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ALLOY INDEX

Index Terms Links

A

16-25-6

broaching 197

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

electron beam welding 173

forgeability rating 93(T)

forging temperature 93(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

solid-solution-strengthened 20

specific heat capacity 246(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength of disks as function of year of

availability 343(F)

yield strength (0.2% offset) 13(T)

17-22-A

temperature-strength capability as function of

year of availability 340(F)

Vac degassed, temperature-strength capability as

function of year of availability 340(F)

19-9DL

annealing 137(T)

composition 4(T)

density 246(T)

descaling 210

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19-9DL (Cont.)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

strengthening mechanisms (as modified stainless

steel) 26

stress relieving 137(T)

thermal conductivity 247(T)

tensile elongation 13(T)

ultimate tensile strength 13(T)

welding and zinc removal 210

yield strength (0.2% offset) 13(T)

19-9W (AMS 5782), composition of filler metals

and electrode wires for arc welding 168(T)

A-286

aging cycles 140(T)

aircraft applications 91

annealing 137(T)

band sawing 190(T) 191(T)

broaching 196(F)

bulge forming, speed for 110(T)

carbon pickup 143

cold reduction effect on hardness 106 107(F)

cold work effect on yield strength 139(F)

composition 4(T)

composition of filler metals and electrode wires

for arc welding (AMS 5804) 168(T)

density 246(T)

draw forming, speed for 110(T)

drilling 190(T) 191(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

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A-286 (Cont.)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

electric arc furnace/argon oxygen decarburization

with electroslag remelting 45(T)

electron beam welding 173

end milling 190(T) 191(T)

energy required for forging 103 104

eta phase precipitation 362(F)

eta phase role in strengthening 225

face milling 190(F,T) 191(T)

forgeability 92

forgeability rating 93(T) 102(T)

forging, aircraft turbine shaft 99(F)

forging, design guides 95(T)

forging temperature 93(T) 102(T)

forging temperature range 103

forming by spinning from a roll forging 111(F)

forming, directionality in bulging 109(F)

gamma prime precipitation for strength 26

gamma prime solvus temperature 324(T)

incipient melting temperature 324(T)

liquating phase for liquation cracking 159(T)

machinability 191 192

mean coefficient of thermal expansion 247(T)

melting range 246(T)

microstructural degradation 329

mill product availability 77

precipitation hardening 214

reaming 190(T) 191(T)

reduction rate during forging 102

restraint fixturing for heat treatment 145

rupture strength vs. Larson-Miller

parameter 248(F)

rupture strength vs. temperature 243(F)

solution treating cycles 140(T)

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A-286 (Cont.)

solution treating temperature 147

specific heat capacity 246(T)

straddle milling 190(T) 191(T)

stress relieving 137(T)

stress-rupture strength 14(T) 19(F)

tapping 190(T) 191(T)

tensile elongation 13(T)

tensile forming, speed for 110(T)

thermal conductivity 247(T)

threading 190(T) 191(T)

turning 190(T) 191(T) 195

ultimate tensile strength 13(T)

useable temperature, versus Al/Ti ratio in PC

castings 216(T)

vacuum induction melting with electroslag

remelting 45(T)

vacuum induction melting with vacuum arc

remelting 45(T)

weldability 153

welding 151

yield strength of disks as function of year of

availability 343(F)

yield strength (0.2% offset) 13(T)

AF 21DA

aircraft applications 119

machinability ranking 192

AF21DA-6, composition of P/M

superalloys 120(T)

AF 56 (SX 792)

composition 273(T)

density 273(T)

AF 115

aircraft applications 119

composition of P/M superalloys 120(T)

AF 1753, carbide formation 37

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AiResist 13

composition 7(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

stress-rupture strength 19(F) 21(F)

tensile elongation 17(T)

ultimate tensile strength 17(T)

yield strength (0.2% offset) 17(T)

AiResist 213

composition 7(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

stress-rupture strength 19(F)

tensile elongation 13(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

AiResist 215

composition 7(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

stress-rupture strength 19(F) 21(F)

tensile elongation 17(T)

ultimate tensile strength 17(T)

yield strength (0.2% offset) 17(T)

AM1

composition 273(T)

density 273(T)

AM3

composition 273(T)

density 273(T)

hot isostatic pressing effect on high-cycle

fatigue (SCDS) 279(F)

AMS 5782. See also 199W.

composition of filler metals and electrode wires

for arc welding 168(T)

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AMS 5794. See also Multimet.

composition of filler metals and electrode wires

for arc welding 168(T)

AMS 5796. See also Haynes 25 (HS-25, L-605).

composition of filler metals and electrode wires

for arc welding 168(T)

AMS 5800. See also

composition of filler metals and electrode wires

for arc welding 168(T)

AMS 5804. See also A-286.

composition of filler metals and electrode wires

for arc welding 168(T)

AMS 5828C. See also Waspaloy.

composition of filler metals and electrode wires

for arc welding 168(T)

AP-1, fatigue crack growth rate, grain size

effect 254 256(F)

ASTM A297 grade HC

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HD

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HE

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HF

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HH

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HI

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

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ASTM A297 grade HK

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HL

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HN

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HP

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HT

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HV

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HW

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A297 grade HX

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A351 grade HK-30

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A351 grade HK-40

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A351 grade HT-30

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HD50

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

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ASTM A608 grade HE35

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HF30

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HH30

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HH33

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HI35

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HK30

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HK40

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HL30

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HL40

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HN40

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HT50

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HU50

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

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ASTM A608 grade HW50

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ASTM A608 grade HX50

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

Astroloy. See also Udimet 700 (U-700).

aerospace applications 120(T)

aging cycles 140(T)

aging rate 156(F)

aircraft applications 91 96 97(F) 118

annealing 137(T)

cobalt addition effect 240

composition 5(T)

cyclic fatigue behavior vs. mesh size

reduction 124

density 246(T)

drilling 198 199(F) 200

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

electrical resistivity 247(T)

elongation 249(T)

energy required for forging 104

extrusion 76

fatigue crack growth rate, grain size effect 254 256(F)

forgeability affected by nitrogen and oxygen

content 104

forgeability and elevated-temperature

strength 103

forgeability rating 93(T) 102(T)

forgeability vs. hardener content 103(T)

forged aircraft components 96 97(F)

forging, design guides 95(T)

forging developments 347

forging, development time requirement 104

forging temperature 93(T) 102(T)

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Astroloy (Cont.)

