Iurii Vorobiov, Kateryna Maiorova, Iryna Voronko, Oleksandr Skyba, Oleh Komisarov
{"title":"利用链式法计算分析标准施工阶段尺寸精度的数学模型创建","authors":"Iurii Vorobiov, Kateryna Maiorova, Iryna Voronko, Oleksandr Skyba, Oleh Komisarov","doi":"10.15587/2706-5448.2024.297732","DOIUrl":null,"url":null,"abstract":"The object of research is the process of forming a mathematical model (MM) for calculating accuracy at the stages of construction an analytical standard (AS) using the chain method, the application of which is shown on the example of an aviation object (AO). The analysis of the investigated AO, namely the helicopter stabilizer, was carried out using modern 3D scanners and the creation of its analytical portrait (AP). The problem is to create the most similar AP and compare it with AS, taking into account the results of the calculations. The following results were obtained: the AS was built and the AP of the stabilizer geometry was created, a comparative analysis of the AP and AS was carried out, and the results of the accuracy of the object geometry calculations were obtained. Aerodynamic calculations of stabilizer characteristics were also carried out, analysis of standardized aerodynamic profiles was carried out taking into account the accepted limitations for forming the stabilizer AS. The scientific and practical novelty of the obtained results is as follows: the created MM for calculating the accuracy of the dimensions of the unit contour using the chain method made it possible to estimate the tying errors that occur when using the loft-template method. This made it possible to choose equipment and software for construction the AS stabilizer. The selection of improved values of the object's aerodynamic characteristics made it possible to build an AS based on the standardized NACA 0012 profile. This can be used as an information basis for the organization of small-scale production of the object under study. That is, in general, the process of reverse engineering made it possible to conduct a detailed analysis of sections, aerodynamic characteristics and improve them for the future improved profile. This design approach provides wider opportunities, eliminates intermediate links and maintains high accuracy of object parameters during its manufacture, which is one of the main requirements in aircraft construction.","PeriodicalId":22480,"journal":{"name":"Technology audit and production reserves","volume":"238 ","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-02-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Mathematical models creation for calculating dimensional accuracy at the construction stages of an analytical standard using the chain method\",\"authors\":\"Iurii Vorobiov, Kateryna Maiorova, Iryna Voronko, Oleksandr Skyba, Oleh Komisarov\",\"doi\":\"10.15587/2706-5448.2024.297732\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The object of research is the process of forming a mathematical model (MM) for calculating accuracy at the stages of construction an analytical standard (AS) using the chain method, the application of which is shown on the example of an aviation object (AO). The analysis of the investigated AO, namely the helicopter stabilizer, was carried out using modern 3D scanners and the creation of its analytical portrait (AP). The problem is to create the most similar AP and compare it with AS, taking into account the results of the calculations. The following results were obtained: the AS was built and the AP of the stabilizer geometry was created, a comparative analysis of the AP and AS was carried out, and the results of the accuracy of the object geometry calculations were obtained. Aerodynamic calculations of stabilizer characteristics were also carried out, analysis of standardized aerodynamic profiles was carried out taking into account the accepted limitations for forming the stabilizer AS. The scientific and practical novelty of the obtained results is as follows: the created MM for calculating the accuracy of the dimensions of the unit contour using the chain method made it possible to estimate the tying errors that occur when using the loft-template method. This made it possible to choose equipment and software for construction the AS stabilizer. The selection of improved values of the object's aerodynamic characteristics made it possible to build an AS based on the standardized NACA 0012 profile. This can be used as an information basis for the organization of small-scale production of the object under study. That is, in general, the process of reverse engineering made it possible to conduct a detailed analysis of sections, aerodynamic characteristics and improve them for the future improved profile. 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引用次数: 0
摘要
研究对象是利用链式方法形成数学模型 (MM),用于计算分析标准 (AS) 各施工阶段的精度,并以航空物体 (AO) 为例进行说明。使用现代 3D 扫描仪对所研究的航空物体(即直升机稳定器)进行了分析,并创建了其分析肖像 (AP)。问题是创建最相似的 AP,并将其与 AS 进行比较,同时考虑到计算结果。结果如下:建立了 AS 并创建了稳定器几何的 AP,对 AP 和 AS 进行了比较分析,并获得了物体几何计算的准确性结果。此外还进行了稳定器特性的空气动力学计算,在考虑到稳定器 AS 的公认形成限制的情况下,对标准化空气动力学剖面进行了分析。所获成果在科学和实用方面的新颖性如下:利用链式方法计算单元轮廓尺寸精度的 MM 使我们能够估算出使用鸽舍模板法时出现的绑扎误差。这样就可以选择建造 AS 稳定器的设备和软件。通过对物体气动特性改进值的选择,可以根据标准化的 NACA 0012 剖面制造 AS。这可以作为组织小规模生产研究对象的信息基础。也就是说,总的来说,逆向工程过程使得对截面、空气动力特性进行详细分析成为可能,并为未来的改进型轮廓进行改进。这种设计方法提供了更广泛的机会,消除了中间环节,并在制造过程中保持了目标参数的高精度,这是飞机制造的主要要求之一。
Mathematical models creation for calculating dimensional accuracy at the construction stages of an analytical standard using the chain method
The object of research is the process of forming a mathematical model (MM) for calculating accuracy at the stages of construction an analytical standard (AS) using the chain method, the application of which is shown on the example of an aviation object (AO). The analysis of the investigated AO, namely the helicopter stabilizer, was carried out using modern 3D scanners and the creation of its analytical portrait (AP). The problem is to create the most similar AP and compare it with AS, taking into account the results of the calculations. The following results were obtained: the AS was built and the AP of the stabilizer geometry was created, a comparative analysis of the AP and AS was carried out, and the results of the accuracy of the object geometry calculations were obtained. Aerodynamic calculations of stabilizer characteristics were also carried out, analysis of standardized aerodynamic profiles was carried out taking into account the accepted limitations for forming the stabilizer AS. The scientific and practical novelty of the obtained results is as follows: the created MM for calculating the accuracy of the dimensions of the unit contour using the chain method made it possible to estimate the tying errors that occur when using the loft-template method. This made it possible to choose equipment and software for construction the AS stabilizer. The selection of improved values of the object's aerodynamic characteristics made it possible to build an AS based on the standardized NACA 0012 profile. This can be used as an information basis for the organization of small-scale production of the object under study. That is, in general, the process of reverse engineering made it possible to conduct a detailed analysis of sections, aerodynamic characteristics and improve them for the future improved profile. This design approach provides wider opportunities, eliminates intermediate links and maintains high accuracy of object parameters during its manufacture, which is one of the main requirements in aircraft construction.