Hybrid Electric Regional Wing Integration Novel Green Technologies - HERWINGT

混合动力电动区域机翼集成新型绿色技术 - HERWINGT

• 批准号: 10087390
• 金额: $ 13.22万
• 依托单位: GOODRICH ACTUATION SYSTEMS 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=10087390
• 关键词: Hybrid; Electric; Regional; Wing; Integration

Development of key technologies to address a new wing design for a HER aircraft maturing up to TRL5: manufacturing, assembly, structural concepts and processes, concept studies, configuration and architecture trade offs for a full wing component are part of the activity. As a physical demonstration concept, the detail design and manufacturing of the relevant components of a centre wing section of a HER Aircraft will be addressed. Conceptual wing studies: configuration and architecture (structural arrangement, Systems allocation and disposition, flight control system) trade offs for a full wing. Full wing structural arrangement mock up for innovative wing concepts, Structural and Multidisciplinary Optimization studies for definition of the optimal structural configuration of wing. Demonstration platform: wingbox, high lift devices, control surfaces, load alleviation devices focusing on the centre section as a demonstration platform: - Integrated Centre section wing box structure with the inner Propulsion stage: Full span (pylon to pylon) torsion box concept representative of more ambitious tip 2 tip concept. Multispar concept, Access manholes and panels, Sustainable aviation fuel and Integrated Fuel vent systems. - Inner section Leading Edges, Integrated Inductive ice protection system integration, Multifunctionality: erosion, impact, Lightning, ice protection, Morphing concepts, Functional tests, Bird strike tests (virtual or real) - Inner section Flap and high lift solutions: Integrated flap solutions. Multifunctionality application to flap. Key processing technologies: Low cost-high integrated out of autoclave technologies. Dry fiber placement and liquid resin infusion for integrated multispar torsion box. Thermoplastic composites processing: In situ consolidation for integrated flap skin and Leading edge applications. Thermoplastic welding and co-consolidation for Integration. Bonding technologies exploration towards certifiable solutions.

开发关键技术，以解决成熟到TRL 5的HER飞机的新机翼设计：制造，装配，结构概念和工艺，概念研究，全机翼部件的配置和架构权衡是活动的一部分。作为一个物理演示的概念，详细设计和制造的中心机翼部分的HER飞机的相关部件将被解决。机翼概念研究：布局和结构（结构布置、系统分配和配置、飞行控制系统）对全机翼的权衡。全机翼结构布局模拟，用于创新机翼概念，结构和多学科优化研究，用于定义机翼的最佳结构配置。示范平台：翼盒、增升装置、操纵面、载荷减缓装置，集中在作为演示平台的中央部分：-具有内部推进级的一体化中央部分翼盒结构：全翼展（挂架到挂架）扭转盒概念，代表了更雄心勃勃的翼尖2翼尖概念。Multispar概念，检修孔和面板，可持续航空燃料和综合燃料通风系统。- 内段前缘，集成感应防冰系统，多功能性：防腐蚀，防撞击，防雷击，防冰，变形概念，功能测试，鸟撞测试（虚拟或真实的）-内段襟翼和增升解决方案：集成襟翼解决方案。皮瓣多功能应用。关键加工技术：低成本高集成的高压釜外技术。干式纤维铺放和液态树脂灌注，用于集成式多梁抗扭箱。热塑性复合材料加工：原位固化，用于一体化皮瓣皮肤和前沿应用。热塑性焊接和共固结的集成。键合技术的探索，走向可认证的解决方案。