grain size 249(T)

hot cracking during forging 101

hot isostatic pressed (as-HIP), aircraft

applications 119

inertia bonding 175

low-cycle fatigue strength 252

mean coefficient of thermal expansion 247(T)

melting range 246(T)

microstructural degradation 329

powder metallurgy/isothermal forging 28

powder metallurgy processing 119

reduction in area 249(T)

reduction rate during forging 102

rupture strength vs. temperature 242(F)

solution treating cycles 140(T)

specific heat capacity 246(T)

strain-controlled low-cycle fatigue properties,

wrought 253(F)

strengthening mechanisms 28

stress relieving 137(T)

stress-rupture strength 14(T)

superplastic forging 114

temperature-strength capability as function of

year of availability 340(F)

tensile elongation 12(T)

thermal conductivity 247(T)

ultimate tensile strength 12(T) 249(T)

U-700 as variant of 239

yield strength (0.2% offset) 12(T) 249(T)

HIP Astroloy, strain-controlled low-cycle fatigue

properties 253(F)

LC Astroloy

aircraft applications 119

composition of P/M superalloys 120(T)

elongation 249(T)

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LC Astroloy (Cont.)

gamma prime solvus temperature 324(T)

grain size 249(T)

hub material for dual-alloy turbine wheel

concept 119

incipient melting temperature 324(T)

as P/M turbine disk alloys 127

prior particle boundaries corrected 119

reduction in area 249(T)

ultimate tensile strength 249(T)

vacuum (soluble gas) atomization process 122 123(F)

yield strength (0.2% offset) 249(T)

B

B-1900

aging cycles 141(T)

aircraft applications 261

aircraft applications, investment

casting 89

Al-Si coated, creep-rupture behavior 264(F)

carbide precipitation 224 362(F)

casting techniques lacking cost benefit 267

columnar grain directionally solidified, creep

behavior 270(F)

columnar grain directionally solidified,

elongation vs. temperature 279(F)

composition 6(T)

creep behavior 269 270(F)

creep elongations 263

creep-rupture strength 261 264(F)

density 262(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

ductility of cast version 263

dynamic modulus of elasticity 261(T)

forging, design guides 95(T)

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B-1900 (Cont.)

gamma prime solvus temperature 325(T)

hafnium addition effect 237

hot corrosion 302(F) 308

hot corrosion resistance 289

hot corrosion resistance from alloying

elements 304

hot corrosion resistance lacking 261

hot corrosion testing 292(F)

hot corrosion testing, specimen weight

change 292(F)

hot isostatic pressing 265

incipient melting temperature 325(T)

mean coefficient of thermal expansion 262(T)

mechanical properties of cast airfoils vs. cast test

bars 230 231(F)

melting range 262(T)

microstructural degradation with

overheating 328(F)

microstructure, carbides present 36(F)

microstructures after various heat treatments for

precipitation hardening 217(F)

molybdenum effect in hot corrosion 303

oxidation 297

polycrystalline, creep behavior 270(F)

polycrystalline, elongation vs.

temperature 279(F)

rupture strength vs. temperature 264(F)

solution treating cycles 141(T)

specific heat 262(T)

stress-rupture curve 259(F)

stress-rupture strength 18(T) 19(F) 20(F)

substituted for U-700 to prevent TMF

cracking 332

temperature-strength capability as function of

year of availability 340(F) 341(F) 350(F)

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B-1900 (Cont.)

tensile elongation 16(T)

thermal conductivity 262(T)

ultimate tensile strength 16(T)

variations developed 342

weld repair of 336

yield strength 239

yield strength (0.2% offset) 16(T)

B-1900+Hf

aging cycles 141(T)

gamma prime solvus temperature 325(T)

incipient melting temperature 325(T)

mechanical properties, cast test bars vs. cast

airfoils 230

solution treating cycles 141(T)

temperature-strength capability as function of

year of availability 341(F)

B-1910, wrought variant of B-1900, rolling 76

C

C263

aircraft applications 75(F) 76

combustor applications 75(F) 76

composition 5(T)

creep strength vs. temperature 75(F) 76

mill product availability 77

sheet product applications 75(F) 76

sheet products 91

yield strength vs. temperature 75(F) 76

Cabot 214

stress-rupture strength 14(T)

tensile elongation 12(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

CG-27, stress-rupture strength 19(F)

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CM-186LC

as columnar grain directionally solidified

alloy 267

cost 349

creep strength 272(F)

stress-rupture strength 260(F)

CM-247 (Ren 108) as columnar grain

directionally solidified alloy 267

CM-247LC (CGDS)

creep behavior 272

creep strength 272(F)

developed to eliminate grain-boundary

cracking 267

stress-rupture strength 260(F)

CMSX-2 (SCDS)

aging cycles 141(T)

cobalt addition effect 240

compliance constants vs. temperature 273(F)

composition 6(T) 273(T)

density 273(T)

fracture toughness for aerospace

applications 286

low-cycle fatigue behavior, thermal solidification

gradient, orientation and HIP effects 280 281(F)

as single-crystal directionally-solidified

alloy 267

solution treating cycles 141(T)

stress-rupture strength 18(T)

temperature-strength capability as function of

year of availability 350(F)

tensile elongation 17(T)

ultimate tensile strength 17(T)

yield strength (0.2% offset) 17(T)

CMSX-2/3 (SCDS)

creep behavior 272

stress-rupture strength 260(F)

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CMSX-3 (SCDS)

composition 273(T)

density 273(T)

gamma prime solvus temperature 325(T)

incipient melting temperature 325(T)

CMSX-4 (SCDS)

composition 6(T) 273(T)

creep strength 272(F)

density 273(T)

fracture toughness for aerospace

applications 286

as single-crystal directionally solidified

alloy 267

temperature range compared to CMSX-10 349

temperature-strength capability as function of

year of availability 350(F)

CMSX-6 (SCDS)

cobalt addition effect 240

composition 6(T) 273(T)

density 273(T)

as single-crystal directionally solidified

alloy 267

CMSX-10 (SCDS)

composition 6(T) 273(T)

creep strength 272(F)

density 273(T)

as single-crystal directionally solidified

alloy 267

temperature range and creep-rupture

strength 349

temperature-strength capability as function of

year of availability 350(F)

CMSX-11B (SCDS)

composition 273(T)

density 273(T)

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CMSX-11C (SCDS)

composition 273(T)

density 273(T)

CRM-6D, stress-rupture strength 19(F)

Custom Age 625 PLUS, composition 5(T)

