CN103870633B - A kind of large scale structure rapid modeling system - Google Patents
A kind of large scale structure rapid modeling system Download PDFInfo
- Publication number
- CN103870633B CN103870633B CN201410061416.4A CN201410061416A CN103870633B CN 103870633 B CN103870633 B CN 103870633B CN 201410061416 A CN201410061416 A CN 201410061416A CN 103870633 B CN103870633 B CN 103870633B
- Authority
- CN
- China
- Prior art keywords
- modeling
- module
- overall
- finite element
- model
- 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.)
- Active
Links
Abstract
本发明公开了一种大型结构快速建模系统,包括:基础数据库模块、结构总体建模模块、结构快速输出模块,及主结构建模模块。结构总体建模模块通过骨架模板继承总体开口、接口等参数要求,进行结构总体建模,该模型为可用于强度有限元分析的线框模型;主结构建模模块,该模块根据初步优化的结构参数进行主结构参数设计,并在结构总体建模的骨架基础上完成主结构三维数字样机建模;结构快速输出子模块,根据强度有限元分析及三维标注等要求细化模型,完成大型结构快速建模,基础数据库模块为建模信息支撑。
The invention discloses a large-scale structure fast modeling system, which comprises: a basic database module, a structure overall modeling module, a structure fast output module, and a main structure modeling module. The overall structural modeling module inherits the overall opening, interface and other parameter requirements through the skeleton template to carry out overall structural modeling. This model is a wireframe model that can be used for strength finite element analysis; parameter design of the main structure, and complete the 3D digital prototype modeling of the main structure on the basis of the skeleton of the overall modeling of the structure; the rapid output sub-module of the structure refines the model according to the requirements of strength finite element analysis and 3D annotation, and completes the rapid Modeling, the basic database module supports the modeling information.
Description
技术领域technical field
本发明涉及结构建模技术领域,特别涉及一种应用于大型结构的快速建模系统。The invention relates to the technical field of structural modeling, in particular to a rapid modeling system applied to large structures.
背景技术Background technique
在航天领域结构建模现有技术中,常用的方式是首先进行各个零部件设计,完成零部件设计后再进行总的装配协调工作。这种建模方法优点是各个模型独立,机器配置要求低,人员设计能力要求低,缺点是设计过程中缺乏总体观念,建模不规范,外部条件变化时修改工作量大。在对设计规范化、精细化、快速化要求严苛的航天领域,这种设计方法的应用有一定的局限性。In the existing technology of structural modeling in the aerospace field, the common method is to design each component first, and then carry out the overall assembly coordination after completing the design of the components. The advantage of this modeling method is that each model is independent, the requirements for machine configuration are low, and the requirements for personnel design ability are low. The disadvantage is that the design process lacks an overall concept, the modeling is not standardized, and the modification workload is heavy when external conditions change. The application of this design method has certain limitations in the aerospace field that requires strict design standardization, refinement, and rapidity.
在运载火箭结构系统中,具有独立功能及要求的舱段近20多个,若采用传统的建模设计方法,建模周期长,修改困难,并且各舱段建模不规范,结构匹配性差,严重影响工作效率。In the structural system of the launch vehicle, there are nearly 20 compartments with independent functions and requirements. If the traditional modeling design method is used, the modeling cycle is long and the modification is difficult. Moreover, the modeling of each compartment is not standardized, and the structural matching is poor, which seriously affects work efficiency.
