Digitally Reverse Modeling for the Repair of Blades in Aero-Engines

Tao Wang; Yi Liu Liu; Li Wen Wang; Hao Wang; Jie Tang

doi:10.4028/www.scientific.net/AMM.141.258

Paper Titles

Design and Implementation of Modular FPGA-Based Multiple-Axis Motion Controller for CNC
p.233

Design of Automatic Assembly System of Saw Chain
p.239

Development of a Master-Slave Architecture Handheld Rotating Machine Fault Diagnosis Instrument
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Development of an Ontology-Based and STEP-Compliant Intelligent CNC System
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Digitally Reverse Modeling for the Repair of Blades in Aero-Engines
p.258

Error Analysis and Calibration of Gyro-Stabilized Platform for Electro-Optical Pointing System
p.264

Evaluation and Design of SNS User Interface in Handheld Device Based on Fuzzy Clustering
p.270

Experimental Research on the Crack Identification of Drawing Parts Based on AE Technique
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Extraction of Frequency-Variable Characteristics and Analysis of Modulation Mechanism under Periodic Excitation
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 141Digitally Reverse Modeling for the Repair of...

Digitally Reverse Modeling for the Repair of Blades in Aero-Engines

Abstract:

Blades are key components in aircraft engines, and flight safety is directly impacted by the repair quality of blades. Digital modeling for the surfaces of high pressure blades is conducted in this study based on the cloud data collected with scan. Boundary points of blades are obtained with the method of varied step lengths according to curvature, and then the envelope curves are plotted from the approximation of these boundary points with a third power B spline. 3-D digital models of blades in aero-engines are established with the envelope curves and the condensed data cloud. Results illustrate the smoothness and accuracy of the proposed engine blade repair model.

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Periodical:

Applied Mechanics and Materials (Volume 141)

Pages:

258-263

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.141.258

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Online since:

November 2011

Authors:

Tao Wang, Yi Liu Liu, Li Wen Wang, Hao Wang, Jie Tang

Keywords:

Aero-Engine, Blade, Envelope Curve, Varied Step Length

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