D

D-6ac, face milling 190(F)

D-31 (Nb), face milling 190(F)

D-979

cold work effect on yield strength 139(F)

density 246(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

rupture strength vs. temperature 242(F)

specific heat capacity 246(T)

stress-rupture strength 14(T) 19(F)

tensile elongation 12(T)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Discaloy

aging cycles 140(T)

annealing 137(T)

composition 4(T)

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

rupture strength vs. temperature 243(F)

solution treating cycles 140(T)

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Discaloy (Cont.)

specific heat capacity 246(T)

stress relieving 137(T)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

DS 002

columnar grain directionally solidified, temperature-

strength capability as function of year of

availability, turbine blade alloys 343(F)

single-crystal directionally solidified, temperature-

strength capability as function of year of

availability, turbine blade alloys 343(F)

E

Elgiloy

density 246(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

F

FSX-414

composition 7(T)

density 262(T)

hot corrosion 308

mean coefficient of thermal expansion 262(T)

melting range 262(T)

specific heat 262(T)

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FSX-414 (Cont.)

stress-rupture curve 259(F)

stress-rupture strength 18(T)

tensile elongation 17(T)

thermal conductivity 262(T)

ultimate tensile strength 17(T)

yie ld strength (0.2% offset) 17(T)

G

GMR 235

composition of filler metals and electrode wires

for arc welding 168(T)

electron beam welding 173

as filler metal for IN-718 welds 167 169

friction welding 175

stress-rupture strength 18(T)

tensile elongation 17(T)

ultimate tensile strength 17(T)

yield strength (0.2% offset) 17(T)

Greek Ascoloy

stress-rupture strength 19(F)

temperature-strength capability as function of

year of availability 340(F)

H

Hastelloy B

composition 4(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

electron beam welding 173

temperature-strength capability as function of

year of availability 350(F)

Hastelloy B-2

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

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Hastelloy C

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

sheet

elongation 284(T)

reduction in area 284(T)

tensile strength 284(T)

yield strength 284(T)

Hastelloy C-22

tensile elongation 12(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Hastelloy C-276

composition 4(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

electric arc furnace/argon oxygen decarburization

with electroslag remelting 45(T)

Hastelloy G-30

tensile elongation 12(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Hastelloy N

composition 4(T)

electron beam welding 173

Hastelloy R-235, intergranular attack 295(F)

Hastelloy S

aging cycles 140(T)

composition 4(T)

composition of filler metals and electrode wires

for arc welding 168(T)

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

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Hastelloy S (Cont.)

as filler metal (AMS 5838), base metals

involved 167

as filler metal (AMS 5838) for IN-718

welds 167

mean coefficient of thermal expansion 247(T)

melting range 246(T)

mill annealing minimum temperature 160(T)

solution annealing temperature range 160(T)

solution treating cycles 140(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 12(T)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Hastelloy W

composition 4(T)

forgeability rating 93(T)

forging temperature 93(T)

Hastelloy X

aging cycles 140(T)

aircraft applications 75(F) 76

anisotropy 108(T)

annealing 137(T)

carbide precipitation 363(F)

carbides and overheating effect on mechanical

properties 326(F)

chromium content in alloy (%) 304(T)

cold reduction effect on hardness 107(F)

combustor applications 75(F) 76

composition 4(T) 6(T)

cost advantage 77

creep strength vs. temperature 75(F) 76

density 246(T)

descaling 210

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Hastelloy X (Cont.)

diffusion welding 174

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

electric arc furnace/argon oxygen decarburization

with electroslag remelting 45(T)

electron beam welding 173

Ericksen cup depth 108(T)

forgeability rating 93(T) 102(T)

forging, design guides 95(T)

forging temperature 93(T) 102(T)

forming and slotting 112

forming characteristics 108(T)

gamma prime solvus temperature 324(T)

heat treatment 146

hot corrosion 302(F)

hot corrosion resistance 304(T)

incipient melting temperature 324(T)

intergranular attack 295(F)

liquating phase for liquation cracking 159(T)

machinability 193

manufacturing ratings 194(T)

manufacturing time for part production 194(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

microstructure, carbide precipitation 329 330(F)

mill annealing minimum temperature 160(T)

mill product availability 77

Olsen cup depth 108(T)

orange peel in forming 107

oxide penetration 295(F)

precipitation hardening 213

reduction rate during forging 102

rupture strength of wrought solid-solution-

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Hastelloy X (Cont.)

strengthened nickel-base superalloys vs.

temperature 244(F)

rupture strength vs. temperature 242(F)

sheet product applications 75(F) 76

sheet products 91

solid-solution strengthened 28

solution annealing temperature range 160(T)

solution treating cycles 140(T)

specific heat capacity 246(T)

stress relieving 137(T)

stress-rupture strength 14(T) 19(F)

temperature-strength capability as function of

year of availability 340(F)

tensile elongation 12(T)

tensile elongation vs. cold work for sheet 76(F)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

UNS number 108(T)

yield strength (0.2% offset) 12(T)

yield strength (0.2% offset) vs. cold work for

sheet 76(F)

yield strength vs. temperature 75(F) 76

Haynes alloys

density 246(T)

melting range 246(T)

specific heat capacity 246(T)

Haynes 21 (HS -21)

composition 7(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

electron beam welding 173

stress-rupture strength 18(T) 19(F) 21(F)

temperature-strength capability as function of

year of availability 350(F)

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Haynes 25 (HS -25, L-605)

aging cycles 140(T)

alloying elements effect on formability 106

annealing 137(T)

band sawing 191(T)

brazing 183 184(T)

bulge forming, speed for 110(T)

carbide precipitation 223 329

chromium content in alloy (%) 304(T)

composition 4(T) 7(T)

composition of filler metals and electrode wires

for arc welding 168(T)

density 246(T)

descaling 208

draw forming, speed for 110(T)

drilling 191(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

end milling 191(T)

explosive forming 113(F)

face milling 191(T)

as filler metal for welding 151

forgeability rating 93(T)

forging 104

forging temperature 93(T)

gamma prime solvus temperature 324(T)

G-ratio 193

hot corrosion resistance 304(T)

incipient melting temperature 324(T)

machinability 193

machinability ranking 192

manufacturing ratings 194(T)

manufacturing time for part production 194(T)

mean coefficient of thermal expansion 247(T)

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Haynes 25 (HS -25, L-605) (Cont.)