发明内容Contents of the invention
本发明针对现有技术存在的上述不足,提供了一种大型结构快速建模系统。本发明通过以下技术方案实现:The present invention provides a large-scale structure rapid modeling system aiming at the above-mentioned deficiencies in the prior art. The present invention is realized through the following technical solutions:
一种大型结构快速建模系统,用以快速建立大型结构的三维数字模型,大型结构快速建模系统包括:A rapid modeling system for large structures, which is used to quickly establish a three-dimensional digital model of large structures. The rapid modeling system for large structures includes:
基础数据库模块,用以存储若干:骨架模板、有限元分析模板、设计参数优化模板以及三维建模模板;The basic database module is used to store several: skeleton template, finite element analysis template, design parameter optimization template and 3D modeling template;
结构总体建模模块,连接基础数据库模块,包括一总体骨架模型建立子模块,总体骨架模型建立子模块根据输入的总体参数、总体开口和接口信息,以及对接协调信息,从基础数据库模块中调用对应的骨架模板进行建模,生成用于强度有限元分析的线框模型及用于主结构建模的骨架模型;The structural overall modeling module is connected to the basic database module, including an overall skeleton model establishment sub-module. The overall skeleton model establishment sub-module calls the corresponding Modeling of the skeleton template to generate a wireframe model for strength finite element analysis and a skeleton model for main structure modeling;
结构快速输出模块,连接结构总体建模模块以及基础数据库模块,包括有限元分析子模块,有限元分析子模块用以接收线框模型,并从基础数据库模块中调用对应的有限元分析模板,对线框模型进行有限元分析;The structure fast output module connects the structural overall modeling module and the basic database module, including the finite element analysis sub-module, which is used to receive the wireframe model and call the corresponding finite element analysis template from the basic database module. Wireframe model for finite element analysis;
主结构建模模块,连接结构总体建模模块、结构快速输出模块以及基础数据库模块,用以接收骨架模型,并根据有限元分析的结果从基础数据库模块中调用对应的设计参数优化模板、三维建模模板,分别对骨架模型的若干部段进行设计参数优化并进行三维建模,得到三维数字样机;The main structure modeling module connects the overall structure modeling module, the structure fast output module and the basic database module to receive the skeleton model, and calls the corresponding design parameter optimization template and 3D modeling from the basic database module according to the results of the finite element analysis. Die template, respectively optimize the design parameters of several sections of the skeleton model and perform three-dimensional modeling to obtain a three-dimensional digital prototype;
其中,结构快速输出模块接收三维数字样机,并根据有限元分析的结果对三维数字样机进行模型细化,生成供生产所需的二维图纸和三维标注模型。Among them, the fast structure output module receives the 3D digital prototype, refines the model of the 3D digital prototype according to the results of finite element analysis, and generates 2D drawings and 3D marked models for production.
较佳的,主结构建模模块包括设计参数优化子模块,用以对骨架模型的若干部段进行设计参数优化。Preferably, the main structure modeling module includes a design parameter optimization sub-module for optimizing design parameters of several sections of the skeleton model.
较佳的,基础数据库模块采用统一的规范标准存储数据。Preferably, the basic database module stores data using a unified specification standard.
本发明的大型结构快速建模系统与传统的建模方法相比,建模标准化、参数化,出图工作自动化,建模效率提高50%。Compared with the traditional modeling method, the large-scale structure rapid modeling system of the present invention has standardized and parameterized modeling, automatic drawing work, and increased modeling efficiency by 50%.
附图说明Description of drawings
图1所示的是本发明的工作流程示意图。What Fig. 1 shows is the working flow schematic diagram of the present invention.
具体实施方式detailed description
以下将结合本发明的附图,对本发明实施例中的技术方案进行清楚、完整的描述和讨论,显然,这里所描述的仅仅是本发明的一部分实例,并不是全部的实例,基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动的前提下所获得的所有其他实施例,都属于本发明的保护范围。The technical solutions in the embodiments of the present invention will be clearly and completely described and discussed below in conjunction with the accompanying drawings of the present invention. Obviously, what is described here is only a part of the examples of the present invention, not all examples. Based on the present invention All other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
为了便于对本发明实施例的理解,下面将结合附图以具体实施例为例作进一步的解释说明,且各个实施例不构成对本发明实施例的限定。In order to facilitate the understanding of the embodiments of the present invention, specific embodiments will be taken as examples for further explanation below in conjunction with the accompanying drawings, and each embodiment does not constitute a limitation to the embodiments of the present invention.
如图1所示,本发明提供的一种大型结构快速建模系统,包括:基础数据库模块40、结构总体建模模块10、结构快速输出模块30,及主结构建模模块20。As shown in FIG. 1 , a large-scale rapid structural modeling system provided by the present invention includes: a basic database module 40 , an overall structural modeling module 10 , a rapid structural output module 30 , and a main structural modeling module 20 .
