Inconel 718 is an alloy of nickel-chromium-niobium- molybdenum
that has high corrosion resistance, strength and excellent fabrication
characteristics. This alloy has high tensile strength and excellent yield &
creep-rupture properties at high temperatures. This alloy can operate at
cryogenic temperatures up to 1200°F. Inconel718 wire has applications in valves, springs, aircraft and land-based
turbine engines. This alloy is used by various industries including nuclear,
automotive, oil, nuclear, gas, defense and aerospace.
Nickel-based superalloys such as Inconel 718 are used in nuclear,
aerospace and chemical industries due to their excellent mechanical and
chemical properties at elevated temperatures. Nickel-based superalloys compose
over half of the materials used in the aerospace industry, in particular for
the hot section of gas turbine engines for components such as blades, turbine
disk, combustors etc. Inconel 718 has low thermal conductivity that increases
the thermal effects during machining. Inconel 718 often exhibits strong
work-hardening behavior, high adhesion characteristic onto the tool face
altering cutting process parameters completely when machining. This alloy may
contain hard abrasive particles and carbides that create excessive tool wear
and hence the surface integrity of the end products can be disappointing.
Electrical discharge machining (EDM) is a competitive alternative
process to machine Inconel 718 as compared to mechanical cutting. EDM can
machine titanium alloys, hardened steels, cemented carbide and conductive
ceramics regardless of their strength and hardness. It allows machining of
complex part geometry. The tool electrode does not rotate for material removal,
holes with sharp corners and irregular contours can be conveniently machined by
EDM unlike mechanical cutting and grinding. The low force nature in the EDM gap
also allows the machining of thin and flexible parts, deep grooves and holes
that otherwise are difficult to machine by milling. The machining accuracy and
surface finish are high especially at trim cutting conditions despite the low
machining efficiency of EDM. These unique process characteristics make EDM an
enabling technology in aerospace, medical device, tool and automotive
industries.
Wire-EDM is widely used as it can be fully automated and flexible
in making complex geometrical shapes in one setup. This process capability is
particularly essential for aero-engine manufacture.
High temperature has
significant impact on the process-induce surface integrity including
microstructure change, microhardness, surface topography, residual stress and
element distributions as EDM is a thermal dominant process. The heat affected
zone (HAZ) with a white layer is associated with high tensile residual stress,
porosity, microcracks, grain growth and alloying from the tool electrode or
dielectric fluid. As per a recent study, wire-EDM is highly detrimental to
surface integrity compared to hard turning and grinding. However, this is not
necessarily true since the degree of thermal damage depends on not only process
conditions but also EDM generators. Thermal damage in main cut can be removed
or minimized by subsequent multiple trim cuts at reduced discharge energy.
Relaxation pulse with low energy has been tried to improve surface quality in
EDM of silicon carbide. It has shown that machining sequence with trim cut and
polishing technology is necessary to guarantee surface integrity. Thermal
damage by EDM may be minimized with the development of low energy generators
and EDM strategy.
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