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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 />

For typical civil engines, CO <strong>and</strong> HC are relatively unchanged through <strong>the</strong> turbine <strong>and</strong> exhaust nozzle. However, <strong>the</strong>y can be reduced by up to two orders of magnitude<br />

in <strong>the</strong> turbine <strong>and</strong> exhaust nozzles (Godin et al., 1995, 1997; Leide <strong>and</strong> Stouffs, 1996; Lukachko et al., 1998) of advanced cycle military engines, where completion of<br />

oxidation in <strong>the</strong> high-temperature regions of <strong>the</strong> turbine results in <strong>the</strong> modest increases of CO 2 mentioned above. Measurements of <strong>the</strong>se species CO 2 <strong>and</strong> total<br />

hydrocarbons) are routine, <strong>and</strong> it is possible to measure <strong>the</strong>m to several percentage points accuracy (Katzman <strong>and</strong> Libby, 1975; Spicer et al., 1992, 1994; Dryer et al.,<br />

1993; Howard et al., 1996).<br />

Table 7-8: LTO cycle measurements for a high bypass GE (CF6-80) turbofan engine (ICAO, 1995b).<br />

Time in Mode<br />

Rated Output<br />

(F00)<br />

Fuel Flow<br />

(kg s-1 ) HC CO<br />

NOx SN<br />

0.7 mins. take-off 100% 2.353 0.08 0.52 28.06 7.1<br />

2.2 mins. climb out 85% 1.913 0.09 0.52 21.34 -<br />

4.0 mins. approach 30% 0.632 0.20 2.19 8.97 -<br />

26 mins. idle 7% 0.205 9.68 43.71 3.74 -<br />

Dp/F 00 (g kN -1 ) LTO cycle miss./rated output measured avg<br />

12.43 57.09 42.17<br />

Dp/F 00 (g kN -1 ) characteristic value to be regulated 16.2 65 46.4 8.3<br />

Current regulatory level 19.6 118 80.2 18.3<br />

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O<strong>the</strong>r reports in this collection<br />

http://www.ipcc.ch/ipccreports/sres/aviation/105.htm (4 von 4)08.05.2008 02:43:40<br />

IPCC Homepage

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