高速旋翼 的英文怎麼說

中文拼音 [gāosùxuányì]
高速旋翼 英文
high-speed rotor
  • 高 : Ⅰ形容詞1 （從下向上距離大; 離地面遠） tall; high 2 （在一般標準或平均程度之上; 等級在上的） above...
  • 速 : Ⅰ形容詞（迅速; 快） fast; rapid; quick; speedy Ⅱ名詞1 （速度） speed; velocity 2 （姓氏） a surna...
  • 旋 : 旋Ⅰ動詞1 （旋轉） whirl 2 （用車床切削或用刀子轉著圈地削） turn sth on a lathe; lathe; pare Ⅱ名詞...
  • 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...
  • 高速 : （高速度） high speed; high velocity （hv）; high rate; swift; fast; express; high-speed
  • 旋翼 : helicopter rotor
  1. Tilt - rotor aircraft combine the vertical takeoff and landing ( vtol ) capability of helicopters with the high speed performance of turboprop airplanes. located at the tips of the wing, the prop - rotors act as helicopter rotors when flying vertically and as airplane propellers in cruising flight

    傾轉旋翼飛機翼尖安裝可以傾轉的發動機短艙和旋翼系統，可以在飛行中根據需要在固定翼模式和直升機模式之間轉換，充分發揮直升機垂直起降、懸停及固定翼飛機高速巡航的優點。
  2. The dynamo runs at rull speed to drive main shaft, then the main shaft makes the emulsifying wings in emulsification grove rotate, which absorbs the liquid in its brand groove into ring groove through guide vanes on upper and lower sides of the groove. the vanes spins circularly at high speed with the main shatf as center, and the blade and emulsificaton groove cut and crush it continuously. after that. it gers squeezed by the vanes highspeed centrifugal rotation. at last, it finishes isotropt emulsification tratment within extremely short time after continuous circulating mixing

    由電動機全速運轉帶動主軸，經主軸轉動乳化框槽內之乳化翼片，使其將桶槽內之液體經框槽上、下兩側之導流葉片吸入環狀框槽內，經以主軸為中心高速圓周旋轉葉片；連續使乳化翼端刀面與乳化框間極小之間系高頻率之強力切割剪斷、粉碎，再借葉片高速離心旋轉排擠，持續循環混合，