flapping track中文是什么意思

發(fā)音:

中文翻譯
造句

揮舞參數(shù)

flapping 揮拍的; 揮舞的; 拍動; 拍平; 拍水現(xiàn)象; 撲動; 振顫; 振動
blade flapping 槳葉揮舞
flapping (of belt) 波動（皮帶）
flapping acceleration 揮舞加速度
flapping action 揮舞運動
flapping angle 揮舞角; 翼動角
flapping articulation 揮舞鉸聯(lián)接; 舞鉸
flapping blade 揮舞槳葉
flapping equation 揮舞方程
flapping flexibility 揮舞撓性
flapping flight 撲翼飛行
flapping frequency 揮舞頻率
flapping hinge 揮舞鉸鏈; 撲動鉸鏈（航空用）
flapping inertia 揮慣性矩
flapping mechanism 旋翼揮舞調節(jié)器
flapping motion 旋翼揮舞運動
flapping movement 揮舞運動; 振翅撲擊樣運動,撲翼樣運動
flapping oscillations 撲翼振動
flapping piston 揮舞平面
flapping rotor 揮舞鉸接式旋翼
flapping screw 緊繩螺旋
flapping sound 拍擊音
flapping sounds 拍擊聲
flapping stop 揮舞限動塊
flapping strip 下垂帶材

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例句與用法

Its absence does not have any flight safety implication . " he said that under the maintenance and operation guidelines of the aircraft manufacturer, the aircraft could continue flying with the flap track fairing removed pending replacement
除去整流罩對飛行安全不會構成影響。發(fā)言人指出根據(jù)飛機制造商的保養(yǎng)及運作指引，飛機可以在未裝上新的襟翼導軌整流罩期間繼續(xù)飛行。
July 28, 2005 in response to press reports today ( july 28 ) regarding a flap track fairing falling from an a330 of ka 363 flying from tokyo to hong kong on july 22, 2005, a spokesman for the civil aviation department ( cad ) clarified that the flap track fairing did not fall off in flight as reported
就傳媒報道有關七月二十二日，由東京返港航班編號ka363的a330型客機的襟翼導軌整流罩掉下，民航處發(fā)言人今日（七月二十八日）澄清該襟翼導軌整流罩并非如報道所言在飛行中掉下。
July 28, 2005 in response to press reports today ( july 28 ) regarding a flap track fairing falling from an a330 of ka 363 flying from tokyo to hong kong on july 22, 2005, a spokesman for the civil aviation department ( cad ) clarified that the flap track fairing did not fall off in flight as reported
就傳媒報道有關七月二十二日，由東京返港航班編號ka363的a330型客機的襟翼導軌整流罩掉下，民航處發(fā)言人今日（七月二十八日）澄清該襟翼導軌整流罩并非如報道所言在飛行中掉下。
Based on the kinematical design criterion of equi-chord percent ratio and spatial rigid body guiding mechanism, three theoretical design methods of arc track, non-arc track, and helical track are proposed in this thesis, meanwhile, different design methods about prime flap and sub-flap driving mechanisms are completed . three cases of different three-gaps-fowler-flap tracks are designed
對后緣三縫富勒襟翼工作時的3個關鍵位置，按照“等弦長百分比”運動的設計準則和空間剛體引導機構的設計思路，提出了圓弧軌道、非圓弧軌道和螺旋線軌道等3種空間位置引導軌道的設計原理，并分別給出主襟翼和子襟翼驅動機構的不同設計方法。