melting range 246(T)

mill annealing minimum temperature 160(T)

mill product availability 77

precipitation hardening 213

reaming 191(T)

rupture strength vs. Larson-Miller

parameter 248(F)

rupture strength vs. temperature 243(F)

sheet products 91

solution annealing temperature range 160(T)

solution treating cycles 140(T)

specific heat capacity 246(T)

straddle milling 191(T)

strengthening mechanisms 29

stress relieving 137(T)

stress-rupture strength 14(T) 19(F) 21(F)

tapping 191(T)

tensile elongation 13(T)

tensile elongation vs. cold work for sheet 76(F)

tensile forming, speed for 110(T)

thermal conductivity 247(T)

threading 191(T)

turning 191(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

yield strength (0.2% offset) vs. cold work for

sheet 76(F)

Haynes 31, mill product availability 77

Haynes 95 (N-155)

annealing 137(T)

stress relieving 137(T)

Haynes 150

density 246(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

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Haynes 150 (Cont.)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Haynes 151 (HS -151), stress-rupture

strength 19(F) 21(F)

Haynes 188

aging cycles 140(T)

aircraft applications 75(F) 76

aircraft applications, components in F-100

engines 76(T)

alloying elements effect on formability 106

anisotropy 108(T)

cold reduction effect on hardness 106 107(F)

combustor applications 75(F) 76

composition 4(T)

composition of filler metals and electrode wires

for arc welding 168(T)

creep-buckling resistance 76(T)

creep life 76(T)

creep strength vs. temperature 75(F) 76

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

Ericksen cup depth 108(T)

forgeability rating 93(T)

forging temperature 93(T)

forming characteristics 108(T)

gamma prime solvus temperature 324(T)

higher-temperature alternative to Hastelloy X 77

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Haynes 188 (Cont.)

high-temperature strength 76(T)

hot corrosion 302(F)

incipient melting temperature 324(T)

lanthanum inclusions, effect on oxidation 297

low-cycle fatigue strength 76(T)

mean coefficient of thermal expansion 247(T)

microstructure, carbide precipitation after

overheating 327(F)

mill annealing minimum temperature 160(T)

mill product availability 77

Olsen cup depth 108(T)

oxidation resistance 76(T)

oxidation resistance improved by aluminide

coating 314

rupture strength vs. Larson-Miller

parameter 248(F)

rupture strength vs. temperature 243(F)

sheet product applications 75(F) 76

sheet products 91

solution annealing temperature range 160(T)

solution treating cycles 140(T)

stress-rupture strength 14(T)

temperature-strength capability as function of

year of availability 340(F)

tensile elongation 13(T)

tensile elongation vs. cold work for sheet 76(F)

thermal conductivity 247(T)

thermal fatigue 76(T)

ultimate tensile strength 13(T)

UNS number 108(T)

welding 151

yield strength (0.2% offset) 13(T)

yield strength (0.2% offset) vs. cold work for

sheet 76(F)

yield strength vs. temperature 75(F) 76

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Haynes 214

alloying elements effects on formability 106

cold reduction effect on hardness 107(F)

composition 4(T)

mill product availability 77

Haynes 230

alloying elements effects on formability 106

anisotropy 108(T)

cold reduction effect on hardness 107(F)

composition 4(T)

density 246(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

Ericksen cup depth 108(T)

forming characteristics 108(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

mill annealing minimum temperature 160(T)

Olsen cup depth 108(T)

solution annealing temperature range 160(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 12(T)

tensile elongation vs. cold work for sheet 76(F)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

UNS number 108(T)

yield strength (0.2% offset) 12(T)

yield strength (0.2% offset) vs. cold work for

sheet 76(F)

Haynes 242, composition 5(T)

Haynes 263, composition 5(T)

Haynes 556

aging cycles 140(T)

composition 4(T)

composition of filler metals and electrode wires

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Haynes 556 (Cont.)

for arc welding 168(T)

density 246(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

solution treating cycles 140(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Haynes 1002

density 262(T)

dynamic modulus of elasticity 261(T)

mean coefficient of thermal expansion 262(T)

melting range 262(T)

specific heat 262(T)

tensile elongation 17(T)

thermal conductivity 262(T)

ultimate tensile strength 17(T)

yield strength (0.2% offset) 17(T)

Haynes HR-120, composition 4(T)

Haynes HR-160, composition 4(T)

Haynes R-41, composition 5(T)

Haynes Stellite 31 (HS -31, X-40). See also

X-40 1

electron beam welding 173

grinding fluid effect on grinding ratio 202(T)

HIP Astroloy. See entry after Astroloy.

I

IN-120, magnesium addition effect on stress-

rupture behavior 238(T)

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IN-162

density 262(T)

dynamic modulus of elasticity 261(T)

mean coefficient of thermal expansion 262(T)

melting range 262(T)

specific heat 262(T)

stress-rupture strength 18(T)

tensile elongation 16(T)

thermal conductivity 262(T)

ultimate tensile strength 16(T)

yield strength (0.2% offset) 16(T)

IN 591, temperature-strength capability as function

of year of availability 350(F)

IN-731

density 262(T)

mean coefficient of thermal expansion 262(T)

melting range 262(T)

specific heat 262(T)

stress-rupture strength 18(T)

tensile elongation 16(T)

thermal conductivity 262(T)

ultimate tensile strength 16(T)

yield strength (0.2% offset) 16(T)

IN 935, temperature-strength capability as function

of year of availability 350(F)

IN-939

aging cycles 141(T)

aircraft applications 227 261

cast in case-type components 348

hot corrosion 308

hot corrosion resistance 307

for industrial and marine turbines 263

oxidation, amorphous silica effect 351(F)

oxidation-resistance potential 351

solution treating cycles 141(T)

stress-rupture strength 18(T)

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IN-939 (Cont.)

temperature-strength capability as function of

year of availability 350(F)

tensile elongation 17(T)

ultimate tensile strength 17(T)

yield strength (0.2% offset) 17(T)

IN 6201, temperature-strength capability as

function of year of availability 350(F)

IN 6202, temperature-strength capability as

function of year of availability 350(F)

IN 6203, temperature-strength capability as

function of year of availability 350(F)

Inco alloy 330

creep-rupture strength 241

rupture strength of wrought solid-solution-

strengthened nickel-base superalloys vs.

temperature 244(F)

INCO 728

hot corrosion testing 292(F)

hot corrosion testing, specimen weight

change 292(F)

Incoloy 800

annealing 137(T)

cold reduction effect on hardness 107(F)

composition 4(T)

