Heat resistant alloys are group of alloys used in the
different industrial sectors-
Aerospace engine, stationary gas turbines, oil and gas and
medical.
The characteristics that make them suitable materials are:
·
Retention of strength and hardness as high
temperatures
·
Corrosion resistance
Heat resistant alloys are divided in three categories-
nickel based, iron based and cobalt based alloys. The physical properties and
machining behaviour of each varies significantly due to the chemical nature of
the alloy and the precise metallurgical processing it receives during
production. Whether the metal is annealed or aged is specifically effective on
the after machining characteristics.
Nickel based alloys are commonly used and presently make
about 50% of weight of advanced aircraft engines. Commonly used alloys in Heat engines are Inconel 718 wire, Inconel 625 and solution strengthened
nickel alloys.
Iron based materials are developed from austenitic stainless
steels. Some have low thermal expansion coefficient that make them suitable for
shafts, rings and casings. But they lack in hot strength properties such as
A286.
Cobalt based alloy show hot corrosion resistance at high
temperature as compare to nickel based alloys. They are costlier and also more
difficult to machine because of their extreme wearability. The application in
turbines is limited to combustion parts in the hottest engine regions. Their
main application is observed in surgical implants that use their inherent
corrosion resistance.
With above wide range of materials in the generic name of
heat resistant alloys, the machining behaviour widely varies even in the same
class of alloys. Actually same material can have different machining recommendations.
Material processing condition
The form of heat treatment affects the hardness of the
component and thus the wear mechanism. The development of the chip is a good
sign of the hardness with hard materials it is easier to crack the chip.
Hardened materials have increased cutting temperatures and
show a potential to notching of the cutting edge at the depth of cut. The
combination of a low entering angle and a hard substrate with a heat barrier
coating is needed. Softer materials machine in a similar way to the stainless
steel family.
Insert grades with greater toughness and decreased hot
hardness, resistance to high temperatures, are needed due to reduced cutting
temperatures and increased chip hammering. The damage to areas outside the real
cutting edge is caused by the chip breaking against the insert. Considering the
size, shape and strength requirements of the component, different production
methods for the empty material will be used. The production methods depends
used depends on the machinability of the material and will alter the wear
characteristics.
These raw material types directly affect the microstructure
of an alloy and also its after machining behaviour.
Forged materials have a finer grain size as compared to in
castings that enhances the strength and grain flow of the component. When
machining forgings, decreasing the speed and increasing the feed normally gives
the maximum feasible metal removal rate with good tool life.
The opposite rule is applied in castings and using low feeds
ad higher speeds can be advantageous. Castings have poor machinability and tend
to be most sensitive to notch wear and abrasive wear. They can be easily
recognized due to their visibly mottled surface.
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