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Figure 12.1 Historic <strong>and</strong> expected future trends in fuel efficiency for aircraft<br />

Energy intensity E i (MJ/ask)<br />

Source: Peeters, P. <strong>and</strong> Middel, J. (2006)<br />

Box 27 Engine <strong>and</strong> airframe technology<br />

UNWTO, 9 July 2008<br />

Mitigation Policies <strong>and</strong> Measures<br />

The expected advances in engine <strong>and</strong> airframe technology to date are: 672, 673, 674<br />

•<br />

•<br />

•<br />

•<br />

•<br />

4.0<br />

3.5<br />

3.0<br />

2.5<br />

2.0<br />

1.5<br />

1.0<br />

0.5<br />

development <strong>of</strong> gas turbine engines with a higher bypass <strong>and</strong> pressure ratios;<br />

optimisation <strong>of</strong> the balance between increasing fuel efficiency (i.e., through higher<br />

temperatures <strong>and</strong> pressure ratios) <strong>and</strong> reduced NOx emissions (by optimised combustion<br />

chambers <strong>and</strong> combustion control);<br />

higher lift-to-drag ratios by increasing wing-span, using, wing-tip devices, increased laminar<br />

flow on the wings <strong>and</strong> advanced airframe skin designs (e.g., riblets);<br />

structure weight reductions;<br />

new aircraft configurations for example the blended wing body.<br />

Alternative fuels<br />

Long-haul aircraft fuel efficiency<br />

0.0<br />

1940 1960 1980 2000 2020 2040 2060<br />

Year <strong>of</strong> market introduction<br />

Penner et al. (1999)<br />

Best fit regression<br />

A380<br />

Piston powered airliners<br />

B787<br />

Various aircraft using alternative fuels have recently been discussed. For instance, hydrogen powered<br />

aircraft would use a clean source <strong>of</strong> energy. However, neither Boeing nor Airbus are currently developing<br />

such an aircraft, <strong>and</strong> it should also be noted that hydrogen is a secondary energy, rather an energy<br />

carrier; i.e., unless it is produced from carbon-neutral primary energy sources there will be no global<br />

reduction in GHG emissions. Producing hydrogen from renewable sources is also constrained by lack<br />

<strong>of</strong> infrastructure, considerably higher costs, <strong>and</strong> competing uses <strong>of</strong> renewable energy. Furthermore,<br />

using liquid hydrogen in conventional turbojets would eliminate CO 2 <strong>and</strong> particle emissions but not<br />

reduce the problem <strong>of</strong> NO x -emissions, <strong>and</strong> it would also lead to the release <strong>of</strong> larger quantities <strong>of</strong> water<br />

vapour (about 2.6 times). Both would cause additional radiative forcing (see Box 23, Chapter 11).<br />

Currently available bi<strong>of</strong>uels are not suitable for use in aviation, except in a very low mix ratio with jet<br />

fuel. Aviation fuels must stay liquid at low temperatures, <strong>and</strong> also have a high energy content by volume.<br />

Fuels such as biodiesel or ethanol do not match these requirements well. However, a bi<strong>of</strong>uel tailored for<br />

aviation could possibly be developed in the future. Virgin Atlantic in partnership with Boeing aims to<br />

develop such a fuel within the next five years. Nevertheless, several problems remain unsolved regarding<br />

147

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