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

rupture strength of wrought solid-solution-

strengthened nickel-base superalloys vs.

temperature 244(F)

specific heat capacity 246(T)

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Incoloy 800 (Cont.)

stress relieving 137(T)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Incoloy 800H

annealing 137(T)

composition 4(T)

strengthening mechanis ms 26

stress relieving 137(T)

Incoloy 800HT

composition 4(T)

rupture strength of wrought solid-solution-

strengthened nickel-base superalloys vs.

temperature 244(F)

Incoloy 801

composition 4(T)

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Incoloy 802

composition 4(T)

density 246(T)

drilling hole sizes 199(T)

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Incoloy 802 (Cont.)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

rupture strength of wrought solid-solution-

strengthened nickel-base superalloys vs.

temperature 244(F)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Incoloy 807

density 246(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Incoloy 825

annealing 137(T)

density 246(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

stress relieving 137(T)

tensile elongation 13(T)

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Incoloy 825 (Cont.)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Incoloy 901

annealing 137(T)

composition 5(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

fine grain, temperature-strength capability as

function of year of availability 340(F)

forgeability rating 93(T)

forging, grain-size variations 104

forging temperature 93(T)

gamma prime precipitation for strength 26

high-cycle fatigue, grain size effect 257(T)

high-cycle fatigue, surface

condition effect 257(T)

low-cycle fatigue, grain size effect 251 252(T)

machinability ranking 192

microstructural degradation 329

precipitation hardening 214

stress relieving 137(T)

stress-rupture strength 19(F)

temperature-strength capability as function of

year of availability 340(F)

Incoloy 903

composition 4(T)

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

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Incoloy 903 (Cont.)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Incoloy 904

density 246(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

thermal conductivity 247(T)

Incoloy 907

composition 4(T)

density 246(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Incoloy 909

composition 4(T)

density 246(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

strengthening mechanisms 28

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

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Incoloy 909 (Cont.)

ultimate tensile strength 13(T)

yield strength (0.2% offset) 13(T)

Incoloy 925

composition 4(T)

electric arc furnace/argon oxygen decarburization

with electroslag remelting 45(T)

Incoloy MA-956

brazing 183

as common ODS alloy 129

composition 129(T) 132

creep-rupture strength 243(F) 244(F)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

electrical resistivity 250(T)

elongation (%) 250(T)

grain structure 132

heat treatment industry applications 133

mean coefficient of thermal expansion at

538 C 250(T)

melting range 250(T)

1000h rupture strength 250(T)

product forms available 132(T)

reduction in area at 1095C 250(T)

rupture strength of wrought solid-solution-

strengthened nickel-base superalloys vs.

temperature 244(F)

rupture strength vs. temperature 243(F)

sheet form available 132

specific heat capacity at 21 C 250(T)

thermal conductivity at 21 C 250(T)

ultimate tensile strength 250(T)

yield strength 250(T)

Inconel alloys

descaling 208(T)

development 1 339

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Inconel alloys (Cont.)

nitrogen pickup 143(F)

sheet products 91

solid-solution-strengthened 20

Inconel 82, as filler metal for IN-718 welds 167

Inconel 100 (IN -100)

aerospace applications 120(T)

aging cycles 141(T)

aircraft applications 261

aircraft applications, investment casting 89

applications, high-temperature 23

availability 342

casting techniques lacking cost benefit 267

centrifugal atomization for P/M processing 122

chromium content in alloy (%) 304(T)

chromium content low for turbine disk

applications 344

cobalt addition effect 240

columnar grain directionally solidified, creep

behavior 270(F)

columnar grain directionally solidified,

elongation vs. temperature 279(F)

composition 5(T) 6(T)

composition of P/M superalloys 120(T)

creep behavior 269 270(F)

data compilation 261 263

density 262(T)

drilling 200

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 261(T)

elongation 249(T)

forging, development time requirement 104

forging temperatures 102

gamma-gamma prime eutectic, white islands

of 360(F)

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Inconel 100 (IN -100) (Cont.)

gamma prime solvus temperature. 324(T) 325(T)

gatorized, rupture strength vs.

temperature 242(F) 264(F)

grain size 249(T)

G-ratio 193

hot corrosion 302(F) 308

hot corrosion resistance 289 304(T)

hot corrosion resistance from alloying

elements 304

hot corrosion testing 292(F)

hot corrosion testing, specimen weight

change 292(F)

incipient melting temperature 324(T) 325(T)

machinability 192

mean coefficient of thermal expansion 262(T)

mechanical properties, cast test bars vs. cast

airfoils 230

melting range 262(T)

microstructural degradation 329

Mod, temperature-strength capability as function

of year of availability 340(F)

physical property data not available 241

polycrystalline, creep behavior 270(F)

polycrystalline, elongation vs.

temperature 279(F)

polycrystalline, temperature-strength capability as

function of year of availability, turbine blade

alloys 343(F)

powder metallurgy form, yo-yo heat

treatment 217

powder metallurgy/isothermal forging 28

powder metallurgy processing 117 119 342

powder metallurgy processing and forging 102

as powder metallurgy turbine disk alloys 127

powder processing with superplastic

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Inconel 100 (IN -100) (Cont.)

forming 115

precipitation hardening 214

reduction in area 249(T)

rupture strength vs. temperature 264(F)

sigma phase formation 362(F)

solution treating cycles 141(T)

specific heat 262(T)

strain-controlled low-cycle fatigue

properties 253(F)

stress-rupture curve 259(F)

stress-rupture strength 18(T) 19(F) 20(F) 272(F)

temperature-strength capability as function of

year of availability 340(F) 341(F) 350(F)

tensile elongation 16(T)

tensile strength, and conversion from cast to

wrought form 243

tensile strength, cast vs. wrought forms 227

tensile yield strength 278(F)

thermal conductivity 262(T)

ultimate tensile strength 16(T) 249(T)

vacuum (soluble gas) atomization

process 122 123(F)

vanadium effect in hot corrosion 303

yield strength 239

yield strength (0.2% offset) 16(T) 249(T)

Inconel 102

composition 5(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

magnesium addition effect on creep rupture

life 238

Inconel 117, composition of filler metals and

electrode wires for arc welding 168(T)

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Inconel 587

dynamic modulus of elasticity 245(T)

stress-rupture strength 14(T)

tensile elongation 12(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Inconel 596, dynamic modulus of

elasticity 245(T)

