民用窄体涡桨飞机环境影响初步分析

Min Chen, Weiqun Gu
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引用次数: 1

摘要

对民用窄体涡桨飞机的环境影响进行了研究。本研究的主要目标是通过典型航线的飞行性能模拟,探讨涡桨发动机是否可以替代涡扇发动机为民用窄体飞机提供环保动力。该研究基于三个代码,飞机性能模型“APM”,燃气轮机性能模型“TURBOMATCH”,排放预测工具“HEPHAESTUS”,由英国克兰菲尔德大学开发。结果表明,用涡桨发动机代替涡扇发动机可以降低总燃油消耗量。但是随着飞行距离从650公里增加到4000公里,由于时间惩罚从23%增加到37%,这一优势从18.9%减少到6.5%。此外,这种替代还可以减少80%左右的NOx排放,而CO2排放的减少与燃料燃烧的减少成正比。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Preliminary analysis on the environment impact of civil narrow body turboprop aircraft
A study on the environment impact of civil narrow body turboprop aircraft was performed. Main target of this study is to investigate whether the turboprop is an environmental friendly power substitution for turbofan to power the civil narrow body aircraft through flight performance simulation in typical routes. The study was based on the utilization of three codes, aircraft performance model `APM', gas turbine performance model `TURBOMATCH', emission prediction tool `HEPHAESTUS', developed by Cranfield University, UK. Results show, the substitution of turbofan with turboprop can reduce the total fuel burn. But this benefit reduces from 18.9% to 6.5% with the increase of the flight range from 650km to 4000km due to stronger and stronger time penalty from 23% to 37%. In addition, this substitution can also reduce around 80% NOx emission, while the reduction of CO2 emission is proportional to the reduction of fuel burn.
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