| 1. | Aerospace fitting joint assembly , radial sealing . o - rings . dimensions
航空航天径向密封装配连接组件. o形圈.尺寸 |
| 2. | Railway transport equipment . rough - quality loose - fitting joints with clevis and tenon . constituent parts
铁路运输设备.带u形环和榫的粗加工质量的松动配合接头.构件 |
| 3. | Aerospace fitting joint assembly , radial sealing . male thread fittings . iso metric thread profile and tolerances . dimensions
航空航天径向密封装配接头组件.阳螺纹接头. iso米制螺纹牙形和公差.尺寸 |
| 4. | Aerospace fitting joint assembly , radial sealing . internal thread bosses . iso metric thread profile and tolerances . dimensions
航空航天径向密封装配接头组件.内螺纹套管. iso米制螺纹牙形和公差.尺寸 |
| 5. | The quality of joint has much effect on the age limit of airplane . the fatigue strength can be improved by using interference - fit joint in metal joint - structure
连接质量极大地影响着飞机的寿命，干涉配合连接能成倍提高接头的疲劳强度。 |
| 6. | Researches have been done on driving interference - fit joint by stress - wave in this paper , to expect to apply the driving method in the manufacturing process soon
本文展开应力波安装干涉配合紧固件的研究，以期将这种安装技术尽快应用到实际生产。 |
| 7. | Owing to considering the existence of stress concentration , to carry out de - sign and check on interference fit joint of hub by the use of finite element method are more tally with the actual situation , thus more reasonable
由于考虑了应力集中的存在，用有限元分析方法对轴毂过盈联接进行设计和校核，更符合实际情况，从而更全理。 |
| 8. | Finite element method could not only obtain all the same stress of interference fit joint under ideal model as that obtained with elastic mechanics method , but also could analyze the contacting edge effect - edge stress concentration caused by con - tact , which could not be solved by elastic mechanics
有限元方法不仅可以获得与弹性力学完全一致的理想模型下过盈联接的应力等，还能够分析弹性力学所不能求解的接触边缘效应?由接触引起的边缘应力集中。 |
