Year: 2013
Type: conference-paper
Abstract: Titanium intermetallic materials are likely to play a significant role in the production of future aeroengines. Although applicable for only a relatively narrow range of applications, gamma-TiAl intermetallic materials are nonetheless the focus of all leading aerospace/gas turbine manufacturers, as a replacement for some nickel-based superalloy components in parts of the engine subject to temperatures < 900 °C. This work presents the results from grinding tests on two types of Gamma TiAl alloys.
Source: Procedia Engineering
Authors: A. Beranoagirre, L.N. López de Lacalle
Language: English
Subfield: Mechanical Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: diamond
OpenAlex ID: W2027805000