The Research of Aeroplane Engine Blade 3D Point Clouds Processing

Hao Wang; Dong Yan Wang; Ting Jian Dong; Tao Wang

doi:10.4028/www.scientific.net/AMM.241-244.2129

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To the Question of Parametrical Dynamic Three-Dimension Model Design of the Automated Power Generating Complex Mixer
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A New Method Based on Finite Element Analysis for Crankshaft Strength
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The Research of Aeroplane Engine Blade 3D Point Clouds Processing
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Numerical Analysis of Stress and Temperature Coupled Field for Boiler Superheater in Thermal Power Plant
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 241-244The Research of Aeroplane Engine Blade 3D Point...

The Research of Aeroplane Engine Blade 3D Point Clouds Processing

Abstract:

This paper made the point cloud data processing for the aircraft engine’s blade. First, collected rough point cloud data by using visual measuring equipment. Then, noise reduced and smoothed, feature detected the point cloud data, took the reasonable simplification, finished pre-processing the point cloud data. Finally, took the surface fitting for the point cloud data after processed. The result proved that processing the point cloud data reduced modeling and machining time, and improved smoothness of the model.

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Periodical:

Applied Mechanics and Materials (Volumes 241-244)

Pages:

2129-2132

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.241-244.2129

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Online since:

December 2012

Authors:

Hao Wang, Dong Yan Wang, Ting Jian Dong, Tao Wang

Keywords:

Aeroplane Engine Blade, Feature Detect, Noise Reduce and Smooth, Surface Fitting

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