Ultra Performance Wing_ Project UP WING

超性能翼_Project UP WING

• 批准号: 10068384
• 金额: $ 35.07万
• 依托单位: MEGGITT AEROSPACE LIMITED
• 依托单位国家: 英国
• 项目类别: EU-Funded
• 财政年份: 2023
• 资助国家: 英国
• 起止时间: 2023 至 无数据
• 项目状态: 未结题
• 来源: https://gtr.ukri.org/projects?ref=10068384
• 关键词: Ultra; Performance; Wing_; Project; UP

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.

超性能机翼项目将验证、筛选、成熟和演示关键技术，并为目标超高效中短程飞机（SMR）（即150-250 PAX和1000- 2000 nm航程）提供“超性能机翼”概念的架构集成。该项目直接解决了清洁航空的目标：与最先进的参考飞机A321 neo相比，燃油消耗减少至少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：一种大展弦比SAF机翼，涡轮风扇发动机目标为10-13%，一种干大展弦比机翼，开放式转子可将机翼水平的能效提高高达17%。UP Wing将发展综合大展弦比SAF机翼直到TRL 4，直到这个项目结束，并将提供几个干翼布局的概念研究。由机身集成商、工业、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。将与架构项目密切合作进行绩效监测，同时考虑到影响监测。对于所有技术，项目目标被分解为需要监测的单个目标。预计将进行地面、风洞和虚拟试验。由于多学科的优化，构型1的整体机翼设计将确保TRL 4之前的所有技术的正确集成。这些结果将在第二个清洁航空阶段获得，实现TRL 6，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的发展计划（SAF SMR & H2 Regional）保持一致，到2050年市场渗透率达到75%。参与的学术界将通过讲座、会议投稿、期刊论文集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TRL 4或更高。