JP2011506852A5 - - Google Patents
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- JP2011506852A5 JP2011506852A5 JP2010538859A JP2010538859A JP2011506852A5 JP 2011506852 A5 JP2011506852 A5 JP 2011506852A5 JP 2010538859 A JP2010538859 A JP 2010538859A JP 2010538859 A JP2010538859 A JP 2010538859A JP 2011506852 A5 JP2011506852 A5 JP 2011506852A5
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- JP
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- Prior art keywords
- durable
- silencing
- substructure
- strips
- vesicle
- 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.)
- Pending
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- 230000030279 gene silencing Effects 0.000 claims description 42
- 238000000034 method Methods 0.000 claims description 22
- 230000008569 process Effects 0.000 claims description 19
- 230000003584 silencer Effects 0.000 claims description 16
- 230000004907 flux Effects 0.000 claims description 12
- 238000005192 partition Methods 0.000 claims description 9
- 230000009467 reduction Effects 0.000 claims description 5
- 238000010257 thawing Methods 0.000 claims description 4
- 239000002131 composite material Substances 0.000 description 6
- 230000007246 mechanism Effects 0.000 description 4
- 238000000465 moulding Methods 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 230000009466 transformation Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000006837 decompression Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0760194A FR2925463B1 (fr) | 2007-12-21 | 2007-12-21 | Structure pour le traitement acoustique plus particulierement adaptee a une entree d'air d'une nacelle d'aeronef |
| PCT/FR2008/052312 WO2009081020A1 (fr) | 2007-12-21 | 2008-12-16 | Structure pour le traitement acoustique plus particulierement adaptee a une entree d'air d'une nacelle d'aeronef |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2011506852A JP2011506852A (ja) | 2011-03-03 |
| JP2011506852A5 true JP2011506852A5 (https=) | 2013-11-14 |
Family
ID=39564791
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2010538859A Pending JP2011506852A (ja) | 2007-12-21 | 2008-12-16 | 航空機のナセルの空気取り入れ口に更に特に適応した消音処理用構造体 |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US8413922B2 (https=) |
| EP (1) | EP2244939B1 (https=) |
| JP (1) | JP2011506852A (https=) |
| CN (1) | CN101952168B (https=) |
| BR (1) | BRPI0819482A2 (https=) |
| CA (1) | CA2709331C (https=) |
| FR (1) | FR2925463B1 (https=) |
| RU (1) | RU2482020C2 (https=) |
| WO (1) | WO2009081020A1 (https=) |
Families Citing this family (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8025122B2 (en) * | 2008-11-06 | 2011-09-27 | The Boeing Company | Acoustically treated exhaust centerbody for jet engines and associated methods |
| FR2950325B1 (fr) * | 2009-09-23 | 2011-09-09 | Airbus Operations Sas | Panneau pour le traitement acoustique plus particulierement adapte a une entree d'air d'une nacelle d'aeronef |
| 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 |
| DE102011008920A1 (de) * | 2011-01-19 | 2012-07-19 | Rolls-Royce Deutschland Ltd & Co Kg | Schallabsorber, insbesondere für einen Gasturbinenabgaskonus und Verfahren zu dessen Herstellung |
| FR2976557B1 (fr) * | 2011-06-20 | 2013-07-12 | Airbus Operations Sas | Procede de realisation d'un panneau pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud |
| FR2980774B1 (fr) * | 2011-10-03 | 2013-10-25 | Airbus Operations Sas | Nacelle d'aeronef comportant un dispositif d'alimentation en air chaud d'un panneau combinant les traitements acoustique et du givre |
| FR2980776B1 (fr) * | 2011-10-03 | 2014-08-22 | Airbus Operations Sas | Nacelle d'aeronef comportant un panneau pour le traitement acoustique integrant des canaux d'air chaud et au moins un canal annulaire |
| FR2981049B1 (fr) * | 2011-10-07 | 2014-04-11 | Aircelle Sa | Procede de fabrication d'un panneau d'absorption acoustique |
| US9488067B2 (en) * | 2014-01-14 | 2016-11-08 | The Boeing Company | Aircraft anti-icing systems having deflector vanes |
| US9592918B2 (en) | 2014-06-23 | 2017-03-14 | Rohr, Inc. | Acoustic liner |
| US9771868B2 (en) * | 2015-07-21 | 2017-09-26 | The Boeing Company | Sound attenuation apparatus and method |
| US9587563B2 (en) | 2015-07-21 | 2017-03-07 | The Boeing Company | Sound attenuation apparatus and method |
| 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 |
| US9764818B2 (en) | 2016-02-10 | 2017-09-19 | Rohr, Inc. | Structural, cellular core with corrugated support walls |
| US9761216B2 (en) | 2016-02-10 | 2017-09-12 | Rohr, Inc. | Acoustic panel with angled corrugated core structures |
| US9704467B1 (en) | 2016-04-15 | 2017-07-11 | Rohr, Inc. | Acoustic panel with corrugated baffles and septums |
| US9978354B2 (en) * | 2016-04-15 | 2018-05-22 | Rohr, Inc. | Acoustic panel with vertical stiffeners |
| FR3060829B1 (fr) * | 2016-12-20 | 2019-05-31 | Airbus Operations | Structure constituant un isolant acoustique |
| US10414481B2 (en) | 2017-02-14 | 2019-09-17 | Rohr, Inc. | Method for forming a structural panel |
