X6CrNiTi18-10
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X6CrNiTi18-10Chemical composition:
Cr | Ni | Mo | Ti | C | Mn | Si | P | N | Fe | |
Min | 17 | 9 | – | 5x(C+N) | – | – | 0.25 | – | – | Bal |
Max | 19 | 12 | 0.75 | 0.7 | 0.08 | 2 | 1 | 0.045 | 0.1 |
X6CrNiTi18-10Physical properties:
Density | Melting point |
0.286 lb/in³ | 2550 – 2600°F |
X6CrNiTi18-10Mechanical properties:
Average high-temperature tensile properties
Temperature, °F | 68 | 400 | 800 | 1000 | 1200 | 1350 | 1500 |
Ultimate tensile strength, ksi | 93.3 | 73.6 | 69.5 | 63.5 | 52.3 | 39.3 | 26.4 |
0.2% yield strength, ksi | 36.5 | 36.6 | 29.7 | 27.4 | 24.5 | 22.8 | 18.6 |
The average stress at break
Temperature,°F | 1050 | 1100 | 1150 | 1200 | 1250 | 1300 | 1350 | 1400 | 1450 | 1500 |
1000hour,ksi | 34 | 29 | 22 | 17.5 | 13 | 11.5 | 7.5 | 6.5 | 5 | 4 |
10000hour,ksi | 27.5 | 22 | 16 | 12.5 | 9 | 7 | 5 | 4 | 3 | 2.5 |
100000hour,ksi | 21.5 | 15 | 10.5 | 7.5 | 5 | 4 | 3.5 | 2.5 | 2.3 | 2 |
X6CrNiTi18-10Stainless steel characteristics:
Oxidation resistance 1600°F
Prevents intergranular corrosion in the weld heat-affected zone (HAZ).
Resistant to polysulfuric acid stress corrosion cracking
X6CrNiTi18-10Uses of stainless steel:
Aircraft piston engine manifolds
Expansion joints, thermal oxidants
Refinery equipment
High-temperature chemical process equipment
Relevant standards:
ASTM: A 240, A 276, A 312, A 479 GE: B50T1181
ASME: SA-240, SA-276, SA-312, SA-479
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