main rotor blade中文是什么意思

• 主旋翼桨叶

• "main"中文翻译    adj. 1.主要的，主，全，总。 2.充分的，尽量的； ...
• "rotor"中文翻译    n. 1.【电机】转子 〔cf. stator〕; 动片 ...
• "blade"中文翻译    n. 1.(壳、草等的)叶片，叶身，叶。 2.刀片；(安 ...
• "main rotor blade area" 中文翻译 :    旋翼桨叶面积
• "main-rotor blade" 中文翻译 :    旋翼桨叶
• "blade rotor" 中文翻译 :    叶片转子
• "rotor blade" 中文翻译 :    水轮机转轮叶片; 旋转机翼; 转动叶片; 转子刀片; 转子叶片
• "main rotor" 中文翻译 :    水平旋翼; 主机转子; 主旋翼; 主转子
• "moving blade rotor blade" 中文翻译 :    动叶
• "anchorage of the rotor blade" 中文翻译 :    转子叶片的固定
• "blade rotor type" 中文翻译 :    旋转式锄铲
• "blade wheel rotor" 中文翻译 :    叶轮型转子; 叶轮转子
• "ceramic rotor blade" 中文翻译 :    陶瓷动叶片
• "fiber-glass rotor blade" 中文翻译 :    玻璃纤维旋翼桨叶
• "fibre rotor blade" 中文翻译 :    纤维旋翼桨叶
• "flexible-blade rotor" 中文翻译 :    柔性桨叶旋翼
• "four-blade rotor" 中文翻译 :    四叶旋翼
• "four-blade rotor helicopter" 中文翻译 :    四叶旋翼直升机
• "non uniform rotor blade" 中文翻译 :    变速叶轮叶片
• "non-uniform rotor blade" 中文翻译 :    变速叶轮叶片
• "rotor blade angle" 中文翻译 :    转子叶片安装角
• "rotor blade feathering" 中文翻译 :    旋翼桨叶周期变距
• "rotor blade flapping" 中文翻译 :    旋翼桨叶挥舞
• "rotor blade folding" 中文翻译 :    旋翼桨叶收折
• "rotor blade tab" 中文翻译 :    旋翼桨叶调整片

• The left skid was substantially damaged . the main rotor blades remained intact but were bent and twisted
  主旋翼桨叶被折弯和扭曲，但保持完整。
• Examination of the wreckage trail indicated that substantial damage was inflicted on the aircraft , in particular the main rotor blades , within the first few metres after initial impact
  坠机路线调查显示，直升机尤其是主旋翼桨叶，在首次撞击后的最初数公尺受损严重。
• Main rotor blades were severed within the first few metres through contact with small trees and rocks , and the underbelly and right side of the fuselage were damaged substantially
  主旋翼桨叶在直升机冲前首数公尺处因碰触地面矮小树丛和石块而断裂，机腹和右侧严重损毁。
• But the variation of its aerodynamic forces will induce flapping motion and produce the cyclic pitch on the main rotor blades by the bell mixing mechanism . in order to study the effect of bell - hiller stabilizer bar on helicopter stability and control , this paper first analyze the function and the principles , give the flapping equation and a flight dynamic model with bell - hiller stabilizer bar . and then works over the stability and control of uav r - 50 in hover and cruise condition , and analyzed the influence from parameters of the bar to it
  为了深入研究希勒伺服旋翼对直升机稳定性和操纵性的影响,本文首先分析了希勒伺服旋翼的功能和工作原理,推导了伺服旋翼的挥舞运动方程,建立了带有希勒伺服旋翼直升机的飞行动力学模型,然后以yamahar - 50无人直升机为例,分析该直升机在悬停和前飞时的平衡、稳定性和操纵性,在此基础上进一步研究希勒伺服旋翼设计参数变化对直升机稳定性和操纵性的影响。

• main rotor blade перевод