ATE276100T1 - Schallabsorbiernedes element insbesondere für flugzeugtriebwerke - Google Patents

Schallabsorbiernedes element insbesondere für flugzeugtriebwerke

Info

Publication number
ATE276100T1
ATE276100T1 AT01402803T AT01402803T ATE276100T1 AT E276100 T1 ATE276100 T1 AT E276100T1 AT 01402803 T AT01402803 T AT 01402803T AT 01402803 T AT01402803 T AT 01402803T AT E276100 T1 ATE276100 T1 AT E276100T1
Authority
AT
Austria
Prior art keywords
sound absorbing
absorbing element
aircraft engines
element particularly
separators
Prior art date
Application number
AT01402803T
Other languages
English (en)
Inventor
Alain Porte
Herve Batard
Original Assignee
Airbus France
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 Airbus France filed Critical Airbus France
Application granted granted Critical
Publication of ATE276100T1 publication Critical patent/ATE276100T1/de

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
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/827—Sound absorbing structures or liners
    • 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
    • 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)
  • Architecture (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Physics & Mathematics (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Aerials With Secondary Devices (AREA)
  • Laminated Bodies (AREA)
  • Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
AT01402803T 2000-10-31 2001-10-29 Schallabsorbiernedes element insbesondere für flugzeugtriebwerke ATE276100T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0013977A FR2815900B1 (fr) 2000-10-31 2000-10-31 Panneau sandwich reducteur de bruit, notamment pour turboreacteur d'aeronef

Publications (1)

Publication Number Publication Date
ATE276100T1 true ATE276100T1 (de) 2004-10-15

Family

ID=8855939

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01402803T ATE276100T1 (de) 2000-10-31 2001-10-29 Schallabsorbiernedes element insbesondere für flugzeugtriebwerke

Country Status (7)

Country Link
US (1) US6536556B2 (de)
EP (1) EP1201420B1 (de)
AT (1) ATE276100T1 (de)
CA (1) CA2359924C (de)
DE (1) DE60105521T2 (de)
ES (1) ES2227094T3 (de)
FR (1) FR2815900B1 (de)

