JP2015534619A5 - - Google Patents

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Publication number
JP2015534619A5
JP2015534619A5 JP2015531945A JP2015531945A JP2015534619A5 JP 2015534619 A5 JP2015534619 A5 JP 2015534619A5 JP 2015531945 A JP2015531945 A JP 2015531945A JP 2015531945 A JP2015531945 A JP 2015531945A JP 2015534619 A5 JP2015534619 A5 JP 2015534619A5
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JP
Japan
Prior art keywords
air flow
wall panel
inner diameter
sandwich structure
honeycomb
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
JP2015531945A
Other languages
English (en)
Japanese (ja)
Other versions
JP6407866B2 (ja
JP2015534619A (ja
Filing date
Publication date
Priority claimed from US13/620,679 external-priority patent/US9168716B2/en
Application filed filed Critical
Publication of JP2015534619A publication Critical patent/JP2015534619A/ja
Publication of JP2015534619A5 publication Critical patent/JP2015534619A5/ja
Application granted granted Critical
Publication of JP6407866B2 publication Critical patent/JP6407866B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2015531945A 2012-09-14 2013-08-26 小さい曲げ半径を有する金属製サンドイッチ構造体 Active JP6407866B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/620,679 2012-09-14
US13/620,679 US9168716B2 (en) 2012-09-14 2012-09-14 Metallic sandwich structure having small bend radius
PCT/US2013/056590 WO2014042857A2 (en) 2012-09-14 2013-08-26 Metallic sandwich structure having small bend radius

Publications (3)

Publication Number Publication Date
JP2015534619A JP2015534619A (ja) 2015-12-03
JP2015534619A5 true JP2015534619A5 (enExample) 2016-10-13
JP6407866B2 JP6407866B2 (ja) 2018-10-17

Family

ID=49162228

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015531945A Active JP6407866B2 (ja) 2012-09-14 2013-08-26 小さい曲げ半径を有する金属製サンドイッチ構造体

Country Status (5)

Country Link
US (1) US9168716B2 (enExample)
EP (1) EP2895392B1 (enExample)
JP (1) JP6407866B2 (enExample)
CN (1) CN104520192B (enExample)
WO (1) WO2014042857A2 (enExample)

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FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2982588B1 (fr) * 2011-11-10 2013-11-22 Aircelle Sa Panneau composite a ecope de prelevement integree
US20150041059A1 (en) * 2013-03-18 2015-02-12 Rohr, Inc. Inner fixed structure with attached corner fitting
US10184398B2 (en) * 2013-10-17 2019-01-22 Rohr, Inc. Acoustic structural panel with slanted core
US9850850B2 (en) * 2013-10-23 2017-12-26 Rohr, Inc. Acoustically treated thrust reverser track beam
US20150267644A1 (en) * 2014-03-19 2015-09-24 The Boeing Company Integrated Primary Nozzle
US9541029B2 (en) * 2014-05-12 2017-01-10 Rohr, Inc. Hybrid IFS with metallic aft section
JP2018513406A (ja) * 2015-04-10 2018-05-24 エムアールエイ・システムズ・エルエルシー 音響ライナおよび音響ライナを組み立てる方法
US9607598B2 (en) 2015-08-17 2017-03-28 The Boeing Company Acoustic sandwich panel and method
US10507931B2 (en) 2015-10-19 2019-12-17 Rohr, Inc. Panel and insert for corner radii
FR3044960A1 (fr) * 2015-12-15 2017-06-16 Aircelle Sa Panneau pour nacelle de turboreacteur d’aeronef, comportant une protection thermique et une protection anti-feu
US10161357B2 (en) 2016-06-17 2018-12-25 Rohr, Inc. Acoustically treated thrust reverser track beam
US10738738B2 (en) * 2016-06-17 2020-08-11 Rohr, Inc. Nacelle with bifurcation extension and integral structural reinforcement
US10569495B2 (en) * 2017-05-08 2020-02-25 The Boeing Company Composite structure assembly having a conformable core
US20190024988A1 (en) * 2017-07-18 2019-01-24 General Electric Company Header assembly for a heat exchanger
US11125157B2 (en) 2017-09-22 2021-09-21 The Boeing Company Advanced inlet design
US10974813B2 (en) * 2018-01-08 2021-04-13 General Electric Company Engine nacelle for an aircraft
GB2570913A (en) * 2018-02-09 2019-08-14 Safran Nacelles Ltd Inner fixed structure
GB2583751B (en) * 2019-05-09 2022-02-02 Safran Nacelles Ltd Acoustic panel
US20200392899A1 (en) * 2019-06-14 2020-12-17 Pratt & Whitney Canada Corp. Acoustic treatment for aircraft engine
FR3100570B1 (fr) * 2019-09-09 2022-06-03 Safran Nacelles Panneau structural et/ou acoustique comprenant une bride de fermeture en U orientée vers l’intérieur du panneau, et procédé de fabrication d’un tel panneau
GB2588204B (en) 2019-10-15 2022-09-14 Safran Nacelles Ltd Aircraft nacelle inlet
CN113123875B (zh) * 2019-12-31 2022-07-08 中国航发商用航空发动机有限责任公司 航空发动机吸声装置及航空发动机
US11535390B2 (en) 2020-02-28 2022-12-27 Rohr, Inc. Structural panel with integrated coupler
FR3113170A1 (fr) * 2020-07-31 2022-02-04 Airbus Operations Matériau acoustique en bande à bride intégrée, et paroi interne d’une entrée d’air d’aéronef réalisée avec ce matériau
BR102022003769A2 (pt) 2021-05-04 2022-11-16 The Boeing Company Estrutura de entrada de nacele de um conjunto de motor
US11780021B2 (en) * 2021-09-10 2023-10-10 Rohr, Inc. Component with structured panel(s) and methods for forming the component
FR3128206A1 (fr) * 2021-10-14 2023-04-21 Safran Nacelles Ensemble arrière pour nacelle de turboréacteur
CN116931507B (zh) * 2023-09-18 2024-01-12 成都飞机工业（集团）有限责任公司 一种群孔穿孔控制方法、装置、存储介质及电子设备

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US6129311A (en) * 1997-07-30 2000-10-10 The Boeing Company Engine nacelle outer cowl panel with integral track fairings
US6098926A (en) * 1998-08-06 2000-08-08 Lockheed Martin Corporation Composite fairing with integral damping and internal helmholz resonators
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US7370467B2 (en) * 2003-07-29 2008-05-13 Pratt & Whitney Canada Corp. Turbofan case and method of making
JP5210505B2 (ja) * 2006-07-12 2013-06-12 横浜ゴム株式会社 防音特性を備えたハニカムサンドイッチパネル
FR2909974B1 (fr) * 2006-12-13 2009-02-06 Aircelle Sa Nacelle pour turboreacteur double flux
FR2915522A1 (fr) * 2007-04-30 2008-10-31 Airbus France Sas Panneau acoustique a caracteristique acoustique variable
FR2917714B1 (fr) 2007-06-25 2009-11-27 Airbus France Turboreacteur pour aeronef
FR2922152B1 (fr) * 2007-10-16 2009-11-20 Aircelle Sa Structure a ame alveolaire pour panneau acoustique
US8152461B2 (en) * 2008-11-19 2012-04-10 Mra Systems, Inc. Integrated inlet design
FR2965859B1 (fr) * 2010-10-07 2012-11-02 Snecma Dispositif de traitement acoustique du bruit emis par un turboreacteur

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