High nickel corrosion resistant alloys are called as
Hastelloy grades. Hastelloy alloys are not just high strength materials in fact
many of them keep such as high level of their room temperature strength at very
high temperatures that structural applications at high temperatures are not atypical.
Their strengths are variable depending on chemistry and form however normally
these alloys have tensile strengths about 100,000 psi and yield strengths of
about 50,000 psi. They are used basically for applications need outstanding corrosion
resistance. Modification of Hastelloy wire is performed by the
fabrication by forming and welding.
Hastelloy alloy B is significant for its exceptionally high
resistance to all concentrations of hydrochloric acid at temperatures up to the
boiling point. It is also resistant to other non-oxidizing acids and salts and
has significant high temperature properties in that it keeps over 2/3rd
of its room temperature strength at 1600oF in oxidizing conditions. It can be
used at high temperatures in reducing atmospheres. It should not be used for
firmly oxidizing acids or salts.
Hastelloy alloy C has an excellent resistance to oxidizing
solutions, particularly those containing chlorides, and hypochlorite solutions
and moist chlorine. It prevents nitric, hydrochloric and sulfuric acids at
average temperatures, has outstanding resistance to diverse corrosive organic
acids and salts and is resistant to oxidizing and reducing conditions up to
2000oF. It should not be used above 120oF in nitric and hydrochloric acid and
salt combinations.
Hastelloy X as outstanding strength and oxidation resistance
up to 2200oF and is significant for many industrial furnace applications for
its resistance to oxidizing, neutral and carburizing atmospheres. It has major applications
in aircraft components like jet engine tail-pipes, after-burners, turbines,
blades and vanes.
The line of demarcation between heat resistant alloys and super
alloys is rather tenuous as indefinite as the dividing line between ferrous and
nonferrous. Single phase alloys like Nichrome and Inconel alloy 600 are weak
above 1250oF however their high temperature strength and resistance to creep
are enhanced by the introduction of stable, hard phase or phases i.e. precipitated
carbides or intermetallic compounds. Most of the high nickel super alloys are
of the Aluminum-Titanium age-hardenable type. Chromium offers oxidation resistance
along with auxiliary strengthening. Columbium, molybdenum, tungsten and
tantalum are usually present to provide solid solution reinforcing of the
matrix. The major part of the strengthening at high temperatures, is because of
the precipitation of the Ni3(Al, Ti) compound, normally designated gamma prime
phase. Precipitation hardening significantly improves the stress-rupture properties of some
nickel base alloys.
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