Elsevier

Transport Policy

Volume 34, July 2014, Pages 36-51
Transport Policy

The potential of future aircraft technology for noise and pollutant emissions reduction

https://doi.org/10.1016/j.tranpol.2014.02.017Get rights and content

Abstract

The negative external impacts of aviation are currently under unprecedented scrutiny. In response, a number of studies into future prospects for improvement have recently been carried out. This paper reviews these studies and discusses their combined implications for emissions of carbon dioxide, oxides of nitrogen, and noise. The results are also compared with targets for emissions reduction proposed by ACARE and NASA. It is concluded that significant future gains are achievable, but not to the extent implied by the ACARE and NASA targets, which represent an unrealistically optimistic view of technological potential over the next 20–40 years. The focus on technological advance also deflects attention from the substantial benefits available from combining present-day technology with behavioural change. Finally, difficult policy decisions will be necessary; the greatest benefits are associated with technological developments that will require major, and long-term, investment for their realisation, and there will be increasing conflict between environmental and noise goals.

Introduction

The introduction of jet-propelled passenger transport aircraft 55 years ago ushered in an era of unprecedented human mobility. Equally, it was associated with noise and local air quality issues that were painfully obvious to those living near airports. Today, these aircraft emissions are regulated, with benefits that are immediately evident to the naked eye and ear when vehicles from the two eras are compared directly. Unfortunately, however, much of this improvement is offset by the huge increase in air traffic over the intervening period. As a result, pressure to reduce noise and local chemical pollutants (specifically oxides of nitrogen, or ‘NOx’) remains high.

In addition, early jet engines were extremely inefficient; they displaced propellors nonetheless because of their ability to deliver thrust at high flight speed with low weight. Historically, their efficiency was not seen as an environmental problem, and the only driver for improvements was fuel cost. Now, however, with carbon dioxide (CO2) from the combustion of fossil fuel recognised as the dominant source of climate change, there is also societal pressure. As a result, the negative external impacts of mass air travel are under scrutiny as never before.

In 2001, recognising this situation, the Advisory Council for Aviation Research and Innovation in Europe (ACARE) published a ‘vision’ for 2020 (European Commission, 2001); this set targets of 50% reductions in fuel-burn and perceived noise, and 80% in landing/take-off NOx emissions, relative to year-2000 aircraft. With both Airbus’ and Boeing’s plans to this date now established, it has become clear that these targets will not be achieved. They have been replaced by a new set, ‘FlightPath 2050’ (European Commission, 2011), which calls for reductions of 75%, 65% and 90% respectively by 2050. In the U.S., similar goals have been proposed by NASA for the ‘N+2’ (service-entry 2025) and ‘N+3’ (service-entry 2030–2035) generations of aircraft (Collier, 2012). These are summarised, along with their ACARE counterparts, in Table 1. (Note that CAEP 6 and Stage 4 are regulatory levels; they are explained in Section 2.) Associated with this activity has been a surge in studies into future mitigation prospects, many of which invoke either radical technology developments or novel aircraft configurations.

The time is thus ripe to take stock, and this is the aim of the current paper. In particular, we seek to review the potential of technological advances in the aircraft itself, in the light of ACARE’s and NASA’s stated goals. At this point, it should be recognised that some contribution towards the fuel-burn and noise targets is envisaged from operational improvements, via elimination of air-traffic-management inefficiencies and alterations to landing approach procedures (see Reynolds, this ssue). Aspects of the latter that are relevant to the regulatory noise measures targeted by ACARE and NASA are accounted for in the studies reported here. Efficiency gains in air-traffic management are typically not; however they have progressively less impact as the fuel-burn target becomes more aggressive. (For example, if 5% of current fuel consumption is due to air-traffic-management inefficiencies, and 60% reduction is required, the aircraft-alone reduction must be 58%.) We will therefore compare predicted technological benefits directly with the targets.

As a final point, one could question the use of fuel consumption as a metric. Emissions of the associated pollutant, CO2, can also be reduced via the use of alternative fuels (see Hileman and Stratton, this issue). This issue, however, is outside the scope of the current review.