Inconel 597

density 246(T)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 12(T)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Inconel 600

aging cycles 140(T)

annealing 137(T)

bar, elongation 284(T)

bar, reduction in area 284(T)

bar, tensile strength 284(T)

bar, yield strength 284(T)

brazing 182

cold reduction effect on hardness 107(F)

composition 4(T)

density 246(T)

descaling 210

diffusion welding 174

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

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Inconel 600 (Cont.)

electric arc furnace/argon oxygen

decarburization with electroslag

remelting 45(T)

electron beam welding 173

filler metals used for welds 167

forgeability 104

forgeability rating 93(T)

forging temperature 93(T)

liquating phase for liquation cracking 159(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

rupture strength of wrought solid-solution-

strengthened nickel-base superalloys vs.

temperature 244(F)

rupture strength vs. temperature 242(F)

solution treating cycles 140(T)

specific heat capacity 246(T)

stress relieving 137(T)

stress-rupture strength 14(T)

temperature-strength capability as function of

year of availability 340(F)

tensile elongation 12(T)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Inconel 601

aging cycles 140(T)

annealing 137(T)

composition 4(T)

composition of filler metals and electrode wires

for arc welding 168(T)

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

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Inconel 601 (Cont.)

electrical resistivity 247(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

rupture strength of wrought solid-solution-

strengthened nickel-base superalloys vs.

temperature 244(F)

rupture strength vs. temperature 242(F)

solution treating cycles 140(T)

specific heat capacity 246(T)

stress relieving 137(T)

stress-rupture strength 14(T)

tensile elongation 12(T)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Inconel 617

aging cycles 140(T)

aircraft applications 75(F) 76

combustor applications 75(F) 76

composition 4(T)

composition of filler metals and electrode

wires for arc welding 168(T)

creep strength vs. temperature 75(F) 76

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

gamma prime solvus temperature 324(T)

incipient melting temperature 324(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

microstructure, incipient melting effect 326(F)

mill annealing minimum temperature 160(T)

mill product availability 77

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Inconel 617 (Cont.)

rupture strength of wrought solid-solution-

strengthened nickel-base superalloys vs.

temperature 244(F)

sheet product applications 75(F) 76

solution annealing temperature range 160(T)

solution treating cycles 140(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 12(T)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

yield strength vs. temperature 75(F) 76

Inconel 625

aging cycles 140(T)

anisotropy 108(T)

annealing 137(T)

cast, density 262(T)

cast, mean coefficient of thermal

expansion 262(T)

cast, melting range 262(T)

cast, specific heat 262(T)

cast, thermal conductivity 262(T)

composition 4(T)

density 246(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

electric arc furnace/argon oxygen decarburization

with electroslag remelting 45(T)

electron beam welding 173

Ericksen cup depth 108(T)

forming characteristics 108(T)

gamma prime solvus temperature 324(T)

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Inconel 625 (Cont.)

incipient melting temperature 324(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

mill annealing minimum temperature 160(T)

mill product availability 77

Olsen cup depth 108(T)

rupture strength vs. temperature 242(F)

solid-solution-strengthened 28

solution annealing temperature range 160(T)

solution treating cycles 140(T)

specific heat capacity 246(T)

stress relieving 137(T)

stress-rupture strength 14(T) 18(T)

tensile elongation 12(T) 16(T)

tensile elongation vs. cold work for sheet 76(F)

thermal conductivity 247(T)

ultimate tensile strength 12(T) 16(T)

UNS number 108(T)

vacuum induction melting with electroslag

remelting 45(T)

vacuum induction melting with vacuum arc

remelting 45(T)

yield strength (0.2% offset) 12(T) 16(T)

yield strength (0.2% offset) vs. cold work for

sheet 76(F)

Inconel 690

annealing 137(T)

density 246(T)

electrical resistivity 247(T)

mean coefficent of thermal expansion 247(T)

melting range 246(T)

specific heat capacity 246(T)

stress relieving 137(T)

thermal conductivity 247(T)

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Inconel 700

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

electron beam welding (not U-700) 173

face milling 190(F)

forgeability rating 93(T)

forging temperature93(T)

Inconel 702

composition 5(T)

weldability as function of aluminum and

titanium hardener content 155(F)

Inconel 706 (IN -706)

aging cycles 140(T)

composition 5(T)

composition of P/M superalloys 120(T)

density 246(T)

development 343

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

eta phase disposed, fatigue life affected 253(F)

forged billets, elongation 284(T)

forged billets, reduction in area 284(T)

forged billets, tensile strength 284(T)

forged billets, yield strength 284(T)

forging, fracture toughness 285(T)

forging, roo m-temperature yield strength 285(T)

forging-weldment, fracture toughness 285(T)

forging-weldment, room-temperature yield

strength 285(T)

gamma double-prime phase effect on

strengthening 226

gamma double-prime precipitate 34

mean coefficient of thermal expansion 247(T)

melting range 246(T)

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Inconel 706 (IN -706) (Cont.)

niobium as gamma prime strengthener 154

no PWHT cracking 155

postweld heat treat cracking of welds 154

solution treating cycles 140(T)

specific heat capacity 246(T)

strengthening mechanisms 28

stress-rupture strength 14(T)

tensile elongation 12(T)

tensile properties 12(T) 283 284(T) 285(T)

thermal conductivity 247(T)

ultimate tensile strength 12(T)

vacuum induction melting with electroslag

remelting 45(T)

vacuum induction melting with electroslag

remelting and vacuum arc remelting 45(T)

vacuum induction melting with vacuum arc

remelting 45(T)

yield strength (0.2% offset) 12(T)

Inconel 713 (IN -713)

aging cycles 141(T)

aircraft applications 261

applications, high-temperature 23

chromium content in alloy (%) 304(T)

cobalt addition effect 240

development 339 341

friction welding 175

hot corrosion 304 305(F)

hot corrosion resistance 304(T)

hot corrosion resistance, aluminide-type coating

applied 311

investment casting, polycrystalline 89

nickel-aluminide-type coating effect on hot

corrosion resistance 304 305(F)

solution treating cycles 141(T)

strengthening mechanisms 28

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Inconel 713 (IN -713) (Cont.)

temperature-strength capability as function of

year of availability 340(F) 341(F)

