This paper reviews the aspects about the reliability and the integrity of aircraft structures.
本文综合评述飞机结构的可靠性和完整性问题。
This paper presents a set of fundamental equations for reliability analysis of aircraft structures.
本文提出飞机结构可靠性分析的基本公式。
Inspects, dismantles and reassembles aircraft structures, and repairs and replaces components of aircraft frames.
检查、拆除和重组飞机结构，维修并更换机体的部件。
Aircraft structures, especially some important units, are commonly fabricated by the use of mechanical bolt joints.
螺栓连接是飞机结构常用的连接方式，特别是一些重要的部件常采用这种连接方法。
Mechanical joint provide the primary means for transferring load among components in the construction of aircraft structures.
在飞机结构中，机械连接是传递力学载荷的主要方式。
The contact corrosion occurred between Ti or Ti-Alloy Parts and other metals in the aircraft structures is described in this paper.
本文叙述了飞机结构中钛及钛合金件与其它金属件之间所发生的接触腐蚀。
The design conception and principle of damageable substitute, and its practical applications in aircraft structures are described in detail.
详细叙述了替损件的设计思想和设计原则，以及在飞机结构上的应用实例。
The corrosion characteristics of aircraft structures were briefed. The definition of the local environmental spectrum on aircraft structure was given.
简要阐述了飞机结构的腐蚀特点，给出飞机结构局部环境谱的定义。
In comparison with the coatings applied presently for aircraft structures, the nano-composite coatings showed better anti-aging performance to UV radiation.
与现役飞机涂层相比，纳米复合涂层的抗紫外线老化性能有明显改进。
This would represent a decade-long reduction in spending for aircraft structures, avionics, engines, sensors, and other electronics by one-third, according to GEIA analysts.
根据GEIA分析家的分析，未来十年，飞机结构、航空电子、工程、传感器和其他电子支出都将消减1/3。
With the increasing effects of corrosive environment on the aircraft structures, calendar life has become a severe trouble of the air force at present and in the future.
随着腐蚀环境对飞机结构寿命的影响日益突出，日历寿命已成为当今乃至今后我军飞机面临的严峻问题。
Classification code system is required for aircraft structures. To meet this requirement a classification code system and the application software are developed by BAMTRI.
本文探讨了飞机结构件对分类编码系统的需求及其开发流程，并介绍了该所开发的一套飞机结构件分类编码系统及应用软件。
This paper introduces the designing goal and requirements, the database structure, and the data component of the database of corrosion control design for aircraft structures.
介绍了飞机结构腐蚀控制设计数据库的设计目标和要求、数据库结构和数据组成。
In this paper the authors proposed that the term of "design allowables" should be replaced by "design values" and "allowables" as composites were used in aircraft structures.
由于复合材料的引入，应该用“设计值”和“许用值”来代替“设计许用值”。
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。
The fatigue life of civil aircraft structures obeys two parameter Weibull distribution, its scatter factor is significantly different from that obeys logarithm normal distribution.
民机结构的疲劳寿命服从双参数威布尔分布，其分散系数与战斗机基于对数正态分布的疲劳寿命分散系数存在明显的不同。
It is most economical and effective to renew the load carrying capability and extend the service life by employing composite patches for repair of damaged metallic aircraft structures.
采用复合材料补片对损伤的金属飞机结构进行胶接修理，可以经济而有效地恢复结构的承载能力和延长结构的使用寿命。
To quantitatively evaluate the effects of corrosion during grounding on fatigue life of aircraft structures, a new power equation is proposed using two-variable linear regression method.
为评估地面停放预腐蚀对飞机结构疲劳寿命的影响，采用二元线性回归方法建立了一种新的预腐蚀疲劳曲线幂函数表达式。
The optical fiber system embedded in composite materials will become a "Neutral Network System" of the future aircraft structures, leading to new concepts of the "Intelligent Structures".
提出了埋设于复合材料内部的光纤系统将成为未来飞行器结构的“神经网络系统”而使结构成为“智能结构”等新概念。
The clash between flying birds and airplanes frequently results in damage of aircraft structures which could even lead to aircraft crash and death of crew members in the most disastrous cases.
鸟与飞行中的飞机相撞是飞机结构损坏的重要因素，严重时会引发机毁人亡的灾难性事故。
New, lightweight ceramics will further reduce the need for metals in aircraft, says Joy DE Lisser, vice-president of ATK Aerospace Structures, the division developing them.
新型轻质陶瓷的使用将进一步减少飞机制造中的金属需求，乔伊•德•丽萨说道，她是AT K航空航天公司的副总，他们分公司正在开发这种材料。
Aircraft industry. Synthetic cloths for the fabric of airplane structures. Peeling strength of the bonding of taping fabric.
航空工业。飞机结构纤维用合成纤维。浆纱并绞纤维粘结的剥离强度。
Structures of aircraft composite parts include honeycomb, inner contained part, inner empty part, and layered etc.
飞机复合材料零件结构分为蜂窝结构、夹心结构、空心结构、夹层结构等。
Therefore, it is an effectivemethod to improve corrosion fatigue property to use the hole cold-expansion technique in the aircraft and other structures.
因此，在飞机和其他结构的关键部位，采用冷胀孔技术是一种提高腐蚀环境下结构疲劳性能的行之有效的方法。
Bonded composite repair has been recognized as an efficient and economical method to extend the service life of damaged aircraft metallic structures.
损伤金属飞机结构的复合材料补片胶接修理技术是一项经济而有效的结构延寿方法。
Alloy 7075 sheet and plate products have application throughout aircraft and aerospace structures where a combination of high strength with moderate toughness and corrosion resistance are required.
7075合金薄板和中厚板产品应用遍及航空航天结构当中，其中，适中的韧性和腐蚀性的高强度结合是材料所必须具有的。
Alloy 7075 sheet and plate products have application throughout aircraft and aerospace structures where a combination of high strength with moderate toughness and corrosion resistance are required.
7075合金薄板和中厚板产品应用遍及航空航天结构当中，其中，适中的韧性和腐蚀性的高强度结合是材料所必须具有的。
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