The structure of the paper is as follows. We first consider the relevant pollutants, and the factors influencing their generation. Then, in Section 3, we describe the studies reviewed here. Section 4 presents a comparative analysis of the studies, in order to identify areas of agreement, and of inconsistency. This then forms the basis for a discussion of future prospects, in Section 5. Our conclusions are summarised in Section 6.

Section snippets

Background

Aircraft emit a number of pollutants, of which three—CO2, NOx, and noise—have received most attention to date. This section reviews production mechanisms and historical trends for each in turn.

Future aircraft concepts

As we have seen, aircraft fuel-burn, NOx generation and noise have reduced significantly since the onset of large-scale commercial aviation. Furthermore, in the cases of fuel-burn and noise at least, historical evidence of diminishing returns suggests that most of the straightforward possible improvements have already been made. Nonetheless, ACARE and NASA have put forward targets that, in broad terms, require advances of comparable magnitude again, on all three fronts, within 40 years at most.

Carbon dioxide

The absence of regulatory standards for this category means that there is no single established metric for aircraft fuel consumption. Furthermore, even when direct comparison between different studies is possible, there may be considerable disagreement in absolute numerical values. (For example, both the CRC and MIT N+3 studies use the Boeing 737-800 as a reference, and there is sufficient information in the former to derive the payload fuel efficiency for comparison with the value given by the

Discussion

This section is split into two parts. In the first, we present our assessment of the studies described here, and their implications. In the second we move from the question of what could happen to what, in our opinion, should happen. The views expressed here, albeit inevitably personal and partial, were refined during TOSCA project discussions with industry experts, whose generosity with their valuable background knowledge we gratefully acknowledge.

Conclusions

In this paper, we have discussed the potential contribution of future technology to reducing the levels of three key aircraft emissions: carbon dioxide, oxides of nitrogen, and noise. Aerosols, the other significant concern, have not been addressed, on the basis that their effect is currently too uncertain to warrant its influencing design decisions. Consideration has also been limited to the aircraft itself; air-traffic-control-related measures and alternative fuels have been excluded as they

Acknowledgements

The authors are grateful to the following for their help in granting and/or obtaining copyright permissions: Ed Greitzer, Kenneth Martin, Linda Nicol, Sophie Schlingemann.

References (28)

  • E. Torenbeek

    ‘Cruise performance and range predictions reconsidered’

    Prog. Aerosp. Sci.

    (1997)
  • Bonet, J.T., 2012. Boeing ERA N+2 advanced vehicle concept results. Oral Presentation at the 50th AIAA Aerospace...
  • Bradley, M.K., Droney, C.K., 2011. Subsonic Ultra Green Aircraft Research: Phase I Final Report....
  • Bruner, S. et al., 2010. NASA N+3 Subsonic Fixed Wing Silent Efficient Low-Emissions Commercial Transport (SELECT)...
  • Collier, F.S., 2012. NASA Aeronautics Environmentally Responsible Aviation Project. Oral Presentation at the 50th AIAA...
  • DGAC, 2012. Noise Certification Database’. Online Database Hosted at...
  • Dowling, A.P., 2007. The Silent Aircraft Initiative – Overview. AIAA-2007-0452, Presented at 45th AIAA Aerospace...
  • Drake, A., 2012. NASA Environmentally Responsible Aviation (ERA) N+2 Advanced Vehicle Study. Oral Presentation at the...
  • European Commission, 2001. European Aeronautics: A Vision for 2020, Office for Official Publications of the European...
  • European Commission

    Flightpath 2050: Europe’s Vision for Aviation

    (2011)
  • Frota, J. et al., 2011. NACRE Final Activity Report 2005–2010. NACRE Project Report;...
  • J.E. Green

    Greener by design – the technology challenge

    Aeronaut. J.

    (2002)
  • Greitzer, E.M., et al., 2011. N+3 Aircraft Concept Designs and Trade Studies, Final Report....
  • C.A. Hall

    Low noise engine design for the Silent Aircraft Initiative

    Aeronaut. J.

    (2009)
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    Present address: Department of Aeronautical and Automotive Engineering, Loughborough University, Leicestershire LE11 3TU, UK.

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