A Study on Direct Machining of Turbine Blades from Point Cloud Data

This paper presents research results on direct machining of Turbine blades in Turbocharger from point cloud data. In the study, the ATOS Core 80 scanner was used to create a point cloud file from the parts of the compression Turbine blades of the sample Turbocharger. From the point cloud data file,...

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Tác giả chính: Ta, Van Ranh, Le, Hong Ky, Tran, Vinh Hung
Định dạng: Bài trích
Ngôn ngữ:English
Nhà xuất bản: Springer 2022
Chủ đề:
Truy cập trực tuyến:https://link.springer.com/chapter/10.1007/978-3-030-99666-6_41
https://dlib.phenikaa-uni.edu.vn/handle/PNK/5938
https://doi.org/10.1007/978-3-030-99666-6_41
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Tóm tắt:This paper presents research results on direct machining of Turbine blades in Turbocharger from point cloud data. In the study, the ATOS Core 80 scanner was used to create a point cloud file from the parts of the compression Turbine blades of the sample Turbocharger. From the point cloud data file, without any processing, the machining code is programmed using Inventor Professional software. The 5-axis HASS VF2 CNC milling machine is used to perform the machining steps. To evaluate the accuracy of machining parts compared with sample parts, the CMM coordinate measuring machine is used, and the original point cloud data file is compared with the detailed point cloud data file after processing by GOM Inspect software. The research results show that it is possible to directly machine Turbine blades from point cloud data using Inventor Professional software without processing, but it still achieves high accuracy.