A wall-thickness compensation strategy for wax pattern of hollow turbine blade
Authors:
Open Access
- 1 August 2019
- journal article
- research article
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 32 (8) , 1982-1993
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (51475374, 51505387)
- Fundamental Research Funds for the Central Universities (3102015ZY087)
This publication has 37 references indexed in Scilit:
- Determination of interfacial heat-transfer coefficient during investment-casting process of single-crystal bladesJournal of Materials Processing Technology, 2011
- Three-dimensional point-based shape registration algorithm based on adaptive distance functionIET Computer Vision, 2011
- A unified framework of error evaluation and adjustment in machiningInternational Journal of Machine Tools and Manufacture, 2008
- An experimental investigation on dimensional stability of injected wax patterns of gas turbine bladesJournal of Materials Processing Technology, 2007
- Conversion of an investment casting sprue wax to a pattern wax by the modification of its propertiesMaterials & Design (1980-2015), 2004
- A novel alternative to the additives in investment casting pattern wax compositionsMaterials & Design (1980-2015), 2003
- An optimum design for 3-D fixture synthesis in a point set domainIEEE Transactions on Robotics and Automation, 2000
- A Variational Method of Robust Fixture Configuration Design for 3-D WorkpiecesJournal of Manufacturing Science and Engineering, 1997
- A method for registration of 3-D shapesIEEE Transactions on Pattern Analysis and Machine Intelligence, 1992
- Deformable curve and surface finite-elements for free-form shape designACM SIGGRAPH Computer Graphics, 1991