2020
DOI: 10.1115/1.4047142
|View full text |Cite
|
Sign up to set email alerts
|

A Comparison of Weldability, Structure, and Mechanical Properties of CM64 and Tribaloy T-800 Welds for Hard-Facing of Turbine Blades

Abstract: Weldability, microstructure and tensile properties of CM64 and Tribaloy T-800 (T800) cobalt-based hard-facing materials were studied. Successful CM64 hard-facing could be achieved at ambient temperature using manual gas tungsten arc welding (GTAW-MA). It was shown that T800 welded at ambient temperature was prone to cold cracking due to a combination of low ductility with high welding stresses that limited accommodation of residual stresses by a plastic deformation within the weld beads, which was not the case… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2021
2021
2024
2024

Publication Types

Select...
6

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(2 citation statements)
references
References 17 publications
0
2
0
Order By: Relevance
“…However, controlling the cooling rate in a laser DED process is challenging. Base plate heating and/or heating the region of interest was previously found to control the cooling rate so that cracking does not occur [40,41]. Conventionally, thermal residual stresses are eliminated via post heat treatment.…”
Section: Discussionmentioning
confidence: 99%
See 1 more Smart Citation
“…However, controlling the cooling rate in a laser DED process is challenging. Base plate heating and/or heating the region of interest was previously found to control the cooling rate so that cracking does not occur [40,41]. Conventionally, thermal residual stresses are eliminated via post heat treatment.…”
Section: Discussionmentioning
confidence: 99%
“…The T800 alloy can be deposited up to a 5 mm thickness with the laser DED system by preheating the base plate to 500 • C [40]. Keshavarz et al used the preheating method for welding a T800 alloy and to mitigate the heat-affected-zone liquation cracking by heating over 900 • C [41]. This approach may be suitable for small components where preheating the substrate alleviates rapid cooling through conductive heat transfer but would not work for larger components where the conductive heat transfer is diminished with increasing the thickness of the component.…”
Section: Introductionmentioning
confidence: 99%