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FR2821788B1 (fr) * 2001-03-09 2004-04-02 Eads Airbus Sa Procede de fabrication d'un panneau a couche resistive acoustique adaptee et panneau acoustique ainsi obtenu
US6871725B2 (en) * 2003-02-21 2005-03-29 Jeffrey Don Johnson Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture
JP4050632B2 (ja) * 2003-02-24 2008-02-20 株式会社神戸製鋼所 吸音構造体
US7328771B2 (en) 2004-07-27 2008-02-12 United Technologies Corporation Zero acoustic splice fan case liner
US8413761B2 (en) * 2005-04-04 2013-04-09 Hexcel Corporation Acoustic honeycomb with perforated septum caps
US7434659B2 (en) * 2005-04-04 2008-10-14 Hexcel Corporation Acoustic septum cap honeycomb
US20070193175A1 (en) * 2006-02-21 2007-08-23 Ta-Chung Hao Structure of decoration acoustic board
US20080083210A1 (en) * 2006-10-04 2008-04-10 Spirit Aerosystems, Inc Monolithic thrust reverser components
FR2922152B1 (fr) * 2007-10-16 2009-11-20 Aircelle Sa Structure a ame alveolaire pour panneau acoustique
US8240427B2 (en) * 2008-10-01 2012-08-14 General Electric Company Sound attenuation systems and methods
DE102008051241B4 (de) 2008-10-10 2011-06-16 Airbus Operations Gmbh Schalldämpfer für ein Hilfstriebwerk eines Flugzeugs
FR2947013B1 (fr) * 2009-06-18 2013-08-02 Airbus France Aerogenerateur carene.
US8127889B1 (en) 2009-09-15 2012-03-06 The Boeing Company Noise reduction system for structures
US8220588B2 (en) * 2010-03-31 2012-07-17 The Boeing Company Unitized engine nacelle structure
US8047329B1 (en) 2010-08-13 2011-11-01 Rohr, Inc. System and method for noise suppression
DE202011001683U1 (de) 2011-01-18 2011-03-17 Pfw Aerospace Ag Schalldämmmaterial
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US10294815B2 (en) 2012-03-01 2019-05-21 The Boeing Company SPF/DB structure for attenuation of noise from air flow
US8800714B2 (en) * 2012-06-26 2014-08-12 Hexcel Corporation Structure with active acoustic openings
CA2904186C (en) * 2013-06-13 2021-03-09 The Boeing Company Superplastic forming/diffusion bonding structure for attenuation of noise from air flow
US9068345B2 (en) * 2013-08-12 2015-06-30 Hexcel Corporation Multi-sectional acoustic septum
US8997923B2 (en) * 2013-08-12 2015-04-07 Hexcel Corporation Sound wave guide for use in acoustic structures
US20150108248A1 (en) * 2013-10-22 2015-04-23 Rohr, Inc. Thrust reverser fan ramp with noise suppression
US9938852B2 (en) 2014-04-30 2018-04-10 The Boeing Company Noise attenuating lipskin assembly and methods of assembling the same
US9656761B2 (en) 2014-04-30 2017-05-23 The Boeing Company Lipskin for a nacelle and methods of making the same
US9708072B2 (en) 2014-04-30 2017-07-18 The Boeing Company Aircraft engine nacelle bulkheads and methods of assembling the same
US9604438B2 (en) 2014-04-30 2017-03-28 The Boeing Company Methods and apparatus for noise attenuation in an engine nacelle
USD726954S1 (en) * 2014-08-05 2015-04-14 General Luminaire Co., Ltd. Hexagonal lamp panel
FR3026122B1 (fr) * 2014-09-24 2019-08-09 Safran Aircraft Engines Panneau de traitement acoustique
FR3036061B1 (fr) * 2015-05-12 2019-08-16 Safran Nacelles Panneau composite et nacelle de turboreacteur d’aeronef comprenant un tel panneau
US10793282B2 (en) 2016-07-28 2020-10-06 The Boeing Company Liner assembly, engine housing, and methods of assembling the same
US10316755B2 (en) * 2016-11-18 2019-06-11 Rohr, Inc. Acoustic panel with sidewall stringers
US10309305B2 (en) * 2016-11-18 2019-06-04 Rohr, Inc. Acoustic panel with sidewall stringers
US10032445B1 (en) * 2016-12-13 2018-07-24 Northrop Grumman Systems Corporation Honeycomb unit cell acoustic metamaterial with in situ buttresses for tuned acoustic frequency attenuation
US10519859B2 (en) * 2017-03-07 2019-12-31 United Technologies Corporation Flutter dampening acoustic liner for a turbofan engine
US10369763B2 (en) * 2017-04-19 2019-08-06 The Boeing Company Segmented acoustic insert
