Modified C-17 taxi procedures: a fuel cost savings exploration

Q3 Decision Sciences
Michael Wells, Michael P. Kretser, B. Hazen, J. Weir
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Abstract

Purpose This study aims to explore the viability of using C-17 reduced-engine taxi procedures from a cost savings and capability perspective. Design/methodology/approach This study model expected engine fuel flow based on the number of operational engines, aircraft gross weight (GW) and average aircraft groundspeed. Using this model, the research executes a cost savings simulation estimating the expected annual savings produced by the proposed taxi methodology. Operational and safety risks are also considered. Findings The results indicate that significant fuel and costs savings are available via the employment of reduced-engine taxi procedures. On an annual basis, the mobility air force has the capacity to save approximately 1.18 million gallons of jet fuel per year ($2.66m in annual fuel costs at current rates) without significant risk to operations. The two-engine taxi methodology has the ability to generate capable taxi thrust for a maximum GW C-17 with nearly zero risks. Research limitations/implications This research was limited to C-17 procedures and efficiency improvements specifically, although it suggests that other military aircraft could benefit from these findings as is evident in the commercial airline industry. Practical implications This research recommends coordination with the original equipment manufacturer to rework checklists and flight manuals, development of a fleet-wide training program and evaluation of future aircraft recapitalization requirements intended to exploit and maximize aircraft surface operation savings. Originality/value If implemented, the proposed changes would benefit the society as government resources could be spent elsewhere and the impact on the environment would be reduced. This research conducted a rigorous analysis of the suitability of implementing a civilian airline’s best practice into US Air Force operations.
改进的C-17滑行程序:节省燃料成本的探索
本研究旨在从节省成本和能力的角度探讨使用C-17减少发动机滑行程序的可行性。设计/方法/方法本研究基于运行中的发动机数量、飞机总重(GW)和飞机平均地面速度对发动机燃油流量进行建模。利用这个模型,研究执行了一个成本节约模拟,估计了拟议的出租车方法所产生的预期年度节约。操作和安全风险也被考虑在内。研究结果表明,通过采用减少发动机的滑行程序,可以节省大量燃料和成本。在每年的基础上,机动空军每年有能力节省大约118万加仑的喷气燃料(按目前的费率计算,每年的燃料成本为266万美元),而不会对作战造成重大风险。双引擎滑行方法能够为最大GW C-17产生有能力的滑行推力,几乎为零风险。本研究仅限于C-17程序和效率改进,尽管它表明其他军用飞机也可以从这些发现中受益,这在商业航空业是显而易见的。实际意义本研究建议与原始设备制造商协调,重新编写检查清单和飞行手册,制定全机队范围的培训计划,并评估未来飞机资本重组需求,以利用和最大化飞机地面运营节约。原创性/价值建议的改变若得以实施,可令社会受惠,因为政府资源可用于其他地方,并可减少对环境的影响。这项研究对美国空军实施民用航空公司最佳实践的适用性进行了严格的分析。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
0.90
自引率
0.00%
发文量
5
审稿时长
12 weeks
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