FR3012067A1 - - Google Patents

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Publication number
FR3012067A1
FR3012067A1 FR1459974A FR1459974A FR3012067A1 FR 3012067 A1 FR3012067 A1 FR 3012067A1 FR 1459974 A FR1459974 A FR 1459974A FR 1459974 A FR1459974 A FR 1459974A FR 3012067 A1 FR3012067 A1 FR 3012067A1
Authority
FR
France
Prior art keywords
noise suppression
cells
layer
perforated layer
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
Application number
FR1459974A
Other languages
English (en)
French (fr)
Other versions
FR3012067B1 (fr
Inventor
Charles Michael Biset
Song Chiou
Claude Hubert
Michael Layland
Christian Soria
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rohr Inc
Original Assignee
Rohr Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rohr Inc filed Critical Rohr Inc
Publication of FR3012067A1 publication Critical patent/FR3012067A1/fr
Application granted granted Critical
Publication of FR3012067B1 publication Critical patent/FR3012067B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • 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)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)
  • Wind Motors (AREA)
FR1459974A 2013-10-17 2014-10-17 Panneau structurel acoustique a coeur incline Active FR3012067B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/056,815 US10184398B2 (en) 2013-10-17 2013-10-17 Acoustic structural panel with slanted core

Publications (2)

Publication Number Publication Date
FR3012067A1 true FR3012067A1 (enExample) 2015-04-24
FR3012067B1 FR3012067B1 (fr) 2021-06-11

Family

ID=52781865

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1459974A Active FR3012067B1 (fr) 2013-10-17 2014-10-17 Panneau structurel acoustique a coeur incline

Country Status (3)

Country Link
US (1) US10184398B2 (enExample)
CN (1) CN104564353B (enExample)
FR (1) FR3012067B1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3091901A1 (fr) * 2019-01-22 2020-07-24 Safran Aircraft Engines Dispositif de réduction de bruit avec structure en nid d’abeille à perçage oblique

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10184398B2 (en) 2013-10-17 2019-01-22 Rohr, Inc. Acoustic structural panel with slanted core
US9650963B2 (en) 2015-01-29 2017-05-16 Rohr, Inc. Acoustic structural panel with herringbone core
US9656452B2 (en) 2015-03-12 2017-05-23 Rohr, Inc. Method of forming an acoustic bond panel with insertable acoustic assemblies
US10800117B2 (en) 2015-03-12 2020-10-13 Rohr, Inc. Method of forming an acoustic bond panel with insertable acoustic assemblies
US9708930B2 (en) 2015-12-09 2017-07-18 Rohr, Inc. Multi-degree of freedom acoustic panel
US10174675B2 (en) * 2015-12-30 2019-01-08 General Electric Company Acoustic liner for gas turbine engine components
US9978354B2 (en) 2016-04-15 2018-05-22 Rohr, Inc. Acoustic panel with vertical stiffeners
US9704467B1 (en) 2016-04-15 2017-07-11 Rohr, Inc. Acoustic panel with corrugated baffles and septums
US10253727B2 (en) * 2016-05-12 2019-04-09 Rohr, Inc. Backside acoustic treatment of nacelle structural fittings
CN106003851B (zh) * 2016-06-21 2017-10-27 赵坤 一种蜂巢结构及蜂巢板
US10487943B2 (en) 2016-07-12 2019-11-26 United Technologies Corporation Multi-ply seal ring
US10577117B2 (en) * 2017-08-04 2020-03-03 Hexcel Corporation Angled acoustic honeycomb
US11059559B2 (en) 2018-03-05 2021-07-13 General Electric Company Acoustic liners with oblique cellular structures
US10906659B2 (en) 2018-04-03 2021-02-02 Rohr, Inc. Structured panel with structural reinforcement(s)
US11047304B2 (en) 2018-08-08 2021-06-29 General Electric Company Acoustic cores with sound-attenuating protuberances
US10823059B2 (en) 2018-10-03 2020-11-03 General Electric Company Acoustic core assemblies with mechanically joined acoustic core segments, and methods of mechanically joining acoustic core segments
US11242822B2 (en) 2018-12-14 2022-02-08 Rohr, Inc. Structured panel with multi-panel structure(s)
US11398214B2 (en) 2018-12-14 2022-07-26 Rohr, Inc. Forming a structured panel with one or more structural reinforcements
US11434819B2 (en) 2019-03-29 2022-09-06 General Electric Company Acoustic liners with enhanced acoustic absorption and reduced drag characteristics
US11480106B2 (en) * 2019-05-03 2022-10-25 Raytheon Technologies Corporation Acoustic liner with obliquely angled slots
US11702982B2 (en) * 2019-10-24 2023-07-18 The Boeing Company Blade fragment barrier for aircraft engine inlet cowl
US11668236B2 (en) 2020-07-24 2023-06-06 General Electric Company Acoustic liners with low-frequency sound wave attenuating features
US11970992B2 (en) 2021-06-03 2024-04-30 General Electric Company Acoustic cores and tools and methods for forming the same
FR3126340B1 (fr) * 2021-08-30 2023-11-03 Safran Nacelles Panneau acoustique à cavités obliques
US12142253B2 (en) 2021-10-05 2024-11-12 General Electric Company Solid adhesive film for acoustic liner and method
CN116733786A (zh) * 2022-03-10 2023-09-12 通用电气公司 用于燃气涡轮发动机的吸声器
US11965425B2 (en) 2022-05-31 2024-04-23 General Electric Company Airfoil for a turbofan engine
US12312969B2 (en) 2023-01-17 2025-05-27 General Electric Company Airfoils for turbofan engines

