dc.description.abstract |
Gas turbine engines for both aerospace and power generation are constantly being
revised to improve running efficiency and performance. Gas turbine engines
essentially consist of three distinct regions: compressor, combustion and turbine
sections with the combustor and turbine sections required to experience higher and
higher temperatures in pursuit of efficiency gains. Stage 1 high pressure turbine
blades (buckets) are located closest to the combustion zone and experience extremely
high temperatures. Further, turbine blades experience high centrifugal force whilst in
operation and therefore engine designers must take into consideration both the
mechanical effects o f operation and the high temperatures associated with engine use.
Environmental resistant coating systems are therefore employed to allow the design of
the base material (nickel-based superalloys) to be biased towards mechanical
properties (high creep resistance).
Nickel-platinum-aluminide coatings are the diffusion coating of choice for both aero-and
industrial turbines with the platinum being typically deposited by electroplating
on the nickel alloys, followed by heat treating to form a platinised enriched area
which is then aluminised by insertion into a chemical vapour deposition (CVD) retort
and reacting with an aluminium halide at elevated temperature. The CVD process is
utilised as it is relatively easy to form desirable intermetallics though this route.
The electrodeposition of aluminium from aqueous media is not possible as water
undergoes hydrolysis before the reduction potential of aluminium is reached. Ionic
liquids are an alternative method o f depositing aluminium via electroplating without
the need o f water as the electrolyte. Ionic liquids have numerous benefits including a
wide electrochemical window and have low toxicity. In comparison to the CVD
process, they are multiuse and can be easily recycled/reused as the ionic liquid itself is
not consumed within the plating process.
Electroplating aluminium from ionic liquids to form a dense coating onto nickelbased
superalloys is therefore proposed within this thesis as an alternative novel
approach to achieving desirable nickel aluminide intermetallic coatings after post
processing heat treatment. Furthermore, the post heat treatment may be done within
either a traditional CVD-type regime or with a new and novel low temperature heat
treatment regime developed as part of this thesis - ICON. Both heat treatments form
β-NiAl. The heat treatment using CVD-type parameters forms coatings akin to those
produced using a CVD route, whereas the ICON coating shows improved chemical
homogeneity and a smaller interdiffusion zone - both o f which are shown to offer
superior coating oxidation performance. Aluminium electrodeposited on CMSX4 heat
treated with CVD-type parameters shows excellent cyclic oxidation data which is at
least equal to, if not greater than those produced using traditional methods. |
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