喷气式飞机油耗估算:数学模型开发

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Amar Benkhaled, Amina Benkhedda, Braham Benaouda Zouaoui, Soheyb Ribouh
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引用次数: 0

摘要

目的降低飞机油耗已成为一个最重要的研究领域,重点是优化巡航阶段的速度和高度等运行参数。然而,现有的降低油耗方法往往依赖于复杂的实验计算和从嵌入式系统中提取数据,这使得实际操作具有挑战性。设计/方法/途径本文提出了一种新的分析方法,用于估算和优化装有喷气发动机的飞机的燃油消耗,尤其侧重于速度和高度参数。同时还考虑了飞行过程中燃料消耗引起的重量动态变化。通过将推导出的油耗方程应用于波音 737-700 飞机,并将结果与波音手册中提供的油耗参考表进行比较,对该方程进行了严格验证。值得注意的是,在所研究的各种高度上,该方程得出的结果都非常接近。在本文的第二部分,介绍了一种利用粒子群优化算法(PSO)的开创性方法。研究结果研究结果表明,利用本研究的主要发现,包括创新方程和 PSO 的应用,大大简化并加快了理想参数的确定过程,展示了该方法的实际应用性。研究局限/意义所建议的方法因其简单实用而脱颖而出,特别是与其他方法相比,因为可以随时获得数据以供利用。不过,在零风效应占主导地位的情况下,该方法的适用性受到限制。原创性/价值该研究为提高航空燃油效率开辟了新的可能性,尤其侧重于开发独特的燃油消耗方程,并率先使用 PSO 算法优化飞行参数。这项研究的方法易于理解,可为更环保、更经济的飞行操作铺平道路。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fuel consumption estimation for jet aircraft: a mathematical model development

Purpose

Reducing aircraft fuel consumption has become a paramount research area, focusing on optimizing operational parameters like speed and altitude during the cruise phase. However, the existing methods for fuel reduction often rely on complex experimental calculations and data extraction from embedded systems, making practical implementation challenging. To address this, this study aims to devise a simple and accessible approach using available information.

Design/methodology/approach

In this paper, a novel analytic method to estimate and optimize fuel consumption for aircraft equipped with jet engines is proposed, with a particular emphasis on speed and altitude parameters. The dynamic variations in weight caused by fuel consumption during flight are also accounted for. The derived fuel consumption equation was rigorously validated by applying it to the Boeing 737–700 and comparing the results against the fuel consumption reference tables provided in the Boeing manual. Remarkably, the equation yielded closely aligned outcomes across various altitudes studied. In the second part of this paper, a pioneering approach is introduced by leveraging the particle swarm optimization algorithm (PSO). This novel application of PSO allows us to explore the equation’s potential in finding the optimal altitude and speed for an actual flight from Algiers to Brussels.

Findings

The results demonstrate that using the main findings of this study, including the innovative equation and the application of PSO, significantly simplifies and expedites the process of determining the ideal parameters, showcasing the practical applicability of the approach.

Research limitations/implications

The suggested methodology stands out for its simplicity and practicality, particularly when compared to alternative approaches, owing to the ready availability of data for utilization. Nevertheless, its applicability is limited in scenarios where zero wind effects are a prevailing factor.

Originality/value

The research opens up new possibilities for fuel-efficient aviation, with a particular focus on the development of a unique fuel consumption equation and the pioneering use of the PSO algorithm for optimizing flight parameters. This study’s accessible approach can pave the way for more environmentally conscious and economical flight operations.

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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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