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Aviation and the Global Atmosphere

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<strong>Aviation</strong> <strong>and</strong> <strong>the</strong> <strong>Global</strong> <strong>Atmosphere</strong><br />

produced over <strong>the</strong> ICAO l<strong>and</strong>ing/take-off cycle, which is intended to represent typical aircraft<br />

operations in <strong>the</strong> vicinity of <strong>the</strong> airport. The mass of each species (in grams) is divided by <strong>the</strong><br />

take-off thrust of <strong>the</strong> engine (in kilo Newtons) so that different size engines can be reasonably compared; thus, <strong>the</strong> resulting units are g kN-1. ICAO l<strong>and</strong>ing/take-off<br />

cycle, measurement procedures, <strong>and</strong> emissions st<strong>and</strong>ards are discussed fur<strong>the</strong>r in Section 7.7.1.<br />

Table 7-4: Typical basic performance <strong>and</strong> operational requirements of a modern aircraft engine combustor.<br />

Item Requirement Value Max/Min<br />

1 Combustion efficiency<br />

- At takeoff thrust (%)<br />

- Idle thrust (%)<br />

2 Low-pressure light-off capability (MPa) 0.03 (Max)<br />

3 Lean blowout fuel/air ratio (at low engine power conditions) 0.005 (Max)<br />

4 Ground light-off fuel/air ratio (with cold air, cold fuel) 0.010 (Max)<br />

5 Total pressure drop-compressor exit to turbine inlet (%) 5.0 (Max)<br />

6 Exit gas temperature distribution<br />

- Pattern factor<br />

0.25 (Max)<br />

- Profile factor<br />

0.11 (Max)<br />

7 Combustion dynamics [dynamic pressure range/inlet air pressure (%)] 3 (Max)<br />

8 Liner metal temperature (K) 1120 (Max)<br />

9 Cyclic life to first repair (cycles) 5000 (Min)<br />

Table 7-5: Combustion developments linked to emissions performance.<br />

Requirements* Emissions Implications <strong>and</strong> Compromise Required<br />

1, 8, <strong>and</strong> 9 Lowering of liner cooling flows improves "idle" efficiency (low HC <strong>and</strong> CO) <strong>and</strong> ability to reduce NOx but must be balanced against<br />

effect on liner temperatures <strong>and</strong> life/durability<br />

2, 3, <strong>and</strong> 4 Wide range of fuel/air ratios <strong>and</strong> long dwell times in combustor favor good light-off performance but must be balanced against need<br />

to control HC <strong>and</strong> CO emissions at low power <strong>and</strong> NOx formation rates at high power<br />

5 <strong>and</strong> 7 Low overall <strong>and</strong> dynamic pressure losses required to minimize SFC losses but must be balanced by need to retain good mixing for<br />

low emissions <strong>and</strong> good liner cooling<br />

6 Long mixing lengths improve exit profiles <strong>and</strong> pattern factors but require more cooling air <strong>and</strong> increase NOx formation times<br />

http://www.ipcc.ch/ipccreports/sres/aviation/101.htm (2 von 3)08.05.2008 02:43:34<br />

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