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US2682235A (en) * 1951-12-12 1954-06-29 Fuller Richard Buckminster Building construction
US3734234A (en) 1971-11-08 1973-05-22 Lockheed Aircraft Corp Sound absorption structure
US3821999A (en) 1972-09-05 1974-07-02 Mc Donnell Douglas Corp Acoustic liner
US3913702A (en) 1973-06-04 1975-10-21 Lockheed Aircraft Corp Cellular sound absorptive structure
US4257998A (en) 1978-05-01 1981-03-24 The Boenig Company Method of making a cellular core with internal septum
GB9101395D0 (en) 1991-01-22 1991-03-06 Short Brothers Plc Structural cellular component
US5923003A (en) 1996-09-09 1999-07-13 Northrop Grumman Corporation Extended reaction acoustic liner for jet engines and the like
DE19722202A1 (de) 1997-05-27 1998-12-03 Emitec Emissionstechnologie Schalldämpfergehäuse und zugehöriger Katalysator-Trägerkörper mit Halteelement sowie Verfahren zu dessen Herstellung
US6176964B1 (en) 1997-10-20 2001-01-23 Vought Aircraft Industries, Inc. Method of fabricating an acoustic liner
FR2914773B1 (fr) 2007-04-04 2012-12-14 Airbus France Procede de realisation d'une structure acoustiquement resistive, structure acoustiquement resistive ainsi obtenue et revetement utilisant une telle structure
FR2954281B1 (fr) 2009-12-22 2012-04-06 Airbus Operations Sas Panneau pour le traitement acoustique a epaisseur evolutive
US8579076B2 (en) * 2012-02-29 2013-11-12 Hexcel Corporation Splicing of curved acoustic honeycomb
US10294815B2 (en) 2012-03-01 2019-05-21 The Boeing Company SPF/DB structure for attenuation of noise from air flow
GB201209658D0 (en) * 2012-05-31 2012-07-11 Rolls Royce Plc Acoustic panel
CN202789033U (zh) 2012-08-29 2013-03-13 无锡盛泽环保科技有限公司 一种控制尾气排放用催化器高性能金属蜂窝载体
US9168716B2 (en) * 2012-09-14 2015-10-27 The Boeing Company Metallic sandwich structure having small bend radius
US10184398B2 (en) 2013-10-17 2019-01-22 Rohr, Inc. Acoustic structural panel with slanted core

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3091901A1 (fr) * 2019-01-22 2020-07-24 Safran Aircraft Engines Dispositif de réduction de bruit avec structure en nid d’abeille à perçage oblique
WO2020152418A1 (fr) * 2019-01-22 2020-07-30 Safran Aircraft Engines Dispositif de réduction de bruit avec structure en nid d'abeille à perçage oblique
CN113423934A (zh) * 2019-01-22 2021-09-21 赛峰飞机发动机公司 具有斜刺穿的蜂窝状结构的噪音降低装置
CN113423934B (zh) * 2019-01-22 2024-07-30 赛峰飞机发动机公司 具有斜刺穿的蜂窝状结构的噪音降低装置

Also Published As

Publication number Publication date
CN104564353A (zh) 2015-04-29
FR3012067B1 (fr) 2021-06-11
CN104564353B (zh) 2018-08-24
US20150110603A1 (en) 2015-04-23
US10184398B2 (en) 2019-01-22

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