| Summary: | The aspects of gas turbine design that are explored herein are focussed on
reduction or elimination of carbon dioxide (CO2) emissions and reduction of noise.
There are 3 separate but related investigations.
1. Aero gas turbine engine thermodynamic cycles for subsonic transport
aircraft are explored to optimise performance (thus reducing CO2 emissions) and to
minimise noise; particular attention is paid to choices of fan pressure ratio, bypass
ratio, installation configuration and fan design. Turbofans with long and short
cowls are explored, as are propfans of various bypass ratios. The performance
and noise comparisons of the engines are made using consistent technology
standards; this approach is not apparently available in the literature. It is shown
that relative to present day engines, useful improvements in Direct Operating Cost
(DOC), fuel burn and noise are possible. It is shown, not surprisingly, that the
optimum installed engine cycles for performance and noise are different.
2. The performance effects of using hydrogen fuel in “conventional”
aero gas turbine engines are discussed. Also, some novel un-conventional
hydrogen fuelled aero gas turbine cycles are examined. Hydrogen fuelled engines
create no emissions of CO2; however, this environmental benefit is partly offset by
the increased water in the engine contrails. It is shown that “conventional” engines
benefit from using hydrogen fuel, measured by the thrust obtained for a given fuel
energy input rate. The novel un-conventional configurations that are examined
offer useful performance benefits, including significant power increases, by suitable
use of the cold “sink” and high pressure of the liquid hydrogen fuel.
3. Two ways of eliminating CO2 emissions from industrial gas turbines
are examined. The first is by use of hydrogen-rich fuel. There are performance
gains, as with the aero engines; however in the industrial cases, the hydrogen is
sometimes produced in such a way that it is mixed with substantial amounts of
nitrogen, which significantly influences the results. The second is the use of CO2 in
the working fluid for partially-closed and closed cycle arrangements. This permits
easy sequestration of excess CO2 without the use of the large separating
equipment that is necessary for extracting CO2 from the exhausts of standard open
cycle plants breathing air. The changes required to a standard gas turbine to allow
it to use CO2 as its working fluid are explored in some detail; this is not clearly
addressed in the literature. It is shown that the turbines - the most expensive part
of the gas turbine - can be operated satisfactorily but changes are sometimes
required to the compressors.
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