JP2013182614A5 - - Google Patents
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- JP2013182614A5 JP2013182614A5 JP2013001461A JP2013001461A JP2013182614A5 JP 2013182614 A5 JP2013182614 A5 JP 2013182614A5 JP 2013001461 A JP2013001461 A JP 2013001461A JP 2013001461 A JP2013001461 A JP 2013001461A JP 2013182614 A5 JP2013182614 A5 JP 2013182614A5
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- JP
- Japan
- Prior art keywords
- analysis
- structural component
- template
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- server
- 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.)
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- 238000005457 optimization Methods 0.000 claims 7
- 230000003068 static effect Effects 0.000 claims 7
- 238000000034 method Methods 0.000 claims 6
- 238000012986 modification Methods 0.000 claims 2
- 230000004048 modification Effects 0.000 claims 2
- 230000000712 assembly Effects 0.000 claims 1
- 238000000429 assembly Methods 0.000 claims 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/409,771 US8949087B2 (en) | 2012-03-01 | 2012-03-01 | System and method for structural analysis |
| US13/409,771 | 2012-03-01 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2013182614A JP2013182614A (ja) | 2013-09-12 |
| JP2013182614A5 true JP2013182614A5 (enExample) | 2016-03-03 |
| JP6104607B2 JP6104607B2 (ja) | 2017-03-29 |
Family
ID=47900611
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013001461A Active JP6104607B2 (ja) | 2012-03-01 | 2013-01-09 | 構造解析のためのシステム及び方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8949087B2 (enExample) |
| EP (1) | EP2634711A3 (enExample) |
| JP (1) | JP6104607B2 (enExample) |
| CN (1) | CN103294843B (enExample) |
| CA (1) | CA2801664C (enExample) |
Families Citing this family (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8843326B1 (en) | 2011-07-22 | 2014-09-23 | The Boeing Company | System, method and computer-readable storage medium for defining a load envelope that envelopes a plurality of load cases |
| US9676019B2 (en) * | 2013-06-13 | 2017-06-13 | The Boeing Company | Determining part orientation for incremental sheet forming |
| US9524356B2 (en) * | 2013-10-16 | 2016-12-20 | General Electric Company | System and methods of generating a computer model of composite component |
| US10140388B1 (en) * | 2014-11-16 | 2018-11-27 | The Boeing Company | System and method for designing composite laminates using lamination parameters |
| WO2017027598A1 (en) * | 2015-08-11 | 2017-02-16 | Sabic Global Technologies B.V. | Multiple ply layered composite having low areal weight |
| EP3371486B1 (en) | 2015-11-07 | 2023-04-19 | Eaton Intelligent Power Limited | Lightweight torque transmission gear |
| US10275564B2 (en) * | 2016-06-17 | 2019-04-30 | The Boeing Company | System for analysis of a repair for a structure |
| CN107844628B (zh) * | 2017-09-26 | 2021-10-08 | 上海电力学院 | 一种大型海上风电场集电系统冗余度优化方法 |
| US20220214244A1 (en) * | 2017-10-18 | 2022-07-07 | Sikorsky Aircraft Corporation | Systems and methods for assessing structural health |
| US20200302025A1 (en) * | 2019-03-18 | 2020-09-24 | The Boeing Company | Automated Method for Support Material Placement in Additive Manufacturing for Improved Finish Machining Performance |
| CN110069833B (zh) * | 2019-03-29 | 2022-06-21 | 汕头大学 | 一种考虑不确定因素的接口刚度优化设计方法 |
| CN110175382B (zh) * | 2019-05-16 | 2022-10-14 | 国网山西省电力公司检修分公司 | 一种基于ansys的盆式绝缘子缺陷模态分析方法 |
| CN111144049B (zh) * | 2019-12-24 | 2023-06-23 | 中国航空工业集团公司西安飞机设计研究所 | 一种复合材料开孔翼梁安全裕度计算方法 |
| US12223238B2 (en) | 2020-06-26 | 2025-02-11 | Autodesk, Inc. | Generative design shape optimization with controlled convergence for computer aided design and manufacturing |
| US11675333B2 (en) | 2020-06-26 | 2023-06-13 | Autodesk, Inc. | Generative design shape optimization with singularities and disconnection prevention for computer aided design and manufacturing |
| US11321508B2 (en) * | 2020-06-26 | 2022-05-03 | Autodesk, Inc. | Generative design shape optimization with damage prevention over loading cycles for computer aided design and manufacturing |
| US11663379B2 (en) | 2020-06-26 | 2023-05-30 | Autodesk, Inc. | Generative design shape optimization using build material strength model for computer aided design and manufacturing |
| CN112710568B (zh) * | 2020-12-17 | 2024-05-28 | 哈尔滨汽轮机厂有限责任公司 | 一种汽轮机定中心梁强度检测方法 |
| US20220284148A1 (en) * | 2021-03-05 | 2022-09-08 | The Boeing Company | System and method of managing a design lifecycle of a structural part |
| EP4060547A1 (en) * | 2021-03-17 | 2022-09-21 | Subaru Corporation | Composite laminate designing method and aircraft |
