There are essential differences in the structure and service
conditions of industrial and aero-gas turbines that prevent the direct use of
standard alloys in the design of industrial engines. Different alloys are used.
Blades for industrial gas turbines are often made from super alloys containing high
chromium concentration that have been evaluated for service in vigorous
conditions whilst those for aero gas engines are made from low carbon high
strength alloys.
Blades made for industrial gas turbines are significantly larger
than those for aero-engines. It results into significant differences in the
process factors during directional solidification that could influence the
structural and properties of the casting. In specific, slow heat flow through
larger castings will influence the cooling rate and the larger mass of molten
metal could cause issues in the containment by current moulding materials.
Industries demand longer lives from the aero-gas turbines
that requires better corrosion resistance. Practical engine trials that are
significant in the evaluation of aero engines, are impractical for industrial
gas turbines, consequently suitable component design by using materials
required for service in the required environment.
The industrial gas turbines are made from alloy that is
directionally solidified by using lab and commercial observation. The operation
of industrial gas turbines with specific emphasis on long term properties and
on both the anisotropy and heterogeneity of the castings.
A major part of the turbine design is the selection or development
of alloys suitable for application in the turbine. As long as candidate alloys
are chosen, basic tests are performed on the alloys that are already selected
such as nickel base super alloys Inconel 617. These alloys have very high
strength and oxidation resistance at atmospheric pressure.
Initial oxidation tests are performed on the test materials
to ensure that they can perform properly and can benefit the boiler research.
Higher heating value also signifies the performance of alloys. Ferritic
stainless steels comprising of 9 to 12% are presently used at steam
temperatures up to 600oC. Most studies of the upper temperature limit are up to
650oC with high temperature strength as a limiting factor.
Austenitic stainless steels keep their strength at higher
temperature as compare to ferritic alloys. Although vigorous thermal fatigue
issues prevented their regular use at the original design temperatures and
pressures. As thermal fatigue becomes more a problem in thicker component
parts, austenitic alloys are still useful in the specific thinner components. They
are used in boiler sections of advanced power stations.
Advancements in the application materials have contributed
in a major way in the development of gas turbine engines with higher power
ratings and efficiency levels. Enhancements in the design of gas turbine
engines over the years have been possible due to the development f materials with
improved performance. Gas turbines are widely used in aircraft engines and land
based applications for power production.
The major use of Inconel wire made from alloy 617 is in the improvement of
high temperature creep rupture strength without affecting oxidation and
corrosion resistance. It is commonly used in manufacturing combustion system
components for higher creep rupture strength.