IN-713C

composition 6(T)

density 262(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 261(T)

electron beam welding 173

friction welding 175

gamma prime solvus temperature 325(T)

incipient melting temperature 325(T)

mean coefficient of thermal expansion 262(T)

melting range 262(T)

oxidation 297

rupture strength vs. temperature 264(F)

specific heat 262(T)

stress-rupture curve 259(F)

stress-rupture strength 18(T) 19(F)

tcp phases formed 357

temperature-strength capability as function of

year of availability 350(F)

temperature-strength capability as function of

year of availability, turbine blade

alloys 343(F)

tensile elongation 16(T)

thermal conductivity 262(T)

ultimate tensile strength 16(T)

yield strength (0.2% offset) 16(T)

IN-713 Hf

stress-rupture strength 18(T)

tensile elongation 17(T)

ultimate tensile strength 17(T)

yield strength (0.2% offset) 17(T)

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Inconel 713LC (IN-713LC)

aircraft applications 261

composition 6(T)

density 262(T)

dynamic modulus of elasticity 261(T)

gamma prime solvus temperature 325(T)

incipient melting temperature 325(T)

mean coefficient of thermal expansion 262(T)

melting range 262(T)

specific heat 262(T)

stress-rupture strength 18(T)

tensile elongation 16(T)

thermal conductivity 262(T)

ultimate tensile strength 16(T)

yield strength (0.2% offset) 16(T)

Inconel 718 (IN -718)

aerospace applications 248

aging cycles 140(T) 141(T)

aging rate 156(F)

aircraft applications 24 152 227

annealing 137(T)

availability 24

bar, elongation 284(T)

bar, fracture toughness 285(T)

bar, reduction in area 284(T)

bar, room-temperature yield strength 285(T)

bar, tensile strength 284(T)

bar, yield strength 284(T)

brazing 183

carbide precipitation 361(F)

cobalt addition effect 240

cogging 75

composition 5(T) 6(T)

composition of filler metals and electrode wires

for arc welding 168(T)

composition of P/M superalloys 120(T)

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Inconel 718 (IN -718) (Cont.)

cost 8 24

cost of materials for destructive test

methods 346

delta, gamma and gamma double-prime

phases 361(F)

delta phase role in preventing stress-rupture

embrittlement 225 (F)

delta phase role in strengthening 225 (F) 227(T)

delta solvus 75

density 246(T)

diffusion welding 174

discrete white spots 64 65(F)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

electron beam welding 173

elongation 249(T)

explosive forming 112(F)

fatigue crack growth rate 253 (F)

fatigue crack growth rate, environment

effects 255 257(F)

as filler metal for IN-718 welds 167

fine grain forged 103

forgeability 24

forgeability rating 93(T) 102(T)

forging 97 98(F)

forging, bands caused by too high

temperature 99 102(F)

forging, design guides 95(T)

forging, elongation 284(T)

forging, fracture toughness 285(T)

forging, GTA weld in, elongation 284(T)

forging, GTA weld in, reduction in area 284(T)

forging, GTA weld in, tensile strength 284(T)

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Inconel 718 (IN -718) (Cont.)

forging, GTA weld in, yield strength 284(T)

forging prior to peeling the billet surface 64(F)

forging, room-temperature yield strength 285(T)

forgings, reduction in area 284(T)

forgings, tensile strength 284(T)

forging temperature 93(T) 99 101(F) 102(T)

forging to three distinctly different

structures 103

forging-weldment, fracture toughness 285(T)

forging-weldment, room-temperature yield

strength 285(T)

forging, yield strength 284(T)

freckle structure 41(F)

friction welding 175

gamma double-prime phase 27

gamma double-prime precipitate 34 218

gamma prime precipitation for strength 26

grain size 249(T)

grain size prediction by mo deling 347

G-ratio 193

hardening retarded 155(F)

heat treatment 136 245 248 251(F)

high strength (HS), tensile and stress-rupture

properties 249 251(F)

homogenization of cast product 73(F)

ingot-metallurgy 348

investment casting 80

for large structural castings 348

lead content effect on tensile properties 234 236(F) 237(T)

liquation cracking 157 158(F)

low-cycle fatigue strength 251

machinability ranking 192

magnesium addition effect on stress-rupture

ductility 238

mean coefficient of thermal expansion 247(T)

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Inconel 718 (IN -718) (Cont.)

melting range 246(T)

microstructural degradation 329

microstructure 33(F)

mill product availability 77

mushy-zone thickness vs. ingot diameter 43(F)

niobium as gamma prime strengthener 154

niobium content 41(F) 43

no PWHT cracking 155

notch ductility lacked 218

notch sensitivity 226 227(T)

overaged, crystal structure and 27(T)

postweld heat treat cracking of welds 154

precipitation hardening 212

process modeling of remelt ingots 345

production size capability 343

pseudobinary phase diagram 41 42(F) 43

reduction in area 249(T)

reduction rate during forging 102

rupture strength vs. temperature 242(F)

sheet, elongation 284(T)

sheet, GTA weld in, elongation 284(T)

sheet, GTA weld in, reduction in area 284(T)

sheet, GTA weld in, tensile strength 284(T)

sheet, GTA weld in, yield strength 284(T)

sheet, reduction in area 284(T)

sheet, tensile strength 284(T)

sheet, yield strength 284(T)

solidification white spots 65(F) 67(F)

solution treating cycles 140(T) 141(T)

solution treating temperature 147

specific heat capacity 246(T)

standard forged 103

standard heat treatment (STD) 248

standard heat treatment, tensile and stress-rupture

properties 249 251(F)

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Inconel 718 (IN -718) (Cont.)

strain-age (PWHT) cracking prevention 155

strengthening mechanisms 28

stress relieving 137(T)

stress-rupture strength 14(T) 19(F)

superplastic forming 113(F)

tensile elongation 12(T) 16(T)

tensile properties 244 249(T) 283 284(T)

285(T)

thermal conductivity 247(T)

time -temperature-transformation diagram 105(F)

tramp element concentrations allowable 235 237(T)

triple-melted ingot processing 72

ultimate tensile strength 12(T) 16(T) 249(T)

vacuum arc remelting 63(F)

vacuum induction melting with electroslag remelting 45(T)

vacuum induction melting with electroslag

remelting and vacuum arc remelting 45(T)

vacuum induction melting with vacuum arc

remelting 45(T)

weldability as function of aluminum and

titanium hardener content 155(F)

welding 149 151 186(F) 187

welding, filler metal choices 167 169

wrought form 2

yield strength of disks as function of year of

availability 343(F)

yield strength (0.2% offset) 12(T)

Inconel 718 Direct Age

forged 103

forged structure 105

stress-rupture strength 14(T)

tensile and stress-rupture properties 249 251(F)

tensile elongation 12(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

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IN-718 SPF

grain growth vs. time 113 114(F)

superplastic-formed product 113(F)

