Development of a Laser Cladding Process for Shrouded Turbine Blades

892300

9/1/1989

Authors
Abstract
Content
A laser cladding process has been successfully developed, qualified and implemented into production for hardfacing shrouded turbine engine blades. These nickel base superalloy hot section blades were hardfaced with a cobalt base filler metal. The process, employing dynamic powder feeding as a means of introducing filler metal to the substrate, offers significant advantages over conventional welding processes including: low heat input, limited dilution, improved metallurgical quality and uniform, near-net-shape build-ups.
Meta TagsDetails
DOI
https://doi.org/10.4271/892300
Citation
lovene, M. and Everett, M., "Development of a Laser Cladding Process for Shrouded Turbine Blades," Aerospace Technology Conference and Exposition, Anaheim, California, United States, September 25, 1989, https://doi.org/10.4271/892300.
Additional Details
Publisher
Published
9/1/1989
Product Code
892300
Content Type
Technical Paper
Language
English