CN105511404B - 一种具有复杂特征的双曲率长桁展开加工方法 - Google Patents
一种具有复杂特征的双曲率长桁展开加工方法 Download PDFInfo
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- CN105511404B CN105511404B CN201510864653.9A CN201510864653A CN105511404B CN 105511404 B CN105511404 B CN 105511404B CN 201510864653 A CN201510864653 A CN 201510864653A CN 105511404 B CN105511404 B CN 105511404B
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/18—Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form
- G05B19/4097—Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by using design data to control NC machines, e.g. CAD/CAM
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/30—Nc systems
- G05B2219/31—From computer integrated manufacturing till monitoring
- G05B2219/31055—Interpretation of assembly design data
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CN201510864653.9A CN105511404B (zh) | 2015-11-30 | 2015-11-30 | 一种具有复杂特征的双曲率长桁展开加工方法 |
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CN201510864653.9A CN105511404B (zh) | 2015-11-30 | 2015-11-30 | 一种具有复杂特征的双曲率长桁展开加工方法 |
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CN105511404A CN105511404A (zh) | 2016-04-20 |
CN105511404B true CN105511404B (zh) | 2017-12-19 |
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Families Citing this family (1)
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CN108555360B (zh) * | 2018-06-27 | 2019-10-18 | 西安飞机工业(集团)有限责任公司 | 一种不等厚蒙皮类零件铣切成形中性层展开方法 |
Citations (5)
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JP2010531776A (ja) * | 2007-06-29 | 2010-09-30 | エアバス・ユ―ケ―・リミテッド | 長尺複合構造メンバおよびその改良 |
EP2439137A2 (en) * | 2007-06-29 | 2012-04-11 | Airbus Operations Limited | Composite panel stiffener |
CN102842147A (zh) * | 2012-07-10 | 2012-12-26 | 西北工业大学 | 一种三维整体壁板展开建模方法 |
CN103197608A (zh) * | 2013-02-27 | 2013-07-10 | 中航飞机股份有限公司西安飞机分公司 | 一种弯扭长桁数模的展开重构方法 |
CN104890854A (zh) * | 2015-04-02 | 2015-09-09 | 中航飞机股份有限公司西安飞机分公司 | 一种弯扭长桁的展开板坯 |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
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US9475569B2 (en) * | 2013-10-29 | 2016-10-25 | Gulfstream Aerospace Corporation | Methods for manufacturing an i-stringer of an aircraft and devices for use in such methods |
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- 2015-11-30 CN CN201510864653.9A patent/CN105511404B/zh active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010531776A (ja) * | 2007-06-29 | 2010-09-30 | エアバス・ユ―ケ―・リミテッド | 長尺複合構造メンバおよびその改良 |
EP2439137A2 (en) * | 2007-06-29 | 2012-04-11 | Airbus Operations Limited | Composite panel stiffener |
CN102842147A (zh) * | 2012-07-10 | 2012-12-26 | 西北工业大学 | 一种三维整体壁板展开建模方法 |
CN103197608A (zh) * | 2013-02-27 | 2013-07-10 | 中航飞机股份有限公司西安飞机分公司 | 一种弯扭长桁数模的展开重构方法 |
CN104890854A (zh) * | 2015-04-02 | 2015-09-09 | 中航飞机股份有限公司西安飞机分公司 | 一种弯扭长桁的展开板坯 |
Non-Patent Citations (6)
Title |
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A key characteristics-based model for quality assurance in supply chain;Yang F;《International Conference on Industrial Engineering and Engineering Management.IEEE》;20111010;第1428-1432页 * |
Application of computer aided tools and methods for unmanned cargo aircraft design;Czyba R et al;《International Conference on Methods and MODELS in Automation and Robotics.IEEE》;20151001;第1068-1073页 * |
Optimal design of aircraft wing structures: a computer aided design method;Ampofo J et al;《 Automation Congress, 2002 Proceedings of the, Bi World.IEEE》;20021210;第471-480页 * |
基于知识的飞机长桁类结构件快速设计研究;裴蕾;《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》;20130415(第04期);C031-12:P6-P25 * |
飞机桁条快速设计技术研究;韩志仁;《沈阳航空航天大学学报》;20110831;第28卷(第04期);第1-4页 * |
飞机长桁类零件工艺板坯数模的展开设计;张耀平;《航空制造技术》;20150815(第15期);第33-35页 * |
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Address after: No. 710089 in Shaanxi province Xi'an city Yanliang District West Avenue Patentee after: AVIC Xi'an Aircraft Industry Group Co.,Ltd. Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee before: AVIC AIRCRAFT Corp. |
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Effective date of registration: 20210610 Address after: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee after: AVIC AIRCRAFT Corp. Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee before: XI'AN AIRCRAFT BRANCH OF XI'AN AIRCRAFT INTERNATIONAL Corp. |