航空发动机氮氧化物排放评估方法

IF 0.5 Q4 ENGINEERING, AEROSPACE International Journal of Sustainable Aviation Pub Date : 2020-02-12 DOI:10.1504/ijsa.2019.10026925
K. Synylo, N. Duchêne
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引用次数: 3

摘要

在过去的十年中,许多调查也集中在评估飞机发动机排放对机场附近当地和区域空气质量的影响。认证的排放指数依赖于在发动机测试期间定义良好的测量程序和条件。然而,在实际情况下,操作条件(功率设置、模式时间和燃油流量)和气象条件(空气温度、湿度和压力)可能与ICAO的定义不同,因此可能会出现与认证排放指数的偏差。为了对飞机发动机进行排放评估,建立了先进的涡扇发动机排放模型(TURBOGAS排放模型),该模型考虑了运行条件和气象条件对排放指标的影响,生成了精确的飞机排放清单以及尾迹的可能性和寿命。BFFM2和P3T3方法均已在TURBOGAS排放模型中实现。
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Methods for assessment of NOx emissions from aircraft engine
During the last decade a lot of investigations also focused on the evaluation of the impact of aircraft engine emissions on the local and regional air quality in the vicinity of the airport. The certificated emission indices rely on well-defined measurement procedures and conditions during engine test. Under real circumstances, however, operational (power setting, time-in-mode and fuel flow rate) and meteorological (air temperature, humidity and pressure) conditions may vary from ICAO definition, consequently deviations from the certificated emission indices may occur. The advanced emission model of turbofan engine (TURBOGAS emission model) was developed for the assessment of aircraft engine emissions taking into account the influences of operational and meteorological conditions on emission indexes to generate precise aircraft emissions inventories as well as contrails likelihood and lifetime. Both BFFM2 and P3T3 methods have been implemented in the TURBOGAS emission model.
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0.20
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