Modeling of worn surface geometry for engine blade repair using Laser-aided Direct Metal Deposition process-Reference-Cited by-同舟云学术

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Modeling of worn surface geometry for engine blade repair using Laser-aided Direct Metal Deposition process

Published:2018-01 Issue: Volume:15 Page:1-4
ISSN:2213-8463
Container-title:Manufacturing Letters
language:en
Short-container-title:Manufacturing Letters

Author:

Zhang Xinchang,Li Wei,Cui Wenyuan,Liou Frank

Funder

National Science Foundation

Intelligent Systems Center

Center for Aerospace Manufacturing Technologies

Material Research Center at Missouri S&T

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanics of Materials

Reference14 articles.

1. Investigation of a 3D non-contact measurement based blade repair integration system;Gao;Aircr Eng Aerosp Technol,2005

2. Gas turbines blades-a critical review of failure on first and second stages;Dewangan;Int J Mech Eng Robot Res,2015

3. A repair and overhaul methodology for aeroengine components;Yilmaz;Robot Comput Integr Manuf,2010

4. Equivalent self-adaptive belt grinding for the real-R edge of an aero-engine precision-forged blade;Xiao;Int J Adv Manuf Technol,2016

5. Remanufacturing of turbine blades by laser direct deposition with its energy and environmental impact analysis;Wilson;J Clean Prod,2014

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