Ultra Performance Wing_ Project UP WING

超性能翼项目将验证、筛选、成熟和演示关键技术，并为目标超高效中短程飞机（SMR）提供“超性能翼”概念的架构集成，即150-250 PAX和1000-2000nm航程。该项目直接实现了清洁航空的目标：与最先进的参考飞机A321neo相比，燃油消耗至少减少30%。UP Wing将考虑两种飞机配置，涵盖清洁航空影响目标中概述的两种开发范围：带有涡扇发动机的高展弦比SAF机翼，目标为10-13%；带有开放式旋翼的干式高展弦比机翼，机翼水平的能效提高17%。在本项目结束前，UP Wing将开发高达TRL4的集成高展弦比SAF机翼，并将提供几种干翼配置的概念研究。由机身集成商、工业界、研究机构和学术界组成的跨学科欧洲联盟将开发涵盖所有相关工程学科的相关使能技术。考虑到与架构项目密切合作的影响监控，将进行性能监控。对于所有的技术，项目目标都被分解为要监控的单个目标。预计将进行地面、风洞和虚拟测试。由于多学科优化，配置1的整体机翼设计将确保所有技术的适当集成，直到TRL4。这些成果将在第二个清洁航空阶段取得，达到TRL6，直到清洁航空计划结束。这些清洁航空目标与2035年投入使用的未来飞机（SAF SMR和H2区域）的发展计划非常一致，到2050年市场渗透率将达到75%。参与的学术界将通过讲座、会议贡献、期刊记录来确保适当的科学开发，而工业合作伙伴将成熟特定的技术砖块，以达到TRL4或更高。

The Ultra Performance Wing project will validate, down select, mature and demonstrate key technologies and provide the architectural integration of “ultra-performance wing” concepts for targeted ultra-efficient Short/Medium Range aircraft (SMR), i.e. 150-250 PAX and 1000-2000nm range. The project directly addresses the Clean Aviation objectives: fuel burn reduction of minimum 30% aircraft level, compared to the state-of-the-art reference Aircraft A321neo. UP Wing will consider 2 aircraft configurations, covering both exploitation horizons outlined in Clean Aviation impact objectives: a high aspect ratio SAF wing with turbofan engine targeting 10-13% and a dry high aspect ratio wing with open rotor up to 17% energy efficiency efficiency increase on wing level. UP Wing will develop the integrated high aspect ratio SAF wing up to TRL4 until the end of this project and will provide concepts studies for several dry wing configurations. The interdisciplinary European consortium, consisting of airframe integrators, industry, research establishments and academia will develop the related enabling technologies covering all relevant engineering disciplines. Performance monitoring considering Impact Monitoring in close collaboration with the architecture project will be done. For all technologies, the project objectives are broken down to individual targets to be monitored. Ground, wind tunnel and virtual testing are foreseen. Thanks to multidisciplinary optimisation the overall wing design for Configuration 1 will ensure the proper integration of all technologies up to TRL4. These results will be picked up in a second Clean Aviation phase achieving TRL6 until the end of the Clean Aviation programme. These Clean Aviation objectives are well aligned to the development plans of future aircrafts entering into service in 2035 (SAF SMR & H2 Regional), with 75% market penetration until 2050. Academia involved will ensure proper scientific exploitations via lectures, conference contributions, journal proceedings whereas the industrial partners will mature specific technology bricks to TRL4 and higher.