槳葉擺動 的英文怎麼說

中文拼音 [jiǎngbǎidòng]
槳葉擺動 英文
blade swing
  • : 名詞1. (劃船用具) oar; paddle 2. (螺旋槳) propeller
  • : Ⅰ動詞1 (安放; 排列) put; arrange; set in order 2 (顯示; 炫耀) display; show off; put on; assu...
  • 槳葉 : awe; paddle
  • 擺動 : 1 (搖擺) swing; sway; oscillate; pendulate; waggle; wobble; vibrate; wiggle 2 [機械工程] jiggin...
  1. Within this analytical model, the factors as unsteady aerodynamic and blade flap / lead - lag coupled motion are both considered

    旋翼機體耦合力學模型考慮了非定常空氣力和揮舞振運耦合。
  2. The flight test of ec155 tells us that inter - blade dampers can work very well in stabilizing the system ; another advantage of this configuration is it can make the hub system simpler and reduce the drag of air to the hub which is very important for helicopters with 4 or more than 4 blades

    Ec155的飛行試驗證明,這種減器布置方式對提高穩定性效果明顯;這種布置方式的另外一個優點是可以簡化轂,降低其氣阻力,對多(四片和四片以上)直升機有重要意義。
  3. To improve the stability, one common method is to install dampers at the roots of blades. however, commonly used dampers can hardly meet different demands when helicopter working in different conditions

    為提高旋翼/機體耦合穩定性,一般採用在根部安裝減器的方法,但目前常用的減器很難滿足直升機不同工作狀態下對振器阻尼的不同需求。
  4. Damping was then determined via exciting the equation at the critical frequency to get the transit decay which was then analyzed with the moving - block method. in chapter 4, the nonlinear dynamic equation of rotor - body system with inter - blade dampers ( taking all possible attachment offsets into consideration, spanwise offset, vertical offset and in - plane offset ) was modeled

    本文重點推導了帶間減器(減器帶三個外伸量:展向,垂向和旋轉方向)的旋翼/機體耦合系統的非線性力學方程,針對該方程提出了一種改進的多坐標變換方法。
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