dc.description.abstract |
In the light of global warming, the associated socio economical consequences, and
the projected shortage of natural energy resources and ever rising oil prices, this
thesis examines the potential for unconventional aero engine architectures to reduce
fuel consumption of passenger aircraft. Current aircraft engines are based on
the Brayton cycle, where the working fluid successively experiences isentropic
compression, isobaric combustion, and isentropic expansion. Deviations from the
ideal cycle in real engines occur through component inefficiencies. The maximum
achievable thermodynamic efficiency of the Brayton cycle increases hand in hand
with its peak cycle temperature. Since the peak cycle temperature is limited by
material properties of the turbine, the maximum cycle efficiency of current jet engines
is limited by the laws of thermodynamics. Hence, efficiency improvements
of jet engines beyond what is possible with conventional turbofan designs are only
feasible through unconventional engine architecture.
Several technologies enabling unconventional engine architectures for aircraft
propulsion have been identified. They include wave rotor, pulse detonation and
internal combustion. These technologies are merged with conventional jet engine
technology to form hybrid designs. A one dimensional engine performance model
was developed to calculate the performance and allow a comparison of the hybrid
cycles with a conventional turbofan cycle. Gradient optimisation techniques were
applied to the allow comparison of the best possible designs. Results suggest that
of the examined cycles, the hybrid internal combustion cycle has the best potential
for fuel savings compared to conventional turbofan cycles. |
en_UK |