| 1. | Rod bodies in aluminium alloy for flight controls - technical specification
飞行控制用铝合金拉杆.技术规范 |
| 2. | Aluminium alloy rod body for flight control and aircraft structure . dimensions
飞行控制和飞机结构用铝合金杆.尺寸 |
| 3. | Aluminium alloy rod body for flight control and aircraft structure . technical specification
飞行控制和飞机结构用铝合金杆.技术规范 |
| 4. | Rod bodies , flight control in aluminium alloy , for adjustable end fittings - dimensions and loads
飞行控制可调节终端配合铝合金杆.尺寸和荷载 |
| 5. | En 2289 aerospace series . rod bodies in aluminium alloy for flight controls . technical specification
航空航天系列.飞行操纵系统用铝合金制杆体.技术规范 |
| 6. | Aerospace series - rod bodies in aluminium alloy for flight controls - technical specification ; german version en 2289 : 1996
航空航天系列.飞行控制用铝合金制棒料.交货技术条件 |
| 7. | Aerospace series . rod bodies , flight control in aluminium alloy for adjustable end fittings . part 1 : dimensions and loads
航空航天系列.棒材可调节末端配件用铝合金飞行控制.第1部分:尺寸和负载 |
| 8. | Aerospace series - rod bodies flight control in aluminium alloy , for adjustable end fittings - part 1 : dimensions and loads ; german version en 2290 - 1 : 1998
航空航天系列.可调节控制杆端部接头的铝合金飞行控制 |
| 9. | The failure of reinforced plastic fiberglass sucker rod is classified into break and thread off , and the break of the rod body is the common failure pattern
玻璃钢抽油杆的失效类型分为断杆和脱扣两种，杆体的劈断和劈散是其最常见的失效形式。 |
| 10. | Abstract : presents the model established for calculation of reliability of connecting rod fatigue strength , and stress analysis made with the connecting rod body of diesel engine , and the reliability calculations made with the connecting rod of 6200zcl diesel as an example for infinite life , and concludes that this method also suits other components with infinite life
文摘:连杆的主要破坏形式是疲劳破坏，疲劳破坏是连杆按强度失效的主要故障模式.本文根据机构可靠性的基本原理，建立了连杆疲劳强度可靠性的计算模型.对直列式柴油机连杆杆身进行了应力分析，并结合6200zcl型柴油机连杆的具体实例，进行了无限寿命下的疲劳强度可靠性计算，所得结果与实际工程情况相符.阐明了所提供方法的具体应用，这种方法对其它寿命很长的机构构件同样适用 |
