1. This paper reviews the aspects about the reliability and the integrity of aircraftstructures.
本文综合评述飞机结构的可靠性和完整性问题。
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2. This paper presents a set of fundamental equations for reliability analysis of aircraftstructures.
本文提出飞机结构可靠性分析的基本公式。
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3. Inspects, dismantles and reassembles aircraftstructures, 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。
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4. Aircraftstructures, 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。
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5. Mechanical joint provide the primary means for transferring load among components in the construction of aircraftstructures.
在飞机结构中，机械连接是传递力学载荷的主要方式。
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6. The contact corrosion occurred between Ti or Ti-Alloy Parts and other metals in the aircraftstructures 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。
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7. The design conception and principle of damageable substitute, and its practical applications in aircraftstructures 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。
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8. The corrosion characteristics of aircraftstructures 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。
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9. In comparison with the coatings applied presently for aircraftstructures, 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。
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10. This would represent a decade-long reduction in spending for aircraftstructures, 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。
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11. With the increasing effects of corrosive environment on the aircraftstructures, 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。
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12. Classification code system is required for aircraftstructures. To meet this requirement a classification code system and the application software are developed by BAMTRI.
13. This paper introduces the designing goal and requirements, the database structure, and the data component of the database of corrosion control design for aircraftstructures.
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。
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14. 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”。
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15. Mechanically fastened joints of composite materials are mainly components in aircraftstructures, which need to be subjected to static loadings and fatigue loadings during working.
16. The fatigue life of civil aircraftstructures obeys two parameter Weibull distribution, its scatter factor is significantly different from that obeys logarithm normal distribution.
17. 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 aircraftstructures.
18. To quantitatively evaluate the effects of corrosion during grounding on fatigue life of aircraftstructures, a new power equation is proposed using two-variable linear regression method.
19. The optical fiber system embedded in composite materials will become a "Neutral Network System" of the future aircraftstructures, leading to new concepts of the "Intelligent Structures".
20. The clash between flying birds and airplanes frequently results in damage of aircraftstructures 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。
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21. 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.
22. 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。
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23. 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。
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24. 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。
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25. However, it is very possible to have many failure modes of aircraft engineering structures.
但对于飞行器结构来说非常有可能出现几种失效模式的混合情况。
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26. 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。
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27. 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.
28. 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.
