IDENTIFICATION MC CARBIDE OF NICKEL-BASED SUPERALLOY RENE 142 AS THE RESULT OF SOLUTION HEAT TREATMENT PROCESS
Rene 142 nickel-based superalloys produced by directional solidification technique with columnar grain widely used for turbine blades of aircraft engines. Columnar grain structures are strengthened by carbide and gamma prime (?????) phases, which is distributed at grain boundary and intergrain....
Saved in:
Main Author: | Pradondon, Kasih |
---|---|
Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/68987 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
EFFECT OF HOLDING TIME AND COOLING RATE ON THE MICROSTRUCTURE OF RENE 142 SUPERALLOY
by: Raihan Renando, Ghiffary -
EVOLUSI PRECIPITATE ?' PADA SUPERALLOY RENE 142 AKIBAT OVER-TEMPERATURE
by: Wira Akira, Muhammad -
CYCLIC OVERAGEING PRE-WELD HEAT TREATMENT FOR NICKEL-BASED SUPERALLOY (RENE 80)
by: LIU NING
Published: (2020) -
Mechanism of post-weld heat treatment cracking in Rene 80 nickel based superalloy
by: Lim, L.C., et al.
Published: (2014) -
Influence of heat treatment on the conductivity of nickel-based superalloys
by: Nagarajan, Balasubramanian, et al.
Published: (2018)