3D Model Reconstruction of the Broken Aero Engine Blade Based on the Detection Operator

Hao Wang; Guo Jun Tong; Tao Wang; Li Wen Wang

doi:10.4028/www.scientific.net/KEM.693.1289

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Optimization of Electrostatic Atomization Cutting Using 3D FE Simulation of Electrostatic Field
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Quantitative Analysis and Evaluation of Valve Core Spherical Surface Grinding Texture
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3D Model Reconstruction of the Broken Aero Engine Blade Based on the Detection Operator
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A Fault Diagnosis System Based on Bistable Stochastic Resonance and Dynamic Time Warping
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A Kind of Vibration Sensor and Testing System in Electromechanical Equipment Based on Fiber Bragg Grating
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HomeKey Engineering MaterialsKey Engineering Materials Vol. 6933D Model Reconstruction of the Broken Aero Engine...

3D Model Reconstruction of the Broken Aero Engine Blade Based on the Detection Operator

Abstract:

This paper made the digital model reconstruction of the RB211 high pressure turban blade. First, collected rough points cloud data by using visual measuring equipment. Then, finished pre-processing the point cloud data, took the rational simplification. Finally, a new algorithm was used to reconstructing the 3D digital model. The results proved that this method improved smoothness of the model, and reduced time and cost of modeling and machining.

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Periodical:

Key Engineering Materials (Volume 693)

Pages:

1289-1293

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.693.1289

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Online since:

May 2016

Authors:

Hao Wang*, Guo Jun Tong, Tao Wang, Li Wen Wang

Keywords:

Digital Model, High Pressure Turban Blade, RB211

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