Ultra Performance Wing_ Project UP WING

超性能机翼项目将验证、选择、成熟和展示关键技术，并为目标超高效中短程飞机(SMR)提供“超性能机翼”概念的架构集成，即150-250 PAX和1000-2000 nm射程。该项目直接实现了清洁航空的目标：与最先进的参考飞机A321 neo相比，飞机的燃料消耗减少了至少30%。UP翼将考虑两种飞机配置，涵盖清洁航空影响目标中概述的两个开发领域：配备涡扇发动机的大展弦比SAF机翼和具有开放旋翼的干式大展弦比机翼，其能效在机翼水平上提高了17%。UP WING将开发高达TRL4的集成大展弦比SAF机翼，直到该项目结束，并将为几种干式机翼配置提供概念研究。由机身集成商、产业界、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。将在与建筑项目密切合作的情况下进行考虑影响监测的绩效监测。对于所有技术，项目目标被细分为要监控的单个目标。预计将进行地面、风洞和虚拟测试。由于多学科的优化，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。这些结果将在实现TRL6的第二个清洁航空阶段获得，直到清洁航空方案结束。这些清洁航空目标与2035年投入使用的未来飞机(SAF SMR和H2地区)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、会议稿件、期刊进展确保适当的科学开发，而工业合作伙伴将使特定的技术砖成熟到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.