转动叶片，转子叶片，动叶片

rotor blades───动叶片

razor blade───刮胡刀刀片；剃须刀片

rotor plane───[航]旋翼机

razor blades───(剃刀的)刀片(razorblade的复数)

rotor planes───[航]旋翼机

motor trade───汽车贸易

motor trades───汽车贸易

rotor clouds───[气象]滚轴云

motor boat───n.摩托艇

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.

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。

It provides the foundation to supervise and diagnose the cracks of rotor blade.───这就为转子叶片裂纹故障的监测与诊断提供了依据.

This NSMS ( noninterference stress - measurement system ) method is an alternative to the strain gauge rotor blade vibration.───此方法将在叶片的振动检测中取代应变计式检测装置.

Aeroelastic model is developed to analyze aeroelastic stability of helicopter rotor blade with swept tips.───通过建立具有后掠桨尖旋翼气弹稳定性的分析模型,研究后掠桨尖旋翼气弹的稳定性.

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.

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。

A rotor blade of titanium alloy TC 11 in an aero - engine fractured at the segment during service.───某型发动机在使用过程中一片钛合金转子叶片在叶根部发生断裂故障.

Rotor blade vibration measurement kept the high - speed rotating blades stable in property.───旋转叶片振动的测量可保证高速旋转叶片在使用中性能稳定.

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.

Connection apparatus for a helicopter rotor blade, comprising.───连接装置的直升机转子叶片，其中包括。

Rotor blade vibration measurement kept the high - speed rotating blades stable in property.

As a critical part of helicopter, rotor blade anti-fatigue design technique is one of the key to improving safety life and decreasing cost.

When tail rotor blade designed into soft in rotary plane, there is a new dynamical problem of coupling stability between tail rotor and tail boom for helicopters with one main rotor and tail rotor.

A rotor blade of titanium alloy TC 11 in an aero - engine fractured at the segment during service.

Dark mosquito shadows across the hilltops, rotor blades beating the air, stirring the ground, pressing down.

The disk formed by the rotor blades is what really flies.

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A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.

A simple puff of air will send the rotor blade spinning and get the LED lights glowing.