Details
Originalsprache | Englisch |
---|---|
Seiten (von - bis) | 304-309 |
Seitenumfang | 6 |
Fachzeitschrift | Procedia CIRP |
Jahrgang | 94 |
Frühes Online-Datum | 15 Sept. 2020 |
Publikationsstatus | Veröffentlicht - 2020 |
Extern publiziert | Ja |
Abstract
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Steuerungs- und Systemtechnik
- Ingenieurwesen (insg.)
- Wirtschaftsingenieurwesen und Fertigungstechnik
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in: Procedia CIRP, Jahrgang 94, 2020, S. 304-309.
Publikation: Beitrag in Fachzeitschrift › Konferenzaufsatz in Fachzeitschrift › Forschung › Peer-Review
}
TY - JOUR
T1 - Single-crystal height extension by Laser Metal Deposition of CMSX-4
AU - Buchbender, I.
AU - Hoff, C.
AU - Hermsdorf, J.
AU - Wesling, V.
AU - Kaierle, S.
N1 - Funding information: This project is funded by the Forschungsgemeinschaft (DFG, German Foundation) – SFB 871/3 – 119193472.
PY - 2020
Y1 - 2020
N2 - The introduction of directionally solidified and single-crystal nickel-based superalloys have led to a higher thermal efficiency of engines by allowing for an increase in turbine inlet temperatures from 1000°C to 1400°C. These temperatures however lead to higher thermal stress and corrosive environments, resulting in a shorter life span. Previous work has shown the applicability of laser metal deposition (LMD) for the regeneration of these high value components, while maintaining primary crystalline orientation of single-crystal high pressure turbine blades. However, the processing of these materials by LMD poses several challenges, such as susceptibility to cracking, the formation of misoriented grains and low weldability. This paper examines deposition strategies to extend single-crystal height. While a continuous, meandering strategy shows the most promising percentage single-crystallinity results, an additional remelting step increases epitaxial deposition height. Apart from percentage single-crystallinity and deposition height, this study quantifies the effect of these strategies on cracking and the formation of misorientations.
AB - The introduction of directionally solidified and single-crystal nickel-based superalloys have led to a higher thermal efficiency of engines by allowing for an increase in turbine inlet temperatures from 1000°C to 1400°C. These temperatures however lead to higher thermal stress and corrosive environments, resulting in a shorter life span. Previous work has shown the applicability of laser metal deposition (LMD) for the regeneration of these high value components, while maintaining primary crystalline orientation of single-crystal high pressure turbine blades. However, the processing of these materials by LMD poses several challenges, such as susceptibility to cracking, the formation of misoriented grains and low weldability. This paper examines deposition strategies to extend single-crystal height. While a continuous, meandering strategy shows the most promising percentage single-crystallinity results, an additional remelting step increases epitaxial deposition height. Apart from percentage single-crystallinity and deposition height, this study quantifies the effect of these strategies on cracking and the formation of misorientations.
KW - Laser cladding
KW - Single-crystal
KW - Superalloys
UR - http://www.scopus.com/inward/record.url?scp=85093361227&partnerID=8YFLogxK
U2 - 10.1016/j.procir.2020.09.057
DO - 10.1016/j.procir.2020.09.057
M3 - Conference article
VL - 94
SP - 304
EP - 309
JO - Procedia CIRP
JF - Procedia CIRP
SN - 2212-8271
ER -