1·Connection apparatus for a helicopter rotor blade, comprising.
连接装置的直升机转子叶片，其中包括。
2·A new way to solve dynamical response of rotor blade in helicopter.
提出了一种全新的计算旋翼桨叶动力响应的方法。
3·A new way to solve dynamical response of rotor blade in helicopter.
提出一种面向设计的复合材料旋翼桨叶结构动力优化方法。
4·Gravity center modification method can be used in high-load rotor blade design...
重心线调节法可应用于高负荷叶片设计。
5·The airfoil member according to claim 1, configured as a rotor blade for a helicopter.
翼型会员根据权利要求1 ，配置为转子叶片为直升机。
6·A simple puff of air will send the rotor blade spinning and get the LED lights glowing.
简单的空气粉扑将发送转子叶片旋转并获得LED灯发光。
7·Rotor blade vibration measurement kept the high-speed rotating blades stable in property.
高速 旋转 叶片在使用中性能稳定。
8·Gravity center modification method can be used in high-load rotor blade design in engineering.
重心线调节法可应用于高负荷叶片设计。
9·The helicopter rotor blade deicing technique is greatly important to ensure the flight safe - ty.
直升机旋翼桨叶除冰技术对保证直升机飞行安全是十分重要的。
10·The cause of water erosion in the end rotor blade of 100 MW steam turbine is analyzed with solution proposal.
对神木发电有限公司100 MW汽轮机末级动叶片水蚀原因进行了分析，并提出了解决方案。