| US10525636B2 (en) | 2017-06-19 | 2020-01-07 | Rohr, Inc. | Process for forming a fiber-reinforced composite structure |
| US10695986B2 (en) | 2017-08-22 | 2020-06-30 | Rohr, Inc. | Method for forming a structural panel |
| FR3070674B1 (fr) | 2017-09-06 | 2019-09-13 | Safran Nacelles | Integration a la levre acoustique degivree |
| US11125157B2 (en) * | 2017-09-22 | 2021-09-21 | The Boeing Company | Advanced inlet design |
| FR3074776B1 (fr) | 2017-12-13 | 2020-02-28 | Safran Nacelles | Levre d’entree d’air de nacelle pour turboreacteur |
| FR3077800B1 (fr) * | 2018-02-12 | 2020-09-25 | Safran Nacelles | Dispositif de degivrage et de traitement acoustique pour une levre d’entree d’air d’une nacelle de turboreacteur |
| US10906659B2 (en) | 2018-04-03 | 2021-02-02 | Rohr, Inc. | Structured panel with structural reinforcement(s) |
| FR3083265A1 (fr) | 2018-06-29 | 2020-01-03 | Airbus Operations | Structure d'entree d'air pour une nacelle d'aeronef comportant un element amortisseur de chocs |
| US11396366B2 (en) | 2018-09-28 | 2022-07-26 | Rohr, Inc. | Active laminar flow control structural plenums fastened |
| US11524770B2 (en) * | 2018-09-28 | 2022-12-13 | Rohr, Inc. | Active laminar flow control plenum panel arrangements and installation methods |
| US11414203B2 (en) | 2018-09-28 | 2022-08-16 | Rohr, Inc. | Active laminar flow control plenum panel arrangement |
| US11398214B2 (en) | 2018-12-14 | 2022-07-26 | Rohr, Inc. | Forming a structured panel with one or more structural reinforcements |
| US11242822B2 (en) | 2018-12-14 | 2022-02-08 | Rohr, Inc. | Structured panel with multi-panel structure(s) |
| US11572850B2 (en) | 2019-06-04 | 2023-02-07 | Rohr, Inc. | Acoustic panel with one or more structural stiffeners |
| FR3100842A1 (fr) * | 2019-09-12 | 2021-03-19 | Airbus Operations | Entrée d'air, nacelle, ensemble propulsif et aéronef à lèvre rainurée |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3033734A (en) * | 1959-08-27 | 1962-05-08 | Gen Electric | Honeycomb structures |
| DE2314396B1 (de) * | 1973-03-22 | 1974-06-20 | Vasiljevic Costa Silard Dipl I | Vorrichtung zur Schalldaempfung unter Verwendung von Resonatoren |
| US3913702A (en) * | 1973-06-04 | 1975-10-21 | Lockheed Aircraft Corp | Cellular sound absorptive structure |
| US3933327A (en) * | 1974-08-30 | 1976-01-20 | Rohr Industries, Inc. | Aircraft anti-icing plenum |
| GB2038410B (en) * | 1978-12-27 | 1982-11-17 | Rolls Royce | Acoustic lining utilising resonance |
| DE3504208A1 (de) * | 1985-02-07 | 1986-08-07 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V., 8000 München | Schalldaempfer-box |
| FR2613773B1 (fr) * | 1987-04-08 | 1990-11-30 | Snecma | Panneau acoustique pour garniture insonorisante et turboreacteur comportant une telle garniture |
| US5228643A (en) * | 1992-06-25 | 1993-07-20 | Mcdonnell Douglas Corporation | Energy-exchange system incorporating small-diameter tubes |
| US5841079A (en) * | 1997-11-03 | 1998-11-24 | Northrop Grumman Corporation | Combined acoustic and anti-ice engine inlet liner |
| US6371411B1 (en) * | 1999-11-23 | 2002-04-16 | The Boeing Company | Method and apparatus for aircraft inlet ice protection |
| FR2820715B1 (fr) * | 2001-02-15 | 2003-05-30 | Eads Airbus Sa | Procede de degivrage d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre |
| 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 |
| FR2844304B1 (fr) * | 2002-09-10 | 2004-12-10 | Airbus France | Couche acoustiquement resistive pour panneau d'attenuation acoustique, panneau utilisant une telle couche |
| US7047725B2 (en) * | 2003-05-28 | 2006-05-23 | Rohr, Inc. | Assembly and method for aircraft engine noise reduction |
| US7328771B2 (en) * | 2004-07-27 | 2008-02-12 | United Technologies Corporation | Zero acoustic splice fan case liner |
| RU44101U1 (ru) * | 2004-10-11 | 2005-02-27 | Открытое акционерное общество "Научно-производственное объединение Наука" (ОАО НПО "Наука") | Глушитель шума |
| US7311175B2 (en) * | 2005-08-10 | 2007-12-25 | United Technologies Corporation | Acoustic liner with bypass cooling |
| FR2917067B1 (fr) * | 2007-06-08 | 2009-08-21 | Airbus France Sas | Revetement pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud |
-
2007
- 2007-12-21 FR FR0760194A patent/FR2925463B1/fr not_active Expired - Fee Related
-
2008
- 2008-12-16 RU RU2010130454/11A patent/RU2482020C2/ru not_active IP Right Cessation
- 2008-12-16 EP EP08864153A patent/EP2244939B1/fr active Active
- 2008-12-16 US US12/809,742 patent/US8413922B2/en not_active Expired - Fee Related
- 2008-12-16 CA CA2709331A patent/CA2709331C/fr not_active Expired - Fee Related
- 2008-12-16 JP JP2010538859A patent/JP2011506852A/ja active Pending
- 2008-12-16 BR BRPI0819482 patent/BRPI0819482A2/pt not_active Application Discontinuation
- 2008-12-16 WO PCT/FR2008/052312 patent/WO2009081020A1/fr not_active Ceased
- 2008-12-16 CN CN2008801230323A patent/CN101952168B/zh active Active
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