Type
Analysis
Element
|
Min
|
Max
|
Carbon
|
--
|
0.08
|
Manganese
|
--
|
0.30
|
Silicon
|
--
|
0.50
|
Sulfur
|
--
|
0.01
|
Nickel + Cobalt
|
70.0 min
|
Chromium
|
14.0
|
17.0
|
Iron
|
5.00
|
9.00
|
Aluminum
|
0.40
|
1.00
|
Titanium
|
2.25
|
2.70
|
Copper
|
--
|
0.50
|
Cb + Ta
|
0.70
|
1.20
|
Description
Alloy X-750 is a
precipitation-hardenable alloy which has been used in applications
such as high temperature structural members for gas turbines, jet
engine parts, nuclear power plant applications, heat-treating
fixtures, forming tools, and extrusion dies. The alloy is highly
resistant to chemical corrosion and oxidation and has high
stress-rupture strength and low creep rates under high stresses at
temperatures up to 1500°F (816°C) after suitable heat
treatment.
Corrosion
Resistance
Alloy X-750 has excellent resistance
to chloride ion stress-corrosion cracking. It exhibits satisfactory
resistance to numerous oxidizing environments. The alloy has similar
corrosion resistance to alloy 600 in many media.
Physical
Properties
Density
lb/cu in...................................... 0.300
kg/cu m...................................... 8303
Melting Range
°F........................................ 2540/2600
°C.........................................1393/1427
Thermal Conductivity
Temperature
|
Btu-in/ft²-hr-°F
|
W/m-K
|
°F
|
°C
|
300 600 1000 1200 1400 1600
|
149 316 538 649 760 871
|
117 142 184 199 218 245
|
16.9 20.5 26.5 28.7 31.4 35.3
|
Electrical Resistivity
Condition
|
ohm-cir
mil/ft
|
microhm-mm
|
At Room
Temperature
|
Hot Rolled Solution
Treated Solution Treated and Aged
|
764 716
746
|
1270 1190
1240
|
Modulus of Elasticity
Temperature
|
psi
x 10(6)
|
MPa
x 10(6)
|
°F
|
°C
|
80 500 1000 1350 1500
|
26.7 260.0 538.0 732.0 816.0
|
31.0 28.7 25.0 21.0 18.5
|
213.7 197.9 172.4 144.8 127.6
|
Coefficient of Thermal Expansion
Temperature
Range
|
10(-6)/°F
|
10(-6)/°C
|
80°F to
|
26.7°C to
|
200 600 1000 1200 1600
|
93 316 538 649 871
|
6.7 7.5 7.9 8.1 9.0
|
12.1 13.5 14.2 14.6 16.2
|
Specific
Heat
|
Btu/lb-°F
|
kJ/kg-K
|
77/212°F
(25/100°C) 77/1650°F (25/899°C)
|
0.10-0.11 0.13
|
0.42-0.46 0.54
|
Heat
Treatment
Alloy X-750 is austenitic under all
conditions. The alloy is heat treated by several different methods
depending upon the application or requirement. Two common treatments
are: 1. For maximum creep, relaxtion and rupture strength at
temperatures above 1100°F (593°C): Solution Treatment -
2100°F (1149°C), 2 to 4 hrs, air cool. Intermediate Age
- 1550°F (843°C), 24 hrs, air cool. Final Age
-1300°F (704°C), 20 hrs, air cool. 2. For highest room
temperature yield strength and tensile ductility: Stress
Equaliztation - 1625°F (885°C), 24 hrs, air
cool. Precipitation Age - 1300°F (704°C), 20 hrs,
air cool.
Workability
The furnace temperature should be
2100°F (1149°C)-for optimal starting temperatures of
1950/2000°F. For service below 1100°F (593°C), higher
strength can be obtained by combining some cold work with heat
treatment because the effects are additive.
Machinabiliy Alloy X-750
work hardens quickly and is more difficult to machine than most
standard ferritic and martensitic alloys. The alloy is most easily
machined in the stress-equalized condition. Because specific cutting
forces are high, the machine tools used must have ample power and the
cutting speed should be slow. The tools must have smooth finishes, be
sharp, and be very rigid. To avoid work hardening , a continuous,
smooth cutting action should be maintained; thus, the machines must
have a minimum of backlash and the tool and workpiece must be rigidly
supported. If at all possible, avoid very small cuts and feeds.
Welding Alloy X-750 should
be welded in the stress-equalized condition, 1625°F (885°C)
heat treatment, and solution treated and age hardened after welding
has been completed. If this is not practical, the alloy should be
welded in the solution-treated condition and age hardened after
welding with or without the inclusion of a short-period
stress-relieving treatment at 1625°F. Weld joints, because of
softening of the alloy within the heat-affected zone, should be
located where lower creep properties are required.
Typical
Mechanical Properties
Room
Temperature Mechanical Properties
Temper
|
Tensile
Strength, psi
|
Yield
Strength 0.2% offset, psi
|
Elongation in
2", %
|
Hardness, Brinell
|
Hot-finished +
1300°F/20 hr,A.C
Hot-finished + Annealed 1800°F/1
hr, A.C + 1350°F/ 8 hr, F.C. 100°F/hr to 1150°F
(total 18 hr), A.C.
Hot-finished + 1625°F/24 hr, A.C
+ 1300°F/20 hr, A.C.
Cold-rolled, annealed + 1300°F/20
hr, A.C.
|
170,000-206,000
162,000-193,000
160,000-188,000
160,000-197,000
|
120,000-163,000
115,000-142,000
100,000-135,000
105,000-150,000
|
25-15
30-15
30-15
30-20
|
313-400
300-390
302-363
300-400
|
Bar Stock: Treatment #1 Solution treatment 2100°F (1149°C), 2 to 4 hrs., air cool intermediate age 1550°F (843°C), 24 hrs., air cool Final age 1300°F (704°C), 20 hrs., air cool
Test Temperature
|
Short-Time Tensile Properties Tests
|
°F
|
°C
|
Yield Strength 0.2% offset
|
Ultimate Tensile Strength
|
% Elongation in 2" (50.8 mm)
|
% Reduction of Area
|
ksi
|
MPa
|
ksi
|
MPa
|
70 1000 1200 1400 1500
|
21.1 538.0 649.0 760.0 816.0
|
92 83 82 68 45
|
634 572 565 469 310
|
161 140 120 80 47
|
1110 965 827 552 324
|
22 20 10 10 20
|
30 30 21 22 32
|
|