JP2019194066A5 - - Google Patents

Download PDF

Info

Publication number
JP2019194066A5
JP2019194066A5 JP2019029006A JP2019029006A JP2019194066A5 JP 2019194066 A5 JP2019194066 A5 JP 2019194066A5 JP 2019029006 A JP2019029006 A JP 2019029006A JP 2019029006 A JP2019029006 A JP 2019029006A JP 2019194066 A5 JP2019194066 A5 JP 2019194066A5
Authority
JP
Japan
Prior art keywords
degrees
stringer
plies
segment
reinforcing material
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
JP2019029006A
Other languages
English (en)
Japanese (ja)
Other versions
JP2019194066A (ja
JP7336202B2 (ja
Filing date
Publication date
Priority claimed from US15/907,224 external-priority patent/US10669005B2/en
Application filed filed Critical
Publication of JP2019194066A publication Critical patent/JP2019194066A/ja
Publication of JP2019194066A5 publication Critical patent/JP2019194066A5/ja
Application granted granted Critical
Publication of JP7336202B2 publication Critical patent/JP7336202B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2019029006A 2018-02-27 2019-02-21 中実積層ストリンガ Active JP7336202B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/907,224 2018-02-27
US15/907,224 US10669005B2 (en) 2018-02-27 2018-02-27 Solid laminate stringer

Publications (3)

Publication Number Publication Date
JP2019194066A JP2019194066A (ja) 2019-11-07
JP2019194066A5 true JP2019194066A5 (enExample) 2022-03-02
JP7336202B2 JP7336202B2 (ja) 2023-08-31

Family

ID=65657245

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2019029006A Active JP7336202B2 (ja) 2018-02-27 2019-02-21 中実積層ストリンガ

Country Status (4)

Country Link
US (2) US10669005B2 (enExample)
EP (1) EP3549755B1 (enExample)
JP (1) JP7336202B2 (enExample)
CN (1) CN110194258B (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10669005B2 (en) 2018-02-27 2020-06-02 The Boeing Company Solid laminate stringer
US10745104B2 (en) * 2018-03-02 2020-08-18 The Boeing Company Stringer transition through a common base charge
US11318705B2 (en) * 2019-08-26 2022-05-03 The Boeing Company Ply stackings for solid laminate stiffened panel
US11628922B2 (en) 2020-02-18 2023-04-18 The Boeing Company Composite plank support for stringer panel
US12220890B2 (en) * 2020-02-18 2025-02-11 The Boeing Company Methods for fabricating solid laminate stringers on a composite panel
IT202000018136A1 (it) * 2020-07-27 2022-01-27 Leonardo Spa Procedimento per la fabbricazione di un componente strutturale in materiale composito irrigidito con almeno un corrente
IT202000018139A1 (it) * 2020-07-27 2022-01-27 Leonardo Spa Procedimento per la fabbricazione di un componente strutturale in materiale composito irrigidito con almeno un corrente
GB2612957A (en) * 2021-11-08 2023-05-24 Airbus Operations Ltd Stiffener with core and shell

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4331723A (en) * 1980-11-05 1982-05-25 The Boeing Company Advanced composite
US7861969B2 (en) 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
US8042315B2 (en) 2007-09-14 2011-10-25 Spectrum Aeronautical, Llc Reinforced composite panel
US8636252B2 (en) * 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same
US8795567B2 (en) * 2010-09-23 2014-08-05 The Boeing Company Method for fabricating highly contoured composite stiffeners with reduced wrinkling
GB201101435D0 (en) * 2011-01-27 2011-03-16 Airbus Uk Ltd Stringer for an aircraft wing and method of forming thereof
ES2619478T3 (es) * 2012-10-31 2017-06-26 Airbus Operations S.L. Larguerillo
US9278748B2 (en) 2012-12-28 2016-03-08 Embraer S.A. Processes to fabricate composite tubular-reinforced panels integrating skin and stringers and the panels thereby fabricated
CA2911447C (en) 2013-08-09 2020-03-10 The Boeing Company Stiffened composite panels and method of their manufacture
US10144203B2 (en) * 2013-10-03 2018-12-04 The Boeing Company Pre-formed thermoplastic filler for thermoset structure
US10040537B2 (en) * 2015-01-15 2018-08-07 The Boeing Company Laminate composite wing structures
US10926435B2 (en) * 2017-05-03 2021-02-23 The Boeing Company Foam mandrel assembly
US10669005B2 (en) 2018-02-27 2020-06-02 The Boeing Company Solid laminate stringer

Similar Documents

Publication Publication Date Title
JP2019194066A5 (enExample)
CN110194258B (zh) 实心层压板桁条
US10046525B2 (en) Advanced variable radius laminated composite radius filler
CN101678890B (zh) 成形的复合长桁及其制造方法
RU2469853C2 (ru) Шпангоут из композитного материала и фюзеляж летательного аппарата с таким шпангоутом
CN100410144C (zh) 直升机叶轮整流装置以及制造该装置的方法和设备
JP2016097945A (ja) タイヤ
EP3134257B1 (en) Panel made of laminates and method of manufacturing the same
CN102407937A (zh) 制造具有减小褶皱的高度轮廓变化的复合加强件的方法和设备
JP7629060B2 (ja) 複合構造体のスプライス及びその方法
WO2016084535A1 (ja) タイヤ
CN102837433B (zh) 非平面复合材料部件的叠铺方法
JP6188786B2 (ja) 複合材料中のヒンジ及びその製造方法
US11718063B2 (en) Splice joint in laminate composite structure
JP2016112787A (ja) 複合構造体及び複合構造体の成形方法
JP2019042934A5 (enExample)
JP2011240925A5 (enExample)
JP2011240925A (ja) 漸進的な剛性を有する複合構造部材
JPS58108896A (ja) スピ−カの膜及びその製法
JP7681953B2 (ja) 中実積層補強パネルのためのプライの積み重ね
CN204507244U (zh) 飞行器复合材料部件和飞行器
EP3323602A1 (en) Method and tool system for manufacturing a multilayer fibre structure
JP6408070B2 (ja) タイヤ
JPWO2023073745A5 (enExample)
JP2019202752A5 (enExample)