Job Description (职位说明)

Wefly is currently seeking multiple self-driven structure analysis engineer with strong composite aircraft structure analysis experience to reshape the future of electric aviation. You will directly lead or participate in the entire life cycle of the next-generation eVTOL aircraft development programs, including but not limited to initial sizing for primary and secondary aircraft structures via structural static and dynamic analysis, developing the analysis methods and tools for static strength, fatigue and damage tolerance analysis, analyzing composite parts and assemblies for primary and secondary flight structures, conducting FEM/FEA analysis and producing technical requirement, interfacing with all aircraft stakeholders for aircraft optimizations, occasionally also support structure analysis of battery and other systems, support aircraft assembly, aircraft structure test, ground test and flight test.

我们目前正在寻找多名具有深度飞机复合材料结构分析经验且自驱动力强的结构分析工程师来一起塑造电动航空的未来。您将直接领导或参与下一代eVTOL飞机研发项目的全生命周期，包括但不限于飞于通过结构静态和动态分析对主要和次要飞机结构进行初始尺寸确定，开发用于静态强度、疲劳和损伤容限分析的分析方法和工具，分析主要和次要飞行结构的复合材料零件和组件，进行 FEM/FEA 分析和提出生产技术要求，与其他飞机团队成员一起进行飞机优化，有时还支持电池和其他系统的结构分析，支持飞机组装、飞机结构测试、地面测试和试飞。

Minimal Qualifications （基本资质）
● Masters or other advanced degrees from top universities in one or more of the following disciplines: aerospace, mechanical engineering, physics/math, and other aerospace related disciplines. Bachelor degree will be considered if more than 3 years of industrial experience or other extraordinary.
● Demonstratable experience in structural load analysis, composite structure static or dynamic analysis, structure limit or endurance testing, or other complex thermal/structure/aero/electrical coupled structural analysis via direct working experience, research experience or extracurricular activity
● Basic understanding of aircraft aerodynamic/inertial load, aircraft flight load conditions and associated critical load cases, aeroelastic phenomena such as flutter, buffeting, and frequency response, and etc.
● Extremely proficient in 3D Computer Aided Design Programs such as CATIA (preferred), FEM/FEA analysis tools such as NASTRAN, PATRAN (Preferred)
● Self-starter, can-do attitude, team player, sense of responsibility, quick learner, and open mind
● High integrity, attention to detail, and safety critical thinking
● Sufficient English writing and reading capabilities.

● 拥有以下一个或多个学科的一流大学硕士学位或其他高级学位：航空航天/航空、机械工程、物理/数学、系统工程和其他航空航天相关学科; 3年以上行业经验或其他非凡经验者可考虑学士学位
● 拥有下列一个或者全部通过工作、研究或个人兴趣爱好项目获取的可证明的经验: 结构载荷分析、复合结构静态或动态分析、结构极限或耐久性测试，或其他复杂的热/结构/航空/电气耦合结构分析
● 基本了解飞机气动/惯性载荷、飞机飞行载荷条件和相关的临界载荷情况、气动弹性现象（如颤振、抖振和频率响应等）
● 做事有上进心、can-do精神、团队精神、责任心、快速学习、思想开放
● 人品正直、注重细节、有很强的安全批判性思维
● 能自如读写英文

Desired Qualifications （期望资质）
● Ph.D degrees from top universities in one or more of the following disciplines: aerospace/aeronautical, mechanical engineering, and other aerospace related disciplines
● 3+ years working experience in one or more of the following domains: aircraft structure such as wing, horizontal / vertical stabilizer/fuselage structure analysis, structure static/flutter test laboratory setup and implementations, flight load analysis, various aeroelastic analysis, and etc
● Deep knowledge in aircraft aerodynamic/inertial load, aircraft flight load conditions and associated critical load cases, more advanced aeroelastic analysis such as flutter, frequency, and transient response
● Understand FAA/EASA/CAAC Part 23/25/27/29 aircraft certification regulations

● 拥有以下一个或者多个国内外一流大学博士学位：航空航天/航空、机械工程、和其他航空航天相关学科
● 3年以上以下一个或多个领域的工作经验：飞机结构如机翼/平尾/垂尾/机身结构分析、结构静力/颤振测试实验室搭建和操作、飞行载荷分析、各种气动弹性分析等
● 深度了解飞机气动/惯性载荷、飞机飞行载荷条件和相关的临界载荷情况、气动弹性现象（如颤振、抖振和频率响应等）
● 理解美国FAA、欧洲EASA或中国民航23/25/27/29部飞机适航标准要求