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Transportation's Role in Reducing U.S. Greenhouse Gas Emissions ...

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Transportations <strong>Role</strong> <strong>in</strong> Reduc<strong>in</strong>g U.S. <strong>Greenhouse</strong> <strong>Gas</strong> <strong>Emissions</strong>: Volume 2<br />

passengers with a range of over 7,000 miles (IPCC, 1999; NASA, 1997), but smaller<br />

variations of the aircraft also are possible. Initially these aircraft will probably provide<br />

services to large and distant urban centers that are associated with dense air traffic, such<br />

as between New York and London or Los Angeles and Tokyo. Because of the unusual<br />

shape of these aircraft, changes <strong>in</strong> <strong>in</strong>frastructure will be required to accommodate these<br />

aircraft (ADL, 2000).<br />

Magnitude and Tim<strong>in</strong>g of GHG Reduction<br />

The application of drag-reduc<strong>in</strong>g surface films is anticipated to decrease fuel usage by up<br />

to 1.6 percent, while multilayer panels used to reduce surface friction across the w<strong>in</strong>g are<br />

expected to reduce fuel consumption and emissions between 6 to 10 percent. Use of w<strong>in</strong>g<br />

tip devices can reduce fuel use by 1.7 to 2 percent for blended w<strong>in</strong>glets (Morris, 2009,<br />

Reneaux, 2004) and up to 10 percent for spiroid w<strong>in</strong>glets applied to smaller aircraft<br />

(Ostrower, 2008). Additional test<strong>in</strong>g is be<strong>in</strong>g implemented for larger aircraft to quantify<br />

fuel consumption improvements associated with spiroid w<strong>in</strong>glets.<br />

Cost-Effectiveness<br />

As mentioned earlier, the high cost of fuel is anticipated to drive the development and<br />

application of these technologies, as they will reduce operat<strong>in</strong>g costs, although the costeffectiveness<br />

of each technology may vary. For example, w<strong>in</strong>g tip retrofit kits cost<br />

approximately $1 million to <strong>in</strong>stall, which would require less than six years to break even<br />

based on a fuel cost of $3.33 per gallon. The payback period for other technologies that<br />

have yet to be commercialized is uncerta<strong>in</strong>, as cost data are not readily available. Blended<br />

w<strong>in</strong>g bodies are anticipated to entail a considerable price premium of $30 to $60 million<br />

per aircraft, <strong>in</strong>clud<strong>in</strong>g development costs.<br />

Cobenefits<br />

S<strong>in</strong>ce these devices primarily improve efficiency at high speeds (i.e., high-altitude<br />

operation), any benefits <strong>in</strong> terms of pollutant reduction are not expected to be significant.<br />

Feasibility<br />

W<strong>in</strong>g tip devices are commercially available and require little assistance from the policymakers<br />

to promote their use. Accelerated adoption of w<strong>in</strong>g tip devices may be<br />

encouraged through voluntary programs such as the EPA’s SmartWay Program. Grooved<br />

adhesives and multi layer panels are likely to be less viable than other technologies<br />

presented <strong>in</strong> this section, due either to short lifetime (adhesives) or uncerta<strong>in</strong> benefits<br />

(panels).<br />

Tests of w<strong>in</strong>g design changes that reduce friction through lam<strong>in</strong>ar flow have been<br />

encourag<strong>in</strong>g, but at this time these designs have yet to be <strong>in</strong>corporated <strong>in</strong>to commercially<br />

available aircraft. Similarly, BWB aircraft have performed well <strong>in</strong> model tests<br />

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