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Design, Operational and Environmental Assessment of a Hybrid-Electric Aircraft

机译:混合电机的设计,操作和环境评估

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While literature about the design and assessment of hybrid-electric aircraft (HEA) often refers to the potential CO_2eq emission reductions compared to reference aircraft on a single design mission, this paper focuses on a more holistic approach including the emissions of other pollutants in-flight and on the ground using a 1D climate model and the climate metric sustained global temperature potential with a time horizon of 100 years (SGTP_(100)). Besides the design of an HEA and analysis of its design mission, the fleet adoption of new HEA concepts is investigated taking into account production capacities and air traffic growth scenarios. Based on these evaluations, an integrated methodology is developed to determine the climate impact of a given HEA concept on a fleet-wide scale considering the aircraft's operational environment in the global aviation market. For a single-aisle short to medium-range HEA, it is shown that the climate impact on the design mission compared to a conventional reference aircraft could be reduced by up to 11.4% SGTP_(100), assuming a battery specific energy of 1500 Wh/kg and renewable electricity production. Disparities regarding the use of CO_2eq as a metric indicate that a holistic approach using the SGTP_(100) as a metric is better suited for evaluating the climate impact reduction potential of HEA. The fleet adoption of HEA until 2050 is approximated under various input assumptions. Similar results to a conventional reference fleet concerning fleet counts as well as transport performance lead to the conclusion of comparability of fleets containing HEA and a conventional reference fleet. While an integrated methodology for fleet-wide ch'mate impact assessment has been developed, its application on a test case proved difficult due to the non-availability of simple climate models. However, via the share of available seat kilometers of the HE As, the order of magnitude of the fleet-wide climate impact reduction potential of a 2050 HEA fleet compared to a 2050 reference fleet is estimated to be in the low single-digit percentage range.
机译:虽然文献关于混合电机(HEA)的设计和评估通常是指在单一设计使命上与参考飞机相比的潜在的CO_2EQ减排,但本文侧重于更全面的方法,包括其他污染物中的排放在地面上使用1D气候模型和气候公制持续全球温度潜力,时间范围为100年(SGTP_(100))。除了为其设计使命的HEA和分析的设计之外,还考虑了生产能力和空中交通增长情景调查了舰队采用新的HEA概念。根据这些评估,开发了一种综合方法,以确定给定HEA概念的气候影响在全球航空市场中飞机的运营环境考虑到飞机的运行环境。对于中档HEA的单通道短,结果表明,与常规参考飞机相比的设计任务的气候影响最多可降低11.4%的SGTP_(100),假设电池特殊的能量为1500WH /千克和可再生电力生产。关于使用CO_2EQ作为度量的差异表明使用SGTP_(100)作为度量的整体方法更适合评估HEA的气候影响降低潜力。在2050年之前的舰队采用在各种输入假设下近似。与舰队计数的常规参考车队相似的结果以及运输绩效导致围舰队的可比性结论,含有HEA和传统参考车队。虽然已经制定了舰队宽的CH'Mate影响评估的综合方法,但由于简单的气候模型的非可用性,其对测试案件的应用证明是困难的。然而,通过他的可用座位公里的份额,与2050个参考局相比,2050个Hea舰队的舰队宽气候影响潜力的大小阶数估计在低单位数百分比范围内。

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