CAD system of design and engineering provision of die forming of compressor blades for aircraft engines

Innovations and Prospects of Development of Mining Machinery and Electrical Engineering

矿业工程;电工学

Khaimovich, I.N.^1

Samara National Research University, 34, Moskovskoe shosse, Samara

443086, Russia^1

关键词: Calculation algorithms;    Compressor blades;    Generalized algorithms;    Point location;    Structural elements;    Technological equipments;    Technological solution;    Three dimensional arrays;   

Others  :  https://iopscience.iop.org/article/10.1088/1755-1315/87/8/082024/pdf
DOI  :  10.1088/1755-1315/87/8/082024

来源: IOP

【 摘 要 】

The articles provides the calculation algorithms for blank design and die forming fitting to produce the compressor blades for aircraft engines. The design system proposed in the article allows generating drafts of trimming and reducing dies automatically, leading to significant reduction of work preparation time. The detailed analysis of the blade structural elements features was carried out, the taken limitations and technological solutions allowed forming generalized algorithms of forming parting stamp face over the entire circuit of the engraving for different configurations of die forgings. The author worked out the algorithms and programs to calculate three dimensional point locations describing the configuration of die cavity. As a result the author obtained the generic mathematical model of final die block in the form of three-dimensional array of base points. This model is the base for creation of engineering documentation of technological equipment and means of its control.