Emission Comparison of Turbofan and Open Rotor Engines under Special Consideration of Aircraft and Mission Design Aspects

机译：特别考虑飞机和任务设计方面的涡扇发动机和开式转子发动机的排放比较

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An integrated parametric model involving the design of propulsion system, airframe and flight mission isrnpresented. Based hereon, the CO2 emission characteristics of advanced conventional turbofan-powered aircraftrnand open rotor-powered aircraft are analysed against essential aircraft and propulsion system design parameters.rnIn addition, first concept-specific trend statements on Nox as well as propulsor noise emission characteristics arernderived. The obtained results may contribute to a better understanding of optimum aircraft design conditions forrnadvanced system architectures.

机译：提出了涉及推进系统，机体和飞行任务设计的集成参数模型。在此基础上，根据飞机的基本参数和推进系统的设计参数，对先进的常规涡扇发动机飞机和开放式旋翼飞机的CO2排放特征进行了分析。此外，还推导了关于NOx的第一个概念特定趋势陈述以及推进器噪声排放特征。获得的结果可能有助于更好地理解先进系统架构的最佳飞机设计条件。

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来源
《New beginnings: challenges for aerospace innovation》|2009年|p.1-16|共16页
会议地点 Manchester(GB)
作者
A. Seitz; D. Schmitt; S. Donnerhack;
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作者单位

Bauhaus Luftfahrt, Lyonel-Feininger-Str. 28, 80807 Munich, Germany;

Bauhaus Luftfahrt, Lyonel-Feininger-Str. 28, 80807 Munich, Germany;

MTU Aero Engines, Dachauer Str. 665, 80995 Munich, Germany;

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正文语种 eng
中图分类航空、航天技术的研究与探索;
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All abbreviations, acronyms and symbols are explained in the text;

机译：所有缩写，首字母缩写和符号均在文本中说明;

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专利

1. Emission comparison of turbofan and open rotor engines under special consideration of aircraft and mission design aspects [J] . A. Seitz, D. Schmitt, S. Donnerhack The Aeronautical Journal . 2011,第1168期

机译：特别考虑飞机和任务设计方面的涡轮风扇发动机和开放式转子发动机的排放比较
2. Modeling Geared Turbofan and Open Rotor Engine Performance for Year-2050 Long-Range and Short-Range Aircraft [J] . Francesco S. Mastropierro, Joshua Sebastiampillai, Florian Jacob, Journal of Engineering for Gas Turbines and Power . 2020,第4期

机译：为2050年远程和短程飞机的齿轮传动涡轮风扇和开式转子发动机性能建模
3. Conceptual design study of a geared turbofan and an open rotor aero engine with intercooled recuperated core [J] . C Salpingidou, D Misirlis, Z Vlahostergios, Proceedings of the Institution of Mechanical Engineers . 2018,第14期

机译：齿轮冷却的涡轮风扇和带有中冷回热芯的开放转子航空发动机的概念设计研究
4. Emission Comparison of Turbofan and Open Rotor Engines under Special Consideration of Aircraft and Mission Design Aspects [C] . A. Seitz, D. Schmitt, S. Donnerhack CEAS European air and space conference . 2009

机译：飞机及任务设计方面特殊考虑下涡轮机和开放式转子发动机的排放比较
5. Comparison of Fault Detection Strategies on a Low Bypass Turbofan Engine Model. [D] . Aull, Mark. 2011

机译：低旁路涡扇发动机模型的故障检测策略比较。
6. Non-volatile particle emissions from aircraft turbine engines at ground-idle induce oxidative stress in bronchial cells [O] . Hulda R. Jonsdottir, Mathilde Delaval, Zaira Leni, 2019

机译：飞机怠速时飞机涡轮发动机的非挥发性颗粒物排放会在支气管细胞中引起氧化应激
7. Withdrawal: Flow Field Analysis Inside First Stage Rotor (LPC) of Low By Pass Ratio Turbofan Engine With Integrated Aircraft Intake Data [O] . Aizaz Farooq, Jehanzeb Masud, Muhammad Usama Bin Shehzad 2019

机译：用集成飞机进气数据取出：通过与集成飞机进口数据提取的第一级转子（LPC）内的流场分析
8. A COMPARISON OF OPTIMUM JP AND LH2 TURBOFAN ENGINES DESIGNED FOR TWO SUBSONIC TRANSPORT MISSIONS [R] . Kestutis C. Civinskas 1974

机译：最优Jp和LH2 TURBOFaN发动机的比较设计用于两个次同运输任务

Emission Comparison of Turbofan and Open Rotor Engines under Special Consideration of Aircraft and Mission Design Aspects

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