JP2022150610A5 - - Google Patents

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Publication number
JP2022150610A5
JP2022150610A5 JP2021053288A JP2021053288A JP2022150610A5 JP 2022150610 A5 JP2022150610 A5 JP 2022150610A5 JP 2021053288 A JP2021053288 A JP 2021053288A JP 2021053288 A JP2021053288 A JP 2021053288A JP 2022150610 A5 JP2022150610 A5 JP 2022150610A5
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JP
Japan
Prior art keywords
adjusted
prepreg
lamination
laminated structure
laminated
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Pending
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JP2021053288A
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English (en)
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JP2022150610A (ja
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Priority to JP2021053288A priority Critical patent/JP2022150610A/ja
Priority claimed from JP2021053288A external-priority patent/JP2022150610A/ja
Priority to US17/695,669 priority patent/US11745445B2/en
Publication of JP2022150610A publication Critical patent/JP2022150610A/ja
Publication of JP2022150610A5 publication Critical patent/JP2022150610A5/ja
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以上のステップ（Ｓ２００～Ｓ４００）により、異方性複合材積層構造の骨組みモデルと積層構成が完成する。
（Ｓ５００）複合材の積層ステップ
その後、本ステップ（Ｓ５００）では、上記設計した積層構成に基づいて、複数枚のプリプレグを積層することで、主翼５のスキン１１や桁１３の各部位における異方性複合材積層構造の厚みや幅が調整される。かかるプリプレグの積層処理は、ロボット等を用いた自動積層技術を適用することが好ましい。
JP2021053288A 2021-03-26 2021-03-26 異方性複合材積層構造の設計方法 Pending JP2022150610A (ja)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP2021053288A JP2022150610A (ja) 2021-03-26 2021-03-26 異方性複合材積層構造の設計方法
US17/695,669 US11745445B2 (en) 2021-03-26 2022-03-15 Method of designing anisotropic composite laminate structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2021053288A JP2022150610A (ja) 2021-03-26 2021-03-26 異方性複合材積層構造の設計方法

Publications (2)

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JP2022150610A JP2022150610A (ja) 2022-10-07
JP2022150610A5 true JP2022150610A5 (ja) 2024-03-08

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ID=83364137

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JP2021053288A Pending JP2022150610A (ja) 2021-03-26 2021-03-26 異方性複合材積層構造の設計方法

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US (1) US11745445B2 (ja)
JP (1) JP2022150610A (ja)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8973871B2 (en) 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
US10195812B2 (en) * 2015-08-26 2019-02-05 The Boeing Company Ply blending and stacking sequence
US20220152947A1 (en) * 2020-11-18 2022-05-19 The Boeing Company Zonal Lamination for Composite Parts in a Moving Line

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