Development of intermetallic materials for aerospace systems

1992 ◽  
Vol 8 (4) ◽  
pp. 367-375 ◽  
Author(s):  
D. M. Dimiduk ◽  
D.B. Miracle ◽  
C. H. Ward
2020 ◽  
Vol 321 ◽  
pp. 04013
Author(s):  
Sesh Tamirisakandala ◽  
Ernie Crist ◽  
Fusheng Sun ◽  
Matthew Dahar

Next generation fuel-efficient jet engines are running hotter presenting a structural challenge for the exhaust systems and structures adjacent to the engines. A conventional and affordable titanium alloy with superior oxidation resistance provides significant weight reductions and associated cost savings by eliminating the need for high density material systems such as nickel-base superalloys for service temperatures in between current titanium and nickel, enabling major technology advancement in high temperature aerospace applications. This paper presents an overview of Arconic’s engineered material ARCONIC-THORTM to address the needs of future aerospace systems.


2021 ◽  
Author(s):  
Vl. V. Zelentsov ◽  
N. G . Surkova ◽  
A. B. Mineev ◽  
G. A. Shcheglov ◽  
S. A. Novikova

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