| CN113158597B (zh) * | 2021-04-25 | 2022-08-19 | 中国电建集团贵阳勘测设计研究院有限公司 | 一种基于catia计算的水闸应力稳定分析方法 |
| CN121009724A (zh) * | 2025-10-28 | 2025-11-25 | 南通鋆鼎精密科技股份有限公司 | 一种海上风电发电机机舱结构件智能应力分析与优化系统 |
Family Cites Families (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5006990A (en) * | 1987-04-10 | 1991-04-09 | The Boeing Company | Method and apparatus for the design and construction of composite parts |
| US5071492A (en) * | 1989-12-19 | 1991-12-10 | Parker Research Inc. | Method for reducing the fatigue crack growth rate of cracks in the aluminum alloy fuselage skin of an aircraft structure |
| US7010472B1 (en) * | 1997-05-12 | 2006-03-07 | Mcdonnell Douglas Corporation | Knowledge driven composite design optimization process and system therefor |
| US5984511A (en) * | 1997-05-12 | 1999-11-16 | Mcdonnell Douglas Corporation | Knowledge driven composite design optimization process and system therefor |
| US6125333A (en) | 1997-11-06 | 2000-09-26 | Northrop Grumman Corporation | Building block approach for fatigue spectra generation |
| JP2001125933A (ja) * | 1999-10-25 | 2001-05-11 | Hitachi Ltd | 設備信頼性設計支援装置 |
| US20030226935A1 (en) * | 2001-11-02 | 2003-12-11 | Garratt Matthew D. | Structural members having improved resistance to fatigue crack growth |
| US6799463B2 (en) * | 2001-11-02 | 2004-10-05 | The Boeing Company | Method and system for automated fatigue and structural analysis of an element |
| JP2003150650A (ja) * | 2001-11-13 | 2003-05-23 | Hitachi Ltd | 解析作業支援装置及び解析作業支援機能を実現するためのプログラム |
| US6813749B2 (en) * | 2002-02-12 | 2004-11-02 | The Boeing Company | Method, system and computer program product for multidisciplinary design analysis of structural components |
| US7640529B2 (en) * | 2002-07-30 | 2009-12-29 | Photronics, Inc. | User-friendly rule-based system and method for automatically generating photomask orders |
| JP2004094465A (ja) | 2002-08-30 | 2004-03-25 | Fujitsu Ltd | 解析支援装置 |
| JP2004314885A (ja) * | 2003-04-18 | 2004-11-11 | Nippon Sheet Glass Co Ltd | 開閉ガラスの製造方法および開閉ガラス |
| US20040250236A1 (en) * | 2003-04-30 | 2004-12-09 | O'malley Austin | Establishing and maintaining a relationship between a three-dimensional model and related data |
| US7003362B2 (en) * | 2004-05-11 | 2006-02-21 | Taiwan Semiconductor Manufacturing Company, Ltd. | System and method for customized tape-out requests for integrated circuit manufacturing |
| US7912681B2 (en) * | 2004-10-15 | 2011-03-22 | Textron Innovations Inc. | Method for designing a flight vehicle |
| US7467070B2 (en) | 2004-10-26 | 2008-12-16 | Meyer Eric S | Methods and systems for modeling stress intensity solutions for integrally stiffened panels |
| US7690837B2 (en) * | 2006-03-07 | 2010-04-06 | The Boeing Company | Method of analysis of effects of cargo fire on primary aircraft structure temperatures |
| US7613527B2 (en) * | 2006-03-16 | 2009-11-03 | 3M Innovative Properties Company | Orthodontic prescription form, templates, and toolbar for digital orthodontics |
| US7889840B2 (en) * | 2007-01-10 | 2011-02-15 | The United States Of America As Represented By The Secretary Of The Navy | System and method for predicting material fatigue and damage |
| JP2009003549A (ja) * | 2007-06-19 | 2009-01-08 | Japan Lucida Co Ltd | データ管理装置およびデータ管理方法、データ管理プログラム、データ管理プログラム記憶媒体 |
| US7809454B2 (en) * | 2007-09-17 | 2010-10-05 | The Boeing Company | Method and apparatus for simulating composite panel manufacturing |
| GB0723224D0 (en) * | 2007-11-27 | 2008-01-09 | Fujitsu Ltd | A multi-level gris embedding process with uniform and non-uniform grid refinement for multigurid-fdtd electromagnetic solver |
| US8401827B2 (en) * | 2008-04-14 | 2013-03-19 | Daa Draexlmaier Automotive Of America Llc | Processing device and method for structure data representing a physical structure |
| US8108058B2 (en) * | 2009-02-09 | 2012-01-31 | The Boeing Company | Method of analyzing composite structures |
| US8831913B2 (en) * | 2009-06-10 | 2014-09-09 | Airbus Operations Limited | Method of design optimisation |
| CN101853320B (zh) * | 2010-05-17 | 2011-10-26 | 北京航空航天大学 | 一种适用于飞机结构腐蚀损伤的模糊综合评判方法 |
| CN101986318A (zh) * | 2010-11-26 | 2011-03-16 | 南京航空航天大学 | 飞行控制系统概念样机设计方法 |
-
2012
- 2012-03-01 US US13/409,771 patent/US8949087B2/en active Active
-
2013
- 2013-01-08 CA CA2801664A patent/CA2801664C/en active Active
- 2013-01-09 JP JP2013001461A patent/JP6104607B2/ja active Active
- 2013-02-07 CN CN201310049373.3A patent/CN103294843B/zh active Active
- 2013-03-01 EP EP13157412.1A patent/EP2634711A3/en not_active Ceased
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