Using conventional wiring, approx. 120 lines used to be laid along the trailing cable, whereas this crane system requires a mere 10 wires - 5 for AS Interface, 5 for the load.
下面的对照，我们会清楚地了解这一优点：通常一个典型的案例我们需要在托链线缆槽中需要布置大致120根线缆，然而，使用新技术我们只需要总共10根电缆－5根AS-interface电缆和5根动力电缆。
Gross load hauled load hauled trailing load.
全部被牵引车辆的自重及其载荷。
On the basis of the tests for single casing pile and the casing pile cluster used for integral trailing of drilling rigs, the authors conduct an investigation in the concerned proper & ties of the piles, including load capacity, destructive condi-tions, horizontal displacement, etc.
本文通过对套管单桩和用于钻机整拖的套管群桩的试验，对套管桩的有关参数，如承载能力、破坏条件、水平位移等进行了分析和研究。
Compared with the cascade without slot, the surface load of cascade with slot increases near the leading edge and trailing edge and decreases at the slot inlet. Experimental Investigation on the Film-Cooling Adiabatic Effectiveness with Different Slot Inlet Hole Pitches
通过开槽处理，改变了叶栅表面的静压分布，使叶栅前段、后段的负荷增大，小槽进口附近的负荷减小.不同缝槽进气孔间距的纯气膜绝热温比试验研究
This thesis, which is devoted to the research on the smart rotor with actively controlled trailing-edge flap for hub oscillatory load reduction, offers a potential approach for the vibration reduction of helicopter.
本文对带有主动控制后缘附翼的智能旋翼用于降低桨毂交变载荷进行探索性的研究，为降低直升机飞行中机体振动水平提供一条有效的新途径。
The load on the rotating cascade along the blade span direction assumes a uniform distribution, and the load in the chord direction is mainly undertaken by the arc segment close to the trailing edge.
动叶栅在叶展方向上的载荷分布均匀，弦向载荷主要由接近尾缘的弧段承担；
If the waterworn notch exists at the blade's trailing edges, the blade's fatigue life will be shortened in the load scope of 40~60MW, so the long-term operation in this load scope should be avoided.
若出汽边存在水蚀缺口，在40～60MW负荷范围的疲劳寿命较短，应避免在此负荷范围长期运行；
High load multi-stage compressor is the most complex part of aero engine, the technological difficulty is how to get the distribution of aerodynamic parameters along the leading and trailing edge of blades under all working conditions and the whole engine performance quickly, completely and accurately.
高负荷多级压气机是最具技术挑战的航空发动机关键部件之一，其技术难点在于如何快速、完整、准确地获得全工况下叶片前尾缘气动参数分布和整机特性结果。
If the waterworn notch exists at the blade's trailing edges, the blade's fatigue life will be shortened in the load scope of 40 ~ 60MW, so the long-term operation in this load scope should be avoided.
若出汽边存在水蚀缺口，在40～60MW负荷范围的疲劳寿命较短，应避免在此负荷范围长期运行；