Additive Manufacturing of IN100 Superalloy Through Scanning Laser Epitaxy for Turbine Engine Hot-Section Component Repair: Process Development, Modeling, Microstructural Characterization, and Process Control
- 28 April 2015
- journal article
- Published by Springer Science and Business Media LLC in Metallurgical and Materials Transactions A
- Vol. 46 (9), 3864-3875
- https://doi.org/10.1007/s11661-015-2912-6
Abstract
No abstract availableKeywords
This publication has 18 references indexed in Scilit:
- Microstructures of Rene 142 nickel-based superalloy fabricated by electron beam meltingActa Materialia, 2013
- Relationship between Ti/Al ratio and stress-rupture properties in nickel-based superalloyMaterials Science and Engineering: A, 2012
- Nickel based superalloy welding practices for industrial gas turbine applicationsScience and Technology of Welding and Joining, 2004
- Direct laser fabrication of superalloy cermet abrasive turbine blade tipsMaterials & Design (1980-2015), 2000
- Practical considerations and capabilities for laser assisted direct metal depositionMaterials & Design (1980-2015), 2000
- In the final analysisJOM, 1999
- Direct SLS Processing for Production of Cermet Composite Turbine Sealing ComponentsMaterials and Manufacturing Processes, 1998
- Freezing-point-blackbody radiation sources for the 2978–108462 °C temperature rangeApplied Optics, 1996
- On the theory of anomalous yield behavior of Ni3Al — Effect of elastic anisotropyScripta Metallurgica, 1986
- Temperature and orientation dependence of the yield stress in Ni{in3}Ga single crystalsActa Metallurgica, 1973