JP2013502335A5 - - Google Patents

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Publication number
JP2013502335A5
JP2013502335A5 JP2012525574A JP2012525574A JP2013502335A5 JP 2013502335 A5 JP2013502335 A5 JP 2013502335A5 JP 2012525574 A JP2012525574 A JP 2012525574A JP 2012525574 A JP2012525574 A JP 2012525574A JP 2013502335 A5 JP2013502335 A5 JP 2013502335A5
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JP
Japan
Prior art keywords
rod
composite
laminated composite
stringer
panel
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
JP2012525574A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013502335A (ja
JP5628313B2 (ja
Filing date
Publication date
Priority claimed from US12/542,594 external-priority patent/US20110039057A1/en
Application filed filed Critical
Publication of JP2013502335A publication Critical patent/JP2013502335A/ja
Publication of JP2013502335A5 publication Critical patent/JP2013502335A5/ja
Application granted granted Critical
Publication of JP5628313B2 publication Critical patent/JP5628313B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2012525574A 2009-08-17 2010-07-14 積層複合ロッド、その製造方法と複合構造における使用 Active JP5628313B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/542,594 2009-08-17
US12/542,594 US20110039057A1 (en) 2009-08-17 2009-08-17 Laminated composite rod and fabrication method
PCT/US2010/041989 WO2011022137A1 (en) 2009-08-17 2010-07-14 Laminated composite rod, fabrication method and use in a composite structure

Publications (3)

Publication Number Publication Date
JP2013502335A JP2013502335A (ja) 2013-01-24
JP2013502335A5 true JP2013502335A5 (https=) 2013-08-22
JP5628313B2 JP5628313B2 (ja) 2014-11-19

Family

ID=42732291

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012525574A Active JP5628313B2 (ja) 2009-08-17 2010-07-14 積層複合ロッド、その製造方法と複合構造における使用

Country Status (5)

Country Link
US (1) US20110039057A1 (https=)
EP (1) EP2467248A1 (https=)
JP (1) JP5628313B2 (https=)
CN (1) CN102470613A (https=)
WO (1) WO2011022137A1 (https=)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9950480B2 (en) 2012-03-09 2018-04-24 The Boeing Company Composite structure and methods of assembling same
EP2749405B1 (en) * 2012-12-26 2016-03-23 Airbus Operations S.L. Reinforced stringer and method of manufacture thereof
US9566739B2 (en) 2014-02-18 2017-02-14 The Boeing Company Composite filler
US11505301B2 (en) 2019-11-21 2022-11-22 Spirit Aerosystems, Inc. Bulb stiffener with sinusoidal web
EP4210934A1 (en) * 2020-09-14 2023-07-19 Aalborg Universitet Method of manufacturing a fibre reinforced composite component having a reinforced hole
FR3129203B1 (fr) * 2021-11-18 2024-05-24 Safran Nacelles Panneau composite ouvert rigide
US20250083791A1 (en) * 2023-09-07 2025-03-13 Jetzero, Inc. Dry fiber construction of a blended wing body aircraft and method of manufacture
US12559230B2 (en) 2024-01-18 2026-02-24 Jetzero, Inc. Blended wing body aircraft with landing gear aft of a rear spar
US12187425B1 (en) 2024-01-19 2025-01-07 Jetzero, Inc. Aircraft component with structural foam
US12534177B2 (en) 2024-01-19 2026-01-27 Jetzero, Inc. Centerbody pressure vessel with an arched compression surface

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