Abstract

Temperature-time cycles are essential for the formation of microstructures and thus the mechanical properties of materials. In additive manufacturing, components undergo changing temperature regimes because of the track- and layer-wise build-up. Because of the high brittleness of titanium aluminides, preheating is used to prevent cracking. This also effects the thermal history. In the present study, local solidification conditions during the additive manufacturing process of Ti-48Al-2Cr-2Nb with laser metal deposition (LMD) are investigated by both simulation and experimental investigations. Dependencies of the build-up height, preheating temperatures, process parameters and effects on the resulting microstructure are considered, including the heat treatment. Solidification conditions are found to be dependent on the build height and thus actual preheating temperature, process parameters and location in the melt pool. Influences on both chemical composition and microstructure are observed. Resulting differences can almost be balanced through post heat treatment.

Highlights

  • DUE to the high aluminum content, titanium aluminides are highly resistant against oxidation and corrosion

  • The authors found the amount of transformed a-phase to be highly dependent on the cooling rates by which the transformation range can be extended to temperatures even well below 900 °C for cooling rates > 10 °C/s, which applies to laser metal deposition (LMD)

  • The solidification conditions and their influence on chemical composition and microstructure during laser cladding of the TiAl alloy GE4822 are investigated by both experimental measurements and simulation

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Summary

INTRODUCTION

DUE to the high aluminum content, titanium aluminides are highly resistant against oxidation and corrosion. The current generations of low-pressure turbines (LPT) installed on GE GEnX-1B and PW1100G TiAl blades are used and manufactured by General Electric (GE)[1] and MTU Aero Engines.[2] airplanes of the A320neo, A321neo and Boeing 787 (Dreamliner) families fly every day with many TiAl blades. For manufacturing of these blades, cast and forging processes are established. The state of the art of LMD of GE4822 is extended by a modeling approach to predict the material’s final characteristics depending on the initial process constraints regarding the microstructure and the chemical composition and influence of subsequent heat treatments

Material
LMD Setup and Processing
Simulation
Thermography
Influence of beam diameter on the actual pre-heating temperature
Influence of preheating temperature on local solidification
Microstructure Analysis
B À1 Dys
CONCLUSION
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