翼軌 的英文怎麼說

中文拼音 [yìguǐ]
翼軌 英文
wing rail （of frog）
  • 翼 : Ⅰ名詞1 （翅膀） the wing of a bird 2 （像翅膀的東西） the wing of an aeroplane etc : 鼻翼 wing of...
  • 軌 : Ⅰ名詞1. （路軌;軌道） rail; track 2. （比喻辦法、規矩、秩序等） rut; path; course Ⅱ動詞[書面語] （遵循; 依循） follow
  1. The delta-winged columbia, before reaching the orbit, jettisoned its dual booster rockets two minutes into flight.

    三角翼的哥倫比亞號航天飛機在進入軌道前，起飛兩分鐘就拋下其兩個助推火箭。
  2. The model contains nose rail, wing rail, locking hooks and all relative components. the crossties are simplified as elastic foundations. thus, the model reveals the real working state of the locking hooks

    論文中採用的計算模型包括心軌、翼軌、鎖閉鉤等幾乎所有的相關部件，沒有建模的枕木及地基也做了相應的簡化處理，並引入到了邊界條件中，比較真實地反映了鎖閉鉤的真實受力狀態。
  3. 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，並分別給出主襟翼和子襟翼驅動機構的不同設計方法。
  4. A multi - phase homing project was obtained, including three different homing trajectories according to the height of initial point being high, or proper, or short. and selection criterion for trajectories was also discussed

    提出了翼傘系統歸航軌跡的分段設計方案，按高度冗餘、高度適中和欠高度三種情況給出了不同的歸航軌跡分段設計方法，並且探討了對應的判斷準則。
  5. Rapid driving of eastern railway transportation tunnel of xutuan coal mine

    許疃煤礦東翼軌道運輸巷道快速施工技術
  6. Air regulation systems in mining - wing air doors for haulage tracks - double - wing type doors with pressure reduction

    采礦的空氣調節系統.運輸軌道翼形通氣門.減壓式雙翼
  7. The objective of the investigation was to determine the circumstances and the causes of the accident with a view to the preservation of life and the avoidance of accidents in the future

    發言人說:根據飛機營運商港龍航空公司提供的資料，該襟翼導軌整流罩在近期一次例行檢查后拆除作維修。
  8. 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。發言人指出根據飛機製造商的保養及運作指引，飛機可以在未裝上新的襟翼導軌整流罩期間繼續飛行。
  9. 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，民航處發言人今日（七月二十八日）澄清該襟翼導軌整流罩並非如報道所言在飛行中掉下。
  10. There are two methods for welding radial stiffeners to bias - rail box girder : welded all around and open at tensile flange

    摘要起重機偏軌箱形梁橫向加強板有加強板四周均焊和在受拉翼緣處空開2種焊接方式。
  11. Thirdly, in term of the results of testing and calculation, the displacement and libration, the difference of altitude, the flexibility and strain of crane - beams are all generally analysed, especially the reason why the crane - beams are attaint is lucubrated, and the reasons why the trigging pole is ruptured, the upper wingspan is damaged, the orbital movement, the exceptional incline of colums are open out, which has instructional significances that improve the design of the steel frame of the coke made by dry flameout

    第三，根據檢測和計算結果，對鋼框架的位移和振動、框架高差、吊車梁撓度和應變等進行了全面的分析，特別對吊車梁系統的損傷原因進行了深入分析，揭示了制動桿件斷裂、上翼緣磨損、軌道竄動、柱異常傾斜等一系列損傷現象的原因，對于改進干熄焦鋼框架的設計有著直接的指導意義。
  12. When escape system is activated, the grille wings at the upper fairing will open, supporting frame will pick up the orbit and returning modules, the lock between the returning and propelling modules will release, the lock between the upper and lower fairings will release, escape rocket will be ignited and finally pull the escape flight vehicle away from the rocket

    該系統由逃逸塔和上部整流罩組成，逃逸系統加上飛船的軌道艙和返回艙構成逃逸飛行器。當需要逃逸時，上部整流罩上的柵格翼打開，支撐機構夾住飛船軌道艙和返回艙，然後返回艙與推進艙解鎖上下整流罩解鎖逃逸發動機點火，逃逸飛行器飛離運載火箭。
  13. Compared with the xv - 15 flight test data, the results are reasonable and effective. improved guidance schemes will be needed, especially in the terminal area for safety and economic viability

    傾轉旋翼飛機起飛過程包含完整的過渡模式，為提高飛機的可靠性和安全性，必須對其起飛軌跡進行控制。
  14. The three basic steps are as follows : firstly, the flow field is computed. secondly, the droplet trajectory equation is solved in order to determinate the limiting droplet trajectories and local collection coefficient. thirdly, a new iced shape is defined according to ice accretion model

    其基本步驟一般分三步：計算物體的繞流流場；求解水滴軌跡方程以確定極限水滴軌跡和收集系數；根據冰增長模型來確定新的結冰翼型形狀。
  15. For specified three work positions as design inputs, the thesis evaluates their geometrical movements of the prime and sub - flaps, and some reasonableness are shown in view of kinematical geometry. the work can provide further aerodynamic analysis with variable wing geometrical data

    以三縫襟翼的3個假定的工作位置作為設計輸入，算出了3種不同軌道下襟翼的運動結果，並從幾何角度進行了簡單對比分析，為進一步的氣動分析提供輸入數據。
  16. With the demands of designing the large - scale cargo airplane, in this thesis, many technical materials about the mechanisms of current wing flap types, of foreign transport airplanes are carefully studied at first, and the mechanical composition of three - gaps - fowler - flap is summarized technically about its major basic components, prime mechanism ( track ), driving device, sub - flaps mechanism and the sub - flaps sequential control system

    在本文中，針對大型運輸機機翼設計的需求，首先對幾種國外運輸機襟翼運動機構的資料進行仔細研究，對三縫富勒襟翼運動機構的組成進行了分析，總結歸納出了三縫富勒襟翼運動機構的3個基本組成部分：主機構（軌道） ，驅動機構，子襟翼機構及子襟翼運動控制機構。
  17. Thirdly, the air - air missile ' s model is studied, and set up guided missile motion equations that passes through the area of the down wash. using the preceding down wash distributing data, the fly situation and orbit changes in initial stages of the guided missile launch have been studied

    再次，對空空導彈的模型進行了研究，並建立了導彈穿越旋翼下洗區域的運動方程，運用前面的下洗分佈數據，研究了導彈發射最初階段的運動情況和軌跡變化。
  18. Then the traditional pd controller and gain - scheduling fuzzy pd controller were designed to realize path following of parafoil system. simultaneously, several control strategies were brought forward in view of the basic flight properties of parafoil system. the important one was described as following : the

    同時，基於翼傘系統基本運動特性，提出了一系列有針對性的控制策略，其中重要的一條是，將平均風的影響在軌跡歸航中修正，而大氣紊流的影響作為干擾由控制器來補償。
  19. The comparison of the computational results of flap movements indicates that three operational positions of the wing flaps guided through the different tracks are nearly close to each other and the non - arc - track is better to guide the flaps to the original three positions exactly

    計算結果表明，不同的軌道下所得的襟翼3個工作位置從幾何角度看比較接近，其中非圓弧軌道能夠使襟翼在3個工作位置與預先設計的姿態完全相同。
  20. Use the collective to make the loop as round as possible

    控制主旋翼的螺距，盡可能使飛行軌跡成為圓形的環狀。
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