Round and Round:
Confronting stress factors in rotating parts design
Confronting stress factors in rotating parts design
The design and operation of gas turbines in aircraft applications provides tough engineering challenges in today’s market. With the rise of fuel prices, new product development has focused on maximizing thermal efficiency, increasing time-on-wing, and reducing weight. A major backbone of gas turbines are rotating parts, which are regularly exposed to high stresses, steep thermal gradients, and corrosive environments. Due to the high energy levels, detailed attention is paid to these components by manufacturers, with regulatory bodies requiring life limits to be established for the majority of these parts. Understanding basic rotating part design provides a sturdy framework for new designs and requirements of new products introduced to the market.
Chuck Adams, General Electric Aviation
Presented September 28, 2015
Chuck Adams is a Design Engineer at General Electric Aviation in Cincinnati, OH, participating in the Engineering Development Program. Chuck is focused on the CFM LEAP-1B High Pressure Turbine module, with the engine line set to enter service in 2017. He’s also performed life management activities for rotating parts in various commercial and military engine programs. Chuck received a B.S. in Mechanical Engineering from Boise State University, a M.S. in Mechanical Engineering from North Dakota State University, and is currently an MBA candidate at Indiana University’s Kelley School of Business.