2003 ◽  
Vol 10 (1) ◽  
pp. 85-91 ◽  
Author(s):  
Goutam Das ◽  
Sandip Ghosh Chowdhury ◽  
Ashok Kumar Ray ◽  
Swapan Kumar Das ◽  
Deepak Kumar Bhattacharya

2020 ◽  
Vol 20 (4) ◽  
pp. 1162-1174
Author(s):  
Khier Sabri ◽  
Mohamed Gaceb ◽  
Mohamed Ouali Si-Chaib

2014 ◽  
Vol 14 (2) ◽  
pp. 160-166 ◽  
Author(s):  
R. K. Mishra ◽  
K. Srinivasan ◽  
Johney Thomas ◽  
Nandi Vaishakhi ◽  
Raghavendra R. Bhat

2015 ◽  
Vol 69 (2) ◽  
pp. 659-663 ◽  
Author(s):  
M. C. Antony Harison ◽  
M. Swamy ◽  
A. H. V. Pavan ◽  
G. Jayaraman

2008 ◽  
Vol 15 (1-2) ◽  
pp. 129-141 ◽  
Author(s):  
Zdzislaw Mazur ◽  
Rafael Garcia-Illescas ◽  
Jorge Aguirre-Romano ◽  
Norberto Perez-Rodriguez

Author(s):  
R. K. Mishra ◽  
Johny Thomas ◽  
K. Srinivasan ◽  
Vaishakhi Nandi ◽  
R. Raghavendra Bhatt

AbstractFailure of a high pressure (HP) turbine blade in a military turbofan engine is investigated to determine the root cause of failure. Forensic and metallurgical investigations are carried out on the affected blades. The loss of coating and the presence of heavily oxidized intergranular fracture features including substrate material aging and airfoil curling in the trailing edge of a representative blade indicate that the coating is not providing adequate oxidation protection and the blade material substrate is not suitable for the application at hand. Coating spallation followed by substrate oxidation and aging leading to intergranular cracking and localized trailing edge curling is the root cause of the blade failure. The remaining portion of the blade fracture surface showed ductile overload features in the final failure. The damage observed in downstream components is due to secondary effects.


2013 ◽  
Vol 1 (3) ◽  
pp. 192-199 ◽  
Author(s):  
D. Ziegler ◽  
M. Puccinelli ◽  
B. Bergallo ◽  
A. Picasso

Sign in / Sign up

Export Citation Format

Share Document