1) fastener joint
螺栓搭接件
1.
The fatigue experimental studies of some multiple holed and cracked plates and fastener joints exposed to constant amplitude as well as flight by flight loading spectra have been carried out for the damage tolerance evaluation of typical aircraft wing structural components.
针对机翼典型对接结构，进行了平板空孔试样和螺栓搭接件在等幅谱及飞－续－飞谱下的多裂纹损伤容限试验，通过该试验开展多裂纹开裂模式及多裂纹扩展规律的试验研究，为多裂纹断裂力学理论分析、多裂纹结构剩余强度准则提供试验依据。
2) bolted fastenings
螺栓连接件
1.
Be aimed at the fatigue life dispersivity of bolted fastenings, the distribution of bolt hole clearance is derived by measuring the sizes of typical bolts and holes in wing spars of a certain aircraft, and the distribution interval of the shearing stiffness of the new specimen is obtained by reliability analysis method.
针对螺栓连接件疲劳寿命分散性问题 ,对某型飞机机翼主梁上的一种典型螺栓和连接孔进行测量 ,获得栓孔的配合间隙分布数据。
3) fillet weldment
搭接焊件
4) lap joint
搭接件
1.
It is found that there are corrosion pillowing cracks in lap joints.
通过对某型退役飞机分解检查,发现搭接件在腐蚀产物的膨胀作用下产生了裂纹。
5) lap joints
搭接件
1.
Analysis of stress and strain in corroded lap joints in aircraft structure;
飞机结构腐蚀搭接件应力应变分析
2.
Fretting fatigue usually occurs in lap joints of aircraft structure.
搭接件是飞机结构中容易产生微动疲劳损伤的部位。
6) member lap
构件搭接
1.
Aiming at the phenomena paying little attention to constructional design, it illustrates the importance of joint designs in structure, analyzes the methods of member lap and joint designs and puts forward some personal opinions about joint designs in landscape Architecture application according to some detailed materials.
针对目前构筑物设计中普遍存在不重视结构设计的现象，本文以翔实的资料从建筑结构技术的发展及设计观念出发，阐明了构筑物构件搭接与节点设计的重要性，分析了构件搭接与节点设计的方法，并对构件搭接与节点设计在景观设计中的应用提出了个人的一些看法，希望以此引起设计师对构筑物设计中结构知识的关注，从而建立构件搭接与节点设计的新观念。
补充资料：黏合搭接接头
分子式：
CAS号：
性质：两个被粘物部分叠合粘接在一起形成的接头。搭接比对接形式抗剪强度高，而且可靠，是一种十分普遍使用的粘接形式。
CAS号：
性质：两个被粘物部分叠合粘接在一起形成的接头。搭接比对接形式抗剪强度高，而且可靠，是一种十分普遍使用的粘接形式。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条