2004-12-02 | 2009-02-03 | The Boeing Company | Acoustic structure and method of manufacturing thereof |
DE602006014338D1 (de) * | 2005-09-15 | 2010-07-01 | Ricoh Kk | Wärmeempfindliche Klebekomponente und wärmeempfindliche Klebeetikettfolie |
US7540354B2 (en) * | 2006-05-26 | 2009-06-02 | United Technologies Corporation | Micro-perforated acoustic liner |
-
2007
- 2007-04-04 FR FR0754275A patent/FR2914773B1/fr not_active Expired - Fee Related
-
2008
- 2008-03-28 US US12/594,657 patent/US7946385B2/en not_active Expired - Fee Related
- 2008-03-28 CN CN2008800114359A patent/CN101652809B/zh not_active Expired - Fee Related
- 2008-03-28 BR BRPI0809177-3A patent/BRPI0809177A2/pt not_active IP Right Cessation
- 2008-03-28 EP EP08788087.8A patent/EP2132730B1/fr not_active Not-in-force
- 2008-03-28 JP JP2010501567A patent/JP5177587B2/ja not_active Expired - Fee Related
- 2008-03-28 CA CA2682306A patent/CA2682306C/fr active Active
- 2008-03-28 RU RU2009140764/28A patent/RU2470383C2/ru not_active IP Right Cessation
- 2008-03-28 WO PCT/FR2008/050561 patent/WO2008135702A2/fr active Application Filing
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102883872A (zh) * | 2010-03-02 | 2013-01-16 | 吉凯恩航空服务有限公司 | 无缝声衬垫 |
CN104564353B (zh) * | 2013-10-17 | 2018-08-24 | 罗尔公司 | 具有倾斜芯的声音结构面板 |
CN104564353A (zh) * | 2013-10-17 | 2015-04-29 | 罗尔公司 | 具有倾斜芯的声音结构面板 |
US10184398B2 (en) | 2013-10-17 | 2019-01-22 | Rohr, Inc. | Acoustic structural panel with slanted core |
US10971128B2 (en) | 2015-04-10 | 2021-04-06 | Mra Systems, Llc | Acoustic liner and methods of constructing an acoustic liner |
CN107438881A (zh) * | 2015-04-10 | 2017-12-05 | Mra***有限公司 | 声衬和建构声衬的方法 |
CN107438881B (zh) * | 2015-04-10 | 2021-12-14 | Mra***有限责任公司 | 声衬和建构声衬的方法 |
CN107664069A (zh) * | 2016-07-28 | 2018-02-06 | 波音公司 | 衬垫组件、发动机壳体及其组装方法 |
CN108725748A (zh) * | 2017-04-25 | 2018-11-02 | 空中客车运营简化股份公司 | 声学处理面板及飞行器 |
CN108725748B (zh) * | 2017-04-25 | 2021-04-23 | 空中客车运营简化股份公司 | 声学处理面板及飞行器 |
CN110573328A (zh) * | 2017-05-01 | 2019-12-13 | 赫克赛尔公司 | 封堵的隔音蜂窝体 |
CN111373470A (zh) * | 2017-09-06 | 2020-07-03 | 赛峰短舱公司 | 用于制造用于吸音板的蜂窝芯体的方法 |
CN111373470B (zh) * | 2017-09-06 | 2024-02-23 | 赛峰短舱公司 | 用于制造用于吸音板的蜂窝芯体的方法 |
CN108759948A (zh) * | 2018-08-31 | 2018-11-06 | 四川菲罗米特仪表有限公司 | 一种气体超声流量计的内置整流器 |
CN109630272A (zh) * | 2018-11-02 | 2019-04-16 | 中国航空工业集团公司西安飞机设计研究所 | 一种减低飞机噪音的方法及消音衬垫 |
CN109630272B (zh) * | 2018-11-02 | 2023-06-23 | 中国航空工业集团公司西安飞机设计研究所 | 一种减低飞机噪音的方法及消音衬垫 |
CN110815901A (zh) * | 2019-10-17 | 2020-02-21 | 成都飞机工业(集团)有限责任公司 | 一种蜂窝夹芯复合材料声衬壁板通孔率控制方法 |
Also Published As
Publication number | Publication date |
---|---|
EP2132730A2 (fr) | 2009-12-16 |
RU2470383C2 (ru) | 2012-12-20 |
FR2914773B1 (fr) | 2012-12-14 |
JP5177587B2 (ja) | 2013-04-03 |
CA2682306A1 (fr) | 2008-11-13 |
RU2009140764A (ru) | 2011-05-10 |
WO2008135702A3 (fr) | 2008-12-31 |
JP2010523878A (ja) | 2010-07-15 |
US20100126798A1 (en) | 2010-05-27 |
BRPI0809177A2 (pt) | 2014-09-16 |
CN101652809B (zh) | 2012-10-03 |
CA2682306C (fr) | 2017-01-31 |
WO2008135702A2 (fr) | 2008-11-13 |
FR2914773A1 (fr) | 2008-10-10 |
EP2132730B1 (fr) | 2015-10-07 |
US7946385B2 (en) | 2011-05-24 |
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