外伸的三脚架有高型和低型两种配置，以满足不同的环境要求。
The outrigger tripod is available in both a high and low profile version, to fulfill a diverse array of environmental requirements.
当离合器踏板按下时，电缆或者液压活塞将推动离合器分离叉杆，离合器分离叉杆推着外伸的轴承贴在膜片弹簧的中间。
When the clutch pedal is pressed, a cable or hydraulic piston pushes on the release fork, which presses the throw-out bearing against the middle of the diaphragm spring.
受到侵犯时，它会将身体作一点点的弯曲，这样可以露出他们锋利的外伸的鳞片。
They seem to have a way of "turning" away aggressors by bending a little to expose their sharp scales that sort of stick out when the fish is bent.
对于具有复杂边界条件的矩形外伸板，在弹性薄板理论中是一个较难解决的问题。
In the theory of elastic thin plates, to solve the problem of rectangular overhanging plates with complicated boundary conditions is very hard for long.
结论肘关节后外侧旋转不稳定除桡侧副韧带的损伤外，可能还有外侧伸肌及伸肌腱膜的损伤。
Conclusions Besides the injury of the radial collateral ligament, the injuries of the external musculus extensor and the aponeurosis can cause the posterolateral rotatory instability of the elbow.
【摘要】目的探讨外固定器背伸位固定治疗三踝骨折时使后踝骨折稳定的最佳踝关节固定位置。
Abstract Objective To find out stable position of posterior malleolar fracture when trimalleolar fractures were treated by external fixation in dorsiflexion position.
网球肘足前臂腕伸肌过度使用的常见病，又称肱骨外上髁炎。
Tennis elbow is a common overuse syndrome of the extensor tendons ofthe forearm.
本文通过34个外伸梁试验，研究了钢筋在反弯点区段的锚固性能。
In this paper, the bond behavior of reinforcing bars in the region withinflexion point was investigated through 34 cantilever beam tests.
结论外固定器背伸位固定治疗三踝骨折时后踝骨折稳定的最佳踝关节固定位置是背伸中立位。
Conclusions Stable position of posterior malleolar fracture when trimalleolar fractures are treated by external fixation is dorsiflexion-neutral position.
而当中间盘比外伸盘质量小很多时，系统的振动响应会降低。
When mass of mid-span is lesser than that of overhung rotor, the response of system will decrease.
对有端板加劲肋的外伸端板连接节点进行了循环荷载作用下试验研究，分析加劲肋对外伸端板连接节点性能的影响。
Research on extended end-plate connection with end-plate stiffer under cyclic load by test, discuss the effect of stiffer on the capability of the connection.
针对一类航天器外伸结构的结构振动问题，提出了一种动应变控制方法。
Some space structures have critical vibration problems owing to their low stiffness and low damping.
针对一类航天器外伸结构的结构振动问题，提出了一种动应变控制方法。
Some space structures have critical vibration problems owing to their low stiffness and low damping.
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