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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 />

Figure 7-28: The ICAO l<strong>and</strong>ing <strong>and</strong> take-off cycle (LTO).<br />

7.6.4.2. Secondary Combustion Products (NO, NO 2, N 2O, SO 2, CO, stable HC)<br />

Secondary products-such as NO, NO 2 , <strong>and</strong> SO 2 , as well as <strong>the</strong>ir oxidative products SO 3 , HONO, HNO 3 , <strong>and</strong> H 2 SO 4 -formed via reactions initiated with <strong>the</strong> reactive<br />

radicals OH <strong>and</strong> O are <strong>the</strong> principal participants of interest in chemical <strong>and</strong> microphysical processes occurring soon after emission. Although OH <strong>and</strong> O are reduced<br />

considerably by <strong>the</strong> engine exit, <strong>the</strong>y continue to play an important role in global atmospheric processes (see Chapters 2 <strong>and</strong> 3). To underst<strong>and</strong> <strong>the</strong> processes<br />

occurring through <strong>the</strong> engine, relative <strong>and</strong> absolute levels of <strong>the</strong>se secondary combustion products, <strong>the</strong>ir oxidative products (<strong>the</strong> acid gases), <strong>and</strong> <strong>the</strong> reactive radicals<br />

need to be accurately characterized. Emissions indices for NO x , CO, <strong>and</strong> HC, as measured by ICAO procedures for stages in a st<strong>and</strong>ard LTO cycle, are documented<br />

(ICAO, 1995b) for most in-use engines as part of <strong>the</strong> engine certification process; <strong>the</strong>se emissions typically correspond to tens to hundreds of ppmv. SO x O emissions<br />

are directly proportional to <strong>the</strong> level of sulfur in <strong>the</strong> fuel [a 400 ppmm fuel S level corresponds to an EI(SO x O) of 0.8]. Emissions of metals, whe<strong>the</strong>r from impurities in<br />

<strong>the</strong> fuel or engine wear, are much smaller than <strong>the</strong> emissions discussed here but may be of interest in soot activation <strong>and</strong> condensation processes (Chen et al., 1998;<br />

Twohy et al., 1998). NO x does not change significantly through <strong>the</strong> turbine <strong>and</strong> nozzle o<strong>the</strong>r than through changes resulting from dilution, although <strong>the</strong> NO 2 /NO ratio<br />

may shift as a result of increased oxidation. Oxidation of NO <strong>and</strong> NO 2 to HONO <strong>and</strong> HNO 3 , respectively, is predicted to be on <strong>the</strong> order of a few percent or less,<br />

occurring largely in <strong>the</strong> high-pressure turbine (Fahey et al., 1995a; Anderson et al., 1996; Lukachko et al., 1998). Although this change in <strong>the</strong> NO x level is not<br />

significant, changes in HONO <strong>and</strong> HNO 3 represent important changes in trace species of NOy (see below). Ground-based <strong>and</strong> in-flight measurements indicate that<br />

emissions of N 2 O are also small relative to NO x (Kleffmann et al., 1994; Fahey et al., 1995b). Fur<strong>the</strong>r validation of NO x chemistry is warranted, but indications are that<br />

current models can predict NO x evolution in <strong>the</strong> turbine <strong>and</strong> nozzle with sufficient accuracy for assessment needs (Dryer et al., 1993), <strong>and</strong> measurements of NO x with<br />

a few percent accuracy are possible.<br />

http://www.ipcc.ch/ipccreports/sres/aviation/105.htm (3 von 4)08.05.2008 02:43:40

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