Inconel 718 Super

stress-rupture strength 14(T)

tensile elongation 12(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Inconel 721, composition 5(T)

Inconel 722, composition 5(T)

Inconel 725, composition 5(T)

Inconel 738 (IN -738)

aging cycles 141(T)

aircraft applications 261

composition 6(T)

density 262(T)

directionally solidified 343

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 261(T)

hot corrosion 302(F) 308

hot corrosion resistance 304 307

hot isostatic pressing, and stress-rupture

strength 265(F)

low-cycle fatigue behavior, atmosphere

effects 255 257(F)

mean coefficient of thermal expansion 262(T)

melting range 262(T)

rupture strength vs. temperature 264(F)

solution treating cycles 141(T)

specific heat 262(T)

stress-rupture curve 259(F)

stress-rupture strength 19(F) 20(F)

temperature-strength capability as function of

year of availability 350(F)

tensile elongation 16(T)

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Inconel 738 (IN -738) (Cont.)

thermal conductivity 262(T)

ultimate tensile strength 16(T)

yield strength (0.2% offset) 16(T)

IN-738C, stress-rupture strength 18(T)

IN-738LC

gamma prime solvus temperature 325(T)

hot isostatic pressing effect on creep

behavior 335(F)

incipient melting temperature 325(T)

stress-rupture strength 18(T)

weld repair of 336

Inconel X-750

aging cycles (AMS 5667) 140(T)

aging cycles (AMS 5668) 140(T)

annealing 137(T)

band sawing 191(T)

bar, elongation 284(T)

bar, reduction in area 284(T)

bar, tensile strength 284(T)

bar, yield strength 284(T)

cold reduction effect on hardness 107(F)

cold work effect on yield strength 139(F)

composition 5(T)

density 246(T)

descaling 210

drilling 191(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

electron beam welding 173

end milling 191(T)

face milling 191(T)

forgeability rating 93(T)

forged billet, GTA weld in, elongation 284(T)

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Inconel X-750 (Cont.)

forged billet, GTA weld in, reduction in

area 284(T)

forged billet, GTA weld in, tensile

strength 284(T)

forged billet, GTA weld in, yield

strength 284(T)

forging, fracture toughness 285(T)

forging, room-temperature yield strength 285(T)

forging temperature 93(T)

forging-weldment, fracture toughness 285(T)

forging-weldment, room-temperature yield

strength 285(T)

gamma prime solvus temperature 324(T)

incipient melting temperature 324(T)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

metallic contaminants for 203

mill product availability 77

reaming 191(T)

rupture strength vs. temperature 242(F)

sheet, elongation 284(T)

sheet, GTA weld in, elongation 284(T)

sheet, GTA weld in, reduction in area 284(T)

sheet, GTA weld in, tensile strength 284(T)

sheet, GTA weld in, yield strength 284(T)

sheet products 91

sheet, reduction in area 284(T)

sheet, tensile strength 284(T)

sheet, yield strength 284(T)

solution treating cycles (AMS 5667) 140(T)

solution treating cycles (AMS 5668) 140(T)

specific heat capacity 246(T)

straddle milling 191(T)

stress relieving 137(T)

stress-rupture strength 14(T) 19(F)

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Inconel X-750 (Cont.)

tapping 191(T)

tensile elongation 12(T)

tensile properties 283 284(T) 285(T)

thermal conductivity 247(T)

thermal treatments for precipitation hardening of

various forms 228 229(T)

threading 191(T)

turning 191(T)

ultimate tensile strength 12(T)

yield strength (0.2% offset) 12(T)

Inconel 751

composition 5(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

forgeability rating 93(T)

forging temperature 93(T)

Inconel 792 (IN -792)

aging cycles 141(T)

aircraft applications 261

applications, high-temperature 23

as columnar grain directionally solidified

alloy 267

columnar grain directionally solidified,

development 343

composition 6(T)

density 262(T)

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

gamma prime solvus temperature 325(T)

hot corrosion 308 309

hot corrosion resistance from alloying

elements 304

incipient melting temperature 325(T)

mean coefficient of thermal expansion 262(T)

melting range 262(T)

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Inconel 792 (IN -792) (Cont.)

SCDS, creep-rupture life, orientation effect 274 276(F)

SCDS, development 343

SCDS, high-angle boundaries effect on rupture

life 271(F)

solution treating cycles 141(T)

specific heat 262(T)

stress-rupture curve 259(F)

stress-rupture strength 18(T)

temperature-strength capability as function of

year of availability 350(F)

tensile elongation 16(T)

thermal conductivity 262(T)

turbine engine applications 267

ultimate tensile strength 16(T)

yield strength 239

yield strength (0.2% offset) 16(T)

Inconel 901 (IN -901)

aging cycles 140(T)

aircraft applications 91

density 246(T)

dynamic modulus of elasticity 245(T)

electrical resistivity 247(T)

elongation 233(T)

eta phase formation 363(F)

forgeability rating 102(T)

forging, design guides 95(T)

forgings, tensile properties of two test

coupons 232 233(T)

forging temperature 102(T)

gamma prime solvus temperature 324(T)

incipient melting temperature 324(T)

Laves phase formation 363(F)

mean coefficient of thermal expansion 247(T)

melting range 246(T)

nickel-base, eta phase role in strengthening 225

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Inconel 901 (IN -901) (Cont.)

reduction in area 233(T)

rupture strength vs. temperature 243(F)

solution treating cycles 140(T)

specific heat capacity 246(T)

stress-rupture strength 14(T)

tensile elongation 13(T)

thermal conductivity 247(T)

ultimate tensile strength 13(T) 233(T)

yield strength 233(T)

yield strength (0.2% offset) 13(T)

Inconel MA-754

aerospace applications 120(T)

aircraft applications 131 133

brazing 183

as common ODS alloy 129

composition 129(T) 132

creep-rupture strength 23

drilling hole sizes 199(T)

drilling speeds and feeds grouping 198(T)

electrical resistivity 250(T)

elongation 250(T)

gamma prime solvus temperature 325(T)

incipient melting temperature 325(T)

mean coefficient of thermal expansion at

538 C 250(T)

melting range 250(T)

nonradioactive dispersoid 132

1000h rupture strength MPa(ksi) 250(T)

as oxide-dispersion-strengthened alloy 28

plate production 131

product forms available 132(T)

production on a large scale 132