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- composite aircraft structure 复合材料飞机结构
- The Outline of New Specifications on Strength of Composite Aircraft Structures 复合材料飞机结构强度新规范要点评述
- 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。
- It is shown that COMPASS is not only an engineering optimum design software hut also an aeroelastic tailoring tool for composite aircraft wing. 利用复合材料各向异性特性和优化设计技术,开展结构气动弹性剪裁研究,是防止前掠翼发散的有效手段。
- 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。
- Wan Z Q,Tang C H,Zou C Q.Static aeroelastic characteristics analysis of a flexible forward-swept composite aircraft [J].Acta Materiae Compositae Sinica,2002,19(5):118-124. [2]万志强;唐长红;邹丛青.;柔性复合材料前掠翼飞机静气动弹性分析[J]
- 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。
- Mechanically fastened joints of composite materials are mainly components in aircraft structures, which need to be subjected to static loadings and fatigue loadings during working. 复合材料连接接头是复合材料航空结构中的主要部件,在工作过程中,要求能承受一定的静载荷及疲劳载荷,其损伤失效及疲劳寿命是设计人员关心的问题之一。
- 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。
- Advanced Design Composite Aircraft 高级设计合成材料飞机
- This paper introduces the reliability analysis and engineering application research of aircraft structure, tespectively applies Stress Severe Coefficient and DFR on the fatigue life astimation and reliability analyisis on the six Selected questions. 介绍了结构疲劳可靠性分析方法及工程应用研究情况，对选定的6个考题分别用应力严重系数法和DFR法进行了疲劳寿命估算和可靠性分析。
- I-DEAS.Through this detailed stress analysis, we may justify the designand repair of aircraft structures. 及经由不同修补方法修补的应力分布 .;以作为读者的参考
- The results indicated that the anticorrosive properties of the heavy-duty coating SEBF/SLF are much better than the ordinary coating on the active service aircraft structures. 结果表明，与现役飞机典型涂层相比，SEBF/SLF重腐蚀防护涂层的抗环境腐蚀性有明显改进。
- Study of Curing-Optical Composite Flexible in Aircraft Structure Rush to Repair 光固化复合材料在飞机结构抢修中的应用研究
- The Aircraft Structure General Repair and Analysis 飞机结构常规修理方法及分析
- The aircraft was flying above thick fog. 飞机在浓雾上空飞行。
