Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-18574
Title: Nonvolatile particulate matter emissions of a business jet measured at ground level and estimated for cruising altitudes
Authors : Durdina, Lukas
Brem, Benjamin T.
Schönenberger, David
Siegerist, Frithjof
Anet, Julien G.
Rindlisbacher, Theo
et. al : No
Published in : Environmental Science & Technology
Publisher / Ed. Institution : American Chemical Society
Issue Date: 3-Oct-2019
License (according to publishing contract) : Licence according to publishing contract
Type of review: Peer review (publication)
Language : English
Subjects : Feinstaub; Luftfahrtemissionen; Luftqualität
Subject (DDC) : 363: Environmental and security problems
Abstract: Business aviation is a relatively small but steadily growing and little investigated emission source. Regarding emissions, aircraft turbine engines rated at and below 26.7 kN thrust are certified only for visible smoke and are excluded from the nonvolatile particulate matter (nvPM) standard. Here, we report nvPM emission characteristics of a widely used small turbofan engine determined in a ground test of a Dassault Falcon 900EX business jet. These are the first reported nvPM emissions of a small in-production turbofan engine determined with a standardized measurement system used for emissions certification of large turbofan engines. The ground-level measurements together with a detailed engine performance model were used to predict emissions at cruising altitudes. The measured nvPM emission characteristics strongly depended on engine thrust. The geometric mean diameter increased from 17 nm at idle to 45 nm at take-off. The nvPM emission indices peaked at low thrust levels (7 and 40% take-off thrust in terms of nvPM number and mass, respectively). A comparison with a commercial airliner shows that a business jet may produce higher nvPM emissions from flight missions as well as from landing and take-off operations. This study will aid the development of emission inventories for small aircraft turbine engines and future emission standards.
Further description : This document is the Accepted Manuscript version of a Published Work that appeared in final form in Environmental Science & Technology, copyright © American Chemical Society after peer review and technical editing by the publisher.
Departement: School of Engineering
Organisational Unit: Centre for Aviation (ZAV)
Publication type: Article in scientific journal
DOI : 10.1021/acs.est.9b02513
10.21256/zhaw-18574
ISSN: 0013-936X
1520-5851
URI: https://digitalcollection.zhaw.ch/handle/11475/18574
Restricted until : 2020-10-04
Published as part of the ZHAW project : AGEAIR: Vermessung der Effekte des Mantelstromtriebwerkverschleisses auf die Schadstoffzusammensetzung
Appears in Collections:Publikationen School of Engineering

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acs.est.9b02513.pdf
  Until 2020-10-04
Accepted Version4.17 MBAdobe PDFView/Open
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