Session: 18-02: Additive Manufacturing II
Paper Number: 152666
From Legacy Alloys to Next-Gen Materials: the Future of Additive Manufacturing in Gas Turbine Hot Sections
The adoption of additive manufacturing (AM) in the turbomachinery sector, particularly for hot section gas turbine parts, has seen rapid growth over the past decade. This technological shift offers the potential to produce complex geometries that were previously unachievable using traditional methods. However, significant challenges remain, particularly in the high-temperature performance of AM-produced nickel- and cobalt-based superalloys. Superalloys such as IN738LC, IN939, Mar-M-247, and Mar-M-509 have been tested extensively, but they present issues related to creep resistance, oxidation, corrosion, and ductility when exposed to extreme turbine operating conditions.
For example, IN738LC and Mar-M-247 have shown promise in their moderate temperature mechanical properties, but the manufacturing process, including selective laser melting (SLM), often leads to microstructural challenges like crack formation due to thermal gradients. To mitigate this, various strategies during manufacturing have been explored, which help enhance material structure and reduce cracking risks. However, these solutions remain imperfect, necessitating continued investigation into the materials’ long-term performance at elevated temperatures.
Recent advancements in AM have led to the development of new superalloys specifically designed for gas turbine applications, including ABD1000, GRX810, LW4275, and the GammaPrint series alloys (GammaPrint 1100 and 700). These materials are engineered to match the limits of temperature resistance and oxidation performance of traditional alloys, but with the promise of improved printability using the SLM process. Initial tests of these newer alloys show promise of good creep resistance and high-temperature properties, positioning them as key contenders in future turbine engine applications.
This paper examines both the current challenges and advancements in AM superalloys, presenting data on their performance and manufacturability. Through published studies and ongoing research, it becomes clear that while additive manufacturing offers revolutionary capabilities, optimizing the high-temperature performance of superalloys remains crucial for achieving widespread industrial adoption.
Presenting Author: Yogiraj Pardhi Sulzer Management Ltd
Presenting Author Biography: Dr. Yogiraj Pardhi is the global lead for Additive Manufacturing at Sulzer Services. As a senior expert in additive manufacturing and materials, he spearheads the implementation of the global strategy for additive manufacturing within Sulzer. Dr. Pardhi has a successful track record in qualifying and industrializing advance manufacturing technologies for both manufacturing and repairing industrial gas turbines and turbomachinery parts. Previously, he served as the AM Lead for materials at Rolls-Royce Plc, where he successfully industrialized additive manufacturing for the production of aeroengine hot section parts. He holds a first degree in Mechanical Engineering and a PhD in Materials Science. Dr. Pardhi brings over 12 years of industry experience in aerospace and turbomachinery equipment manufacturing and repair, and he is a fellow of The Institute of Materials, Minerals, and Mining.
Authors:
Yogiraj Pardhi Sulzer Management LtdFrom Legacy Alloys to Next-Gen Materials: the Future of Additive Manufacturing in Gas Turbine Hot Sections
Paper Type
Technical Paper Publication