Superalloys 1992 (Seventh International Symposium) 1992
DOI: 10.7449/1992/superalloys_1992_457_466
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The Effect of Process Variables on the Structure and Properties of ODS, γ'-Hardened Nickel-Base Superalloys

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Cited by 2 publications
(22 citation statements)
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“…Both Baker et al [36,37] and Zhang et al [38,41,44] have found that in particle-free metals or alloys, there is a lower limit to the annealing temperature for columnar grain formation through directional secondary Si 1373 NS 3-30 [13] Ni-based superalloy PWA1123 NS NS NS [14] Fe-3wt-%Si 1323-1623 320-550 increased with increasing T 19 [15] Ni-base superalloy TMO-2 1563 25 50-100 [16] Ni-base superalloy MA6000 1123-1373 NS NS [17] Ni-base superalloy MA6000 1373-1573 NS 48-600 [18] Ni-base superalloy APK-6 1493 NS 2.0-20.0 [19] Ni-base superalloy MA6000 and MA760 1523 NS 2-200 K min −1 (heating rate) [20] Ni-base superalloy MA6000 1443 25 38 [21] Fe-based Superalloy MA957 1673 NS 20-75 [22] Ni-base superalloy MA6000 1623 40 38 [23] Ni-base superalloy MA6000 1223-1503 NS 15-400 [24] Ni-based superalloy PM3030 1503 100 NS [25] Ni-base superalloy MA6000 and MA760 1573 40 38 [26] Fe-based Superalloy MA 956 and MA957 1533-1613 50-140 24-75 [27] Ni-base superalloy MA6000 and MA760 1448 NS 38 [28] Ni-base superalloy MA760 and iron-based superalloy MA 956 ∼1523 NS 48-600 [29] Ni-base superalloy MA6000 1223-1273 NS 10-100 [30] Ni-base superalloy SRR99 ∼1533 NS 5 [31] Ni-base superalloy MA6000 1573 NS 38 [32] N i 3 Al 1698 NS 25-100 [33] Ni-base superalloy APK-6 1493 NS NS [34] TiAl-based alloy 1553-1593 NS 1.62 and 4.02 K min −1 (heating rate) [35] Cu 643-743 70-270 2-600 [36] Ni 1273 ∼1000 and 50 2-100 [37] Ni 1073-1273 ∼1000 and 50 2-100 [38] Iron 973-1123 ∼200 3.6-90 [39] Iron 1123-1473 ∼200 and 400 3.6-90 [40] Iron 1123 ∼200 0.36-90 [41] Iron 948-1173 ∼200 1.08-108 …”
Section: Annealing Temperaturementioning
confidence: 99%
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“…Both Baker et al [36,37] and Zhang et al [38,41,44] have found that in particle-free metals or alloys, there is a lower limit to the annealing temperature for columnar grain formation through directional secondary Si 1373 NS 3-30 [13] Ni-based superalloy PWA1123 NS NS NS [14] Fe-3wt-%Si 1323-1623 320-550 increased with increasing T 19 [15] Ni-base superalloy TMO-2 1563 25 50-100 [16] Ni-base superalloy MA6000 1123-1373 NS NS [17] Ni-base superalloy MA6000 1373-1573 NS 48-600 [18] Ni-base superalloy APK-6 1493 NS 2.0-20.0 [19] Ni-base superalloy MA6000 and MA760 1523 NS 2-200 K min −1 (heating rate) [20] Ni-base superalloy MA6000 1443 25 38 [21] Fe-based Superalloy MA957 1673 NS 20-75 [22] Ni-base superalloy MA6000 1623 40 38 [23] Ni-base superalloy MA6000 1223-1503 NS 15-400 [24] Ni-based superalloy PM3030 1503 100 NS [25] Ni-base superalloy MA6000 and MA760 1573 40 38 [26] Fe-based Superalloy MA 956 and MA957 1533-1613 50-140 24-75 [27] Ni-base superalloy MA6000 and MA760 1448 NS 38 [28] Ni-base superalloy MA760 and iron-based superalloy MA 956 ∼1523 NS 48-600 [29] Ni-base superalloy MA6000 1223-1273 NS 10-100 [30] Ni-base superalloy SRR99 ∼1533 NS 5 [31] Ni-base superalloy MA6000 1573 NS 38 [32] N i 3 Al 1698 NS 25-100 [33] Ni-base superalloy APK-6 1493 NS NS [34] TiAl-based alloy 1553-1593 NS 1.62 and 4.02 K min −1 (heating rate) [35] Cu 643-743 70-270 2-600 [36] Ni 1273 ∼1000 and 50 2-100 [37] Ni 1073-1273 ∼1000 and 50 2-100 [38] Iron 973-1123 ∼200 3.6-90 [39] Iron 1123-1473 ∼200 and 400 3.6-90 [40] Iron 1123 ∼200 0.36-90 [41] Iron 948-1173 ∼200 1.08-108 …”
Section: Annealing Temperaturementioning
confidence: 99%
“…The lower processing temperatures required for directional recrystallisation allow easier processing of high melting point materials such as tungsten [5,6]; . It is likely that minimal solute redistribution will occur, allowing single crystals or columnar grain structures to be produced from non-castable alloys, such as advanced nickel-based superalloys [7][8][9][10][11]13,[15][16][17][18][19][20][23][24][25][27][28][29][30][31]43,46,50,51], and avoiding the homogenisation anneals that are required to remove the interdendritic segregation that occurs in single crystals of nickel-based superalloys grown by directional solidification, again potentially producing cost savings; . Complex net-shaped (but not re-entrant geometry) structures can, in principle, be processed, producing cost savings compared to directional solidification by avoiding the need for costly moulds and cores [13,66,75], see, for example, the hollow turbine blade with cooling holes shown in Figure 2 [75]; .…”
Section: Introductionmentioning
confidence: 99%
“…Directional recrystallization can be used to produce columnar grain structures that have grain boundaries roughly parallel to the direction of hot zone movement [1][2][3][4][5][6][7][8][9][10][11]. Besides this effect on the grain shape, marked changes in texture also occur during directional recrystallization.…”
Section: Introductionmentioning
confidence: 99%
“…A "stopper", a length of specimen run at a lower temperature, was used to differentiate two differently processed regions of the specimen [8]. Since long strips of nickel (>250 mm) were used, five or six different velocities could be examined per strip.…”
Section: Introductionmentioning
confidence: 99%
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