在工作中,结构总体建模模块10中的总体骨架模型建立子模块根据输入的总体参数、总体开口和接口信息,以及对接协调信息,从基础数据库模块中调用对应的骨架模板进行建模,生成用于强度有限元分析的线框模型及用于主结构建模的骨架模型;During work, the overall skeleton model building sub-module in the structural overall modeling module 10 calls the corresponding skeleton template from the basic database module to model according to the input overall parameters, overall opening and interface information, and docking coordination information, and generates Wireframe model for strength finite element analysis and skeleton model for main structure modeling;
结构快速输出模块30中的有限元分析子模块,用以接收线框模型,并从基础数据库模块中调用对应的有限元分析模板,对线框模型进行有限元分析,件分析的结果返回至主结构建模模块;The finite element analysis sub-module in the structure rapid output module 30 is used to receive the wireframe model, and call the corresponding finite element analysis template from the basic database module to perform finite element analysis on the wireframe model, and the result of the part analysis is returned to the main Structural modeling module;
主结构建模模块20,接收骨架模型,并根据有限元分析的结果从基础数据库模块中调用对应的设计参数优化模板、三维建模模板,分别对骨架模型的若干部段进行设计参数优化并进行三维建模,得到三维数字样机,并传输至结构快速输出模块;The main structure modeling module 20 receives the skeleton model, and calls the corresponding design parameter optimization template and three-dimensional modeling template from the basic database module according to the results of the finite element analysis, respectively optimizes the design parameters of several sections of the skeleton model and performs 3D modeling, get 3D digital prototype, and transfer to the structure fast output module;
结构快速输出模块30根据有限元分析的结果对三维数字样机进行模型细化,生成供生产所需的二维图纸和三维标注模型。The fast structure output module 30 refines the model of the 3D digital prototype according to the results of the finite element analysis, and generates 2D drawings and 3D marked models for production.
在本发明中,基础数据库模块40为建模提供骨架模板、有限元分析模板、设计参数优化模板、三维建模模板、材料属性、标准零件库等信息支撑,各模块通过调用基础数据库模块中的对应信息完整工作。基础数据库中的信息采用统一的规范标准存储数据,设计参数自动相互关联,设计参数传递唯一准确。各模块可独立输入设计参数完成独立设计功能,各模块可独立调取设计参数、模板进行修改设计。In the present invention, the basic database module 40 provides information support such as skeleton templates, finite element analysis templates, design parameter optimization templates, three-dimensional modeling templates, material properties, and standard parts libraries for modeling. Corresponding information complete work. The information in the basic database adopts a unified standard to store data, the design parameters are automatically correlated with each other, and the design parameter transmission is unique and accurate. Each module can independently input design parameters to complete independent design functions, and each module can independently call design parameters and templates to modify the design.
本发明的大型结构快速建模系统与传统的建模方法相比,建模标准化、参数化,出图工作自动化,建模效率提高50%。Compared with the traditional modeling method, the large-scale structure rapid modeling system of the present invention has standardized and parameterized modeling, automatic drawing work, and increased modeling efficiency by 50%.
以上所述,仅为本发明较佳的具体实施方式,但本发明的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,可轻易想到的变化或替换,都应涵盖在本发明的保护范围之内。因此,本发明的保护范围应该以权利要求的保护范围为准。The above is only a preferred embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any person skilled in the art within the technical scope disclosed in the present invention can easily think of changes or Replacement should be covered within the protection scope of the present invention. Therefore, the protection scope of the present invention should be determined by the protection scope of the claims.
