2013
DOI: 10.1016/j.matchar.2012.11.006
|View full text |Cite
|
Sign up to set email alerts
|

Solution heat-treatment of Nb-modified MAR-M247 superalloy

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

0
5
0
1

Year Published

2014
2014
2023
2023

Publication Types

Select...
8
1

Relationship

0
9

Authors

Journals

citations
Cited by 28 publications
(6 citation statements)
references
References 11 publications
(11 reference statements)
0
5
0
1
Order By: Relevance
“…The initial as-cast microstructures of the investigated alloys were similar, presenting dendritic segregations with c¢ particles and MC-type carbides dispersed in the c matrix, in agreement with other studies found in the literature for alloys with similar composition. [10][11][12][13][14][15][16][17][18] At 1000°C, parabolic oxidation behavior was observed only in the first 100 hours of oxidation for both alloys, before oxide scale spallation began to be the predominant degradation mechanism. On the other hand, the oxidation curves at 800°C and 900°C presented parabolic behavior for the entire tests' duration.…”
Section: Discussionmentioning
confidence: 99%
“…The initial as-cast microstructures of the investigated alloys were similar, presenting dendritic segregations with c¢ particles and MC-type carbides dispersed in the c matrix, in agreement with other studies found in the literature for alloys with similar composition. [10][11][12][13][14][15][16][17][18] At 1000°C, parabolic oxidation behavior was observed only in the first 100 hours of oxidation for both alloys, before oxide scale spallation began to be the predominant degradation mechanism. On the other hand, the oxidation curves at 800°C and 900°C presented parabolic behavior for the entire tests' duration.…”
Section: Discussionmentioning
confidence: 99%
“…The recommended temperature for this treatment is approximately 1260˚C for 8 hours, which enables the alloy to achieve a homogeneous gamma matrix with fine gamma prime phases. However, incipient melting was observed at 1280˚C in this alloy [9]. Thermodynamic calculations have shown that the lower temperature for solutioning in Mar-M247 superalloy is around 1220˚C.…”
Section: Introductionmentioning
confidence: 74%
“…3a, 3b). In the microstructure, M 23 C 6 -, M 6 C-, and MC-type carbides can be present [2]. Evidence of an MC-type carbide (Hf, Ta)C was confirmed during energy dispersive spectroscopy (Fig.…”
Section: Fig 2 Cast Mar-m247: A) Microstructure; B) Eds Spectrummentioning
confidence: 86%
“…: AGH University of Science and Technology, Faculty of Metals Engineering and Industrial Computer Science, Krakow, Poland; lrakoczy@agh.edu.pl at high temperatures, and high mechanical properties (including creep strength) made it a widely used alloy in gas turbine structures. Its combination of unique properties contributed to MAR-M247's use for rotating components in aircraft engines, including turbine blades and segments [1,2]. Strengthening of the alloy mainly corresponds with semicoherent precipitation γ' .…”
Section: Introductionmentioning
confidence: 99%