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Haynes 242

Source£ºhttp://www.zytcsteel.com Time£º2023/3/11 16:16:38 View£º

HAYNES 242 alloy (UNS N10242) is an age-hardenable nickel-molybdenum chromium alloy which derives its strength from a long-range ordering reaction upon aging. It has tensile and creep strength properties up to 1200 - 1300¡ãF (649 - 704¡ãC) which are as much as double those for solid solution strengthened alloys, but with high ductility in the aged condition. The thermal expansion characteristics of 242 alloy are much lower than those for most other alloys, and it has very good oxidation resistance up to 1500¡ãF (816¡ãC). Other attractive features include excellent low cycle fatigue properties, very good thermal stability, and resistance to high-temperature fluorine and fluoride environments.  HAYNES® 244® alloy has been developed as an upgrade from 242 alloy, with enhanced tensile and creep properties up to 1400¡ãF (760¡ãC), as well as a lower coefficient of thermal expansion.

HAYNES 242 alloy is produced in the form of reforge billet, bar, plate, sheet, and wire welding products, all in various sizes. Other forms may be produced upon request.

Applications

HAYNES 242 alloy combines properties which make it ideally suited for a variety of component applications in aero and industrial gas turbine engines. It may be used for seal rings, containment rings, duct segments, casings, fasteners, rocket nozzles, pumps, and many others. In the chemical process industry, 242 alloy will find use in high-temperature hydrofluoric acid vapor-containing processes as a consequence of its excellent resistance to that environment. The alloy also displays excellent resistance to high-temperature fluoride salt mixtures. The high strength and fluorine environment-resistance of 242 alloy has also been shown to provide for excellent service in fluoroelastomer process equipment, such as extrusion screws.

 

Chemical Composition:

 

Element

Content (%)

Nickel, Ni

58

Molybdenum, Mo

24-26

Chromium, Cr

7-9

Cobalt, Co

2.50

Iron, Fe

2

Manganese, Mn

0.80

Silicon, Si

0.80

Copper, Cu

0.50

Aluminum, Al

0.50

Carbon, C

0.030

Boron, B

0.0060

 

Mechanical Properties:

Properties

Metric

Imperial

Tensile strength

1290 MPa

187000 psi

Yield strength (@strain 0.200%)

845 MPa

123000 psi

Elastic modulus

229 GPa

33200 ksi

Elongation at break (in 4D)

33.70%

33.70%

Reduction of area

45.70%

45.70%

Hardness, Brinell (converted from Vickers hardness)

257

257

Hardness, Knoop (converted from Vickers hardness)

286

286

Hardness, Rockwell C (converted from Vickers hardness)

19

19

Hardness, Vickers

271

271

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