US10577117B2 (en) * 2017-08-04 2020-03-03 Hexcel Corporation Angled acoustic honeycomb
FR3070438B1 (fr) * 2017-08-25 2020-09-11 Safran Nacelles Structure alveolaire et dispositif d’attenuation acoustique pour nacelle d'ensemble propulsif d'aeronef
US10783869B2 (en) * 2017-09-12 2020-09-22 Honeywell International Inc. Cell structure for use in an acoustic panel, and methods of producing the same
US10726824B2 (en) * 2017-09-29 2020-07-28 The Boeing Company Composite sound absorption panel assembly
US11034460B2 (en) * 2017-12-08 2021-06-15 The Boeing Company Additively manufactured septa for acoustic panels
US10836502B2 (en) * 2017-12-15 2020-11-17 The Boeing Company Wave-shaped acoustic insert and core
US11092077B2 (en) * 2018-03-28 2021-08-17 Pratt & Whitney Canada Corp. Aircraft component and method of manufacture
US11052987B2 (en) * 2018-05-30 2021-07-06 The Boeing Company Integrally damped composite aircraft floor panels
FR3082987B1 (fr) * 2018-06-25 2020-09-18 Airbus Operations Sas Structure constituant un isolant acoustique
US11359577B2 (en) 2018-08-22 2022-06-14 Rohr, Inc. Multi-degree of freedom acoustic panel
US11260641B2 (en) 2019-05-10 2022-03-01 American Honda Motor Co., Inc. Apparatus for reticulation of adhesive and methods of use thereof
EP3747735A1 (de) * 2019-06-07 2020-12-09 SABIC Global Technologies B.V. Strukturkörper für fahrzeuge mit wabeneinsätzen und verfahren zur herstellung und verwendung davon
US11715450B2 (en) 2020-12-22 2023-08-01 Rohr, Inc. Acoustic panel core cell with funnel shaped septum
US11965465B2 (en) 2020-12-22 2024-04-23 Rohr, Inc. Acoustic panel with multiple layer corrugated core
IT202100002015A1 (it) * 2021-02-01 2021-05-01 Aprea Vincenzo Dispositivo di isolamento acustico ottimizzato
FR3120732B1 (fr) * 2021-03-10 2023-10-27 Airbus Operations Sas Procédé de fabrication d’une structure d’absorption acoustique, structure d’absorption acoustique ainsi obtenue
FR3121710B1 (fr) * 2021-04-12 2023-11-24 Safran Nacelles Panneau acoustique pour turbomachine
US11869472B2 (en) 2021-08-02 2024-01-09 Rohr, Inc. Acoustic panel with reconfigurable chamber constrictions
CN114453596B (zh) * 2021-09-29 2023-07-11 厦门大学 一种具有降噪功能的飞机壁板3d打印系统
WO2023119130A1 (en) * 2021-12-21 2023-06-29 Sabic Global Technologies B.V. Multiwall sheet including an acoustic resonator
US12319425B2 (en) 2022-01-04 2025-06-03 Rohr, Inc. Multi-core acoustic panel for an aircraft propulsion system
US12180608B2 (en) * 2022-03-07 2024-12-31 Rohr, Inc. Forming acoustic panel with multi-layered septum(s)
US12339032B2 (en) 2022-06-03 2025-06-24 International Business Machines Corporation Acoustic dampening air moving device housing
US12012217B2 (en) * 2022-08-22 2024-06-18 Gulfstream Aerospace Corporation Auxiliary power unit air inlet door with specified acoustic reflecting and/or diffusing characteristics
US12163472B2 (en) 2022-09-02 2024-12-10 Rohr, Inc. Engine exhaust nozzle with acoustic attenuation
FR3151933B1 (fr) * 2023-08-04 2025-11-28 Safran Nacelles Structure alveolaire pour un panneau acoustique
EP4654182A1 (de) * 2024-05-24 2025-11-26 Airbus SAS Schallabsorbierende struktur mit mindestens einem in mindestens einer zelle positionierten trennwandsystem zur bildung zweier resonatortypen, verfahren zur herstellung einer solchen struktur
EP4685787A1 (de) * 2024-07-25 2026-01-28 Airbus Operations (S.A.S.) Schallabsorbierende struktur mit einem trennwandsystem mit mindestens einem fuss

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Also Published As

Publication number Publication date
DE60105521D1 (de) 2004-10-21
US6536556B2 (en) 2003-03-25
US20020050420A1 (en) 2002-05-02
FR2815900A1 (fr) 2002-05-03
ES2227094T3 (es) 2005-04-01
CA2359924A1 (en) 2002-04-30
EP1201420B1 (de) 2004-09-15
EP1201420A1 (de) 2002-05-02
DE60105521T2 (de) 2005-10-13
CA2359924C (en) 2012-03-06
FR2815900B1 (fr) 2003-07-18

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Legal Events

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