For Gas Turbine and Aerospace Applications Requiring Low Thermal Expansion, High-Strength, and Oxidation-Resistance
HAYNES242 alloy is a unique, age-hardenable alloy that combines relatively low thermal expansion characteristics with outstanding strength, fatigue-resistance, and oxidation resistance for service temperatures as high as 1400°F (760°C). It is ideally suited to use in seal rings, containment rings, duct segments, casings, fasteners, rocket nozzles, pumps, and many other components. 242® alloy has tensile and creep strength properties up to 1300°F (705°C). These properties are as much as double those of solid solution-strengthened alloys and are comparable to those of some precipitation-hardened super alloys.
242 alloy has excellent tensile ductility over the entire temperature range and superior, low-cycle fatigue strength. It is also readily formed and welded by conventional techniques. Although 242® alloy contains only 8% chromium, its oxidation resistance is sufficient to allow its use in an uncoated condition at temperatures as high as 1500°F (815°C). This attribute gives this alloy a real advantage over other low-expansion alloys.
Haynes alloy 242 is furnished in the annealed condition, unless otherwise specified. The alloy is usually annealed in the range of 1900-2050°F (925-1120°C),depending upon specific requirements, followed by an air cool (or more rapid cooling) before aging. A water quench is recommended for heavy section components..
Aging is performed at 1200°F (650°C) for a period of 24 hours, followed by an air cool.
Typical Tensile Properties, Plate
Test Temperature | 0.2%Yield Strength | UltimateTensile Strength | Elongation | |||
---|---|---|---|---|---|---|
°F | °C | ksi | MPa | ksi | MPa | % |
RT | RT | 110 | 760 | 179 | 1235 | 39 |
800 | 425 | 80 | 550 | 154 | 1060 | 44 |
1000 | 540 | 70 | 485 | 145 | 1000 | 47 |
1200 | 650 | 76 | 525 | 142 | 980 | 43 |
1400 | 760 | 42 | 290 | 106 | 730 | 66 |
1600 | 870 | 40 | 275 | 69 | 475 | 56 |
1800 | 980 | 28 | 195 | 41 | 285 | 65 |
Typical Rupture Strength, Plate
Test Temperature | Typical Rupture Properties: Stress Required to Produce Rupture in Hours Shown | ||||||
---|---|---|---|---|---|---|---|
10 h | 100 h | 1,000 h | |||||
°F | °C | ksi | MPa | ksi | MPa | ksi | MPa |
1000 | 540 | 160 | 1105 | 140 | 965 | 120 | 825 |
1100 | 595 | 130 | 895 | 110 | 760 | 93 | 640 |
1200 | 650 | 105 | 725 | 85 | 585 | 68 | 470 |
1300 | 705 | 80 | 550 | 63 | 435 | 43 | 295 |
1400 | 760 | 59 | 405 | 35 | 240 | 17 | 120 |
Typical Room Temperature Physical Properties
Physical Property | British Units | Metric Units |
---|---|---|
Density | 0.327 lb/in3 | 9.06 g/cm3 |
Electrical Resistivity | 48.0 µohm-in | 122.0 µohm-cm |
Modulus of Elasticity | 33.2 x 106 psi | 229 GPA |
Thermal Conductivity | 75.7 Btu-in/ft2-h-°F | 11.3 W/m-°C |
Specific Heat | 0.092 Btu/lb-°F | 386 J/Kg-°C |