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410061416.4A CN103870633B (en) | 2014-02-24 | 2014-02-24 | A kind of large scale structure rapid modeling system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410061416.4A CN103870633B (en) | 2014-02-24 | 2014-02-24 | A kind of large scale structure rapid modeling system |
Publications (2)
Publication Number | Publication Date |
---|---|
CN103870633A CN103870633A (en) | 2014-06-18 |
CN103870633B true CN103870633B (en) | 2017-06-06 |
Family
ID=50909160
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410061416.4A Active CN103870633B (en) | 2014-02-24 | 2014-02-24 | A kind of large scale structure rapid modeling system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103870633B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106951589B (en) * | 2017-02-16 | 2020-08-14 | 北京宇航系统工程研究所 | Carrier rocket digital prototype design method based on maturity |
CN110705084B (en) * | 2019-09-26 | 2023-05-05 | 内蒙动力机械研究所 | Rapid design software system for composite material shell |
CN112131656A (en) * | 2020-08-21 | 2020-12-25 | 成都飞机工业(集团)有限责任公司 | Optimization method for rapid design of airplane structure scheme |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7483818B2 (en) * | 2001-09-18 | 2009-01-27 | Fujitsu Nagano Systems Engineering Limited | Structural analysis program, a structural analysis method, a structural analysis apparatus, and a production process of a semiconductor integrated circuit |
CN102012958A (en) * | 2010-12-29 | 2011-04-13 | 奇瑞汽车股份有限公司 | Method for designing automobile body structure layout |
CN102184285A (en) * | 2011-05-03 | 2011-09-14 | 三一集团有限公司 | Digital prototyping design integrated development method and system |
-
2014
- 2014-02-24 CN CN201410061416.4A patent/CN103870633B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7483818B2 (en) * | 2001-09-18 | 2009-01-27 | Fujitsu Nagano Systems Engineering Limited | Structural analysis program, a structural analysis method, a structural analysis apparatus, and a production process of a semiconductor integrated circuit |
CN102012958A (en) * | 2010-12-29 | 2011-04-13 | 奇瑞汽车股份有限公司 | Method for designing automobile body structure layout |
CN102184285A (en) * | 2011-05-03 | 2011-09-14 | 三一集团有限公司 | Digital prototyping design integrated development method and system |
Also Published As
Publication number | Publication date |
---|---|
CN103870633A (en) | 2014-06-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104123412B (en) | A kind of curtain wall collision checking method by BIM technology | |
CN107066676A (en) | A kind of finite element automation modeling method based on satellite plate and shell structure | |
CN104239603B (en) | A kind of three-dimensional process model generating method combined based on positive sequence backward | |
CN107169214A (en) | A kind of BUILDINGS MODELS design method | |
CN104376152B (en) | A kind of parametric modeling and mask method | |
CN106354924A (en) | FMI-based equipment cooperation simulation system and construction method | |
CN105242538A (en) | Layer-based part multi-processing procedure MBD model and realization method thereof | |
CN112307396B (en) | Platform architecture based on multi-engine data modeling calculation analysis and processing method thereof | |
CN103870633B (en) | A kind of large scale structure rapid modeling system | |
CN104239653A (en) | Casting three-dimensional process designing method | |
CN103324541B (en) | The self-propagating method of data between software | |
CN104992023A (en) | Aircraft parametric design method based on state type function | |
CN104123411B (en) | A kind of succinct derivation method of powertrain system of automobile rotary inertia synthesis | |
CN105957138B (en) | A kind of furniture item three-dimensional modeling method and system based on assembly | |
CN105488240A (en) | Rapid generating method for three-dimensional model of integral wing rib | |
CN105867308B (en) | A kind of sheet metal component rapid development system based on precision controlling | |
CN103514331B (en) | A kind of method from Simulink model conversion to uml model | |
CN103902750A (en) | Design method for achieving parameterized three-dimensional modeling and two-dimensional diagram conversion of parts similar to main part | |
CN113642079B (en) | A factory design method based on 3D technology | |
CN105787999A (en) | Rocket total frame curved surface erecting system and method | |
CN105956346A (en) | Aluminum alloy template design system and aluminum alloy template design method | |
CN103679811A (en) | Multiple curved surface materialized modeling method | |
CN106354913A (en) | Parametric design platform for helical gear drive system and application method thereof | |
CN104992034A (en) | Rapid generation method of air duct for automobile painting workshop | |
CN104090994A (en) | Model converting method, testing method, converting system and testing system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant | ||
TR01 | Transfer of patent right |
Effective date of registration: 20250707 Address after: 201108 Shanghai City Minhang District Chundelu Road 395.NO Patentee after: China Aerospace Science and Technology Corporation Commercial Rocket Co.,Ltd. Country or region after: China Patentee after: AEROSPACE SYSTEM ENGINEERING SHANGHAI Address before: 201108 Minhang District, Shanghai Jin Road, No. 3805 Patentee before: AEROSPACE SYSTEM ENGINEERING SHANGHAI Country or region before: China |