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- aircraft structure design 航空器结构设计
- Steel structure design experience is an advantage. 有钢结构设计经验者优先。
- New Structure Design Plan for Rotary Core Shooter. 回转式射芯机结构设计方案
- Since the crew and passengers' bodies are not rigidly attached to the airframe of the aircraft, the design of the aircraft structure and the seat may cause the acceleration forces experienced by the crew and passengers to be amplified or attenuated. 因爲机组人员和乘客的身体并非死死地固定在飞机的机身上，飞机结构与座位的设计也许会造成对机组人员和乘客所经历的加速力的增加或减少。
- The detail fatigue rating (DFR) method, based on probability fatigue, is one of fatigue reliability life design and prediction methods for civil aircraft structure, and has been widespreadly developed both home and abroad. 细节疲劳额定值法(DFR法)是基于概率疲劳的民机结构疲劳可靠性寿命分析方法之一，该方法在国内外都有了较大的发展。
- Describe structure design of light bulk urea storage house. 介绍一种轻型尿素散装仓库结构设计。
- New product design, structure design for new product. 工作职责:负责公司新产品的设计。
- On the Structure Design of Support Mechanism of Cupola. 论冲天炉支撑部件的结构设计。
- Linking Riveting Process Parameters to the Fatigue Performance of Riveted Aircraft Structure. 铆接过程参数与铆接飞机结构的疲劳性能的联系。
- Minimum 3 years of steel structure design experience. 3年以上钢结构设计经验。
- Civil engineering structure design and technical consultation. 工业与民用建筑结构设计和业务咨询。
- Using the concept of structure design is entity attribute analysis. 概念结构设计采用的是实体属性分析法。
- A formula in terms of DFR value to describe the relationship between the fatigue properties of aircraft structure and the corrosion time was presented. 提出了一种用DFR值描述飞机结构的疲劳性能随腐蚀时间变化的关系式。
- To undertake structural design and drawing review. 承担结构设计和图纸审核。
- Bases on the aircraft structure fatigue life theory, consider the characteristics of small UAV, the model of fatigue life prediction for small UVA structure is established. 在飞机结构寿命理论的基础上，结合小型无人机机体结构特点，建立了小型无人机机体寿命分析方法。
- The corrosion damage of aircraft structure has randomness and fuzziness, a new method is proposed to express corrosion damage by fuzzy equivalent corrosion damage. 针对飞机结构腐蚀损伤的随机性和模糊性,提出了利用模糊等效腐蚀损伤来直观表示腐蚀损伤的新方法。
- The finite element analysis was used to compute the natural frequencies of main material LY12-CZ in aircraft structure which was damaged by different levels of corrosion. 摘要为了研究腐蚀对LY12-CZ铝合金板性能的影响，采用有限元法对航空结构中的主体材料LY12-CZ铝合金板进行了不同程度腐蚀后的动力特性分析，得到其在不同腐蚀损伤后的固有频率。
- Landing gear is one of the important equipments in the aircraft structure, it can influence the aircraft during the process of takeoff, landing and taxiing. 起落架是飞机结构中的重要装置之一,它影响到飞机的起飞、着陆和滑跑过程。
- Good knowledge in big structure design, especially out of home product. 具有大型结构设计经验,最好有户外产品设计经验。
- Structure design of piezoresistive silicon-micro-accelerometer is introduced. 介绍压阻式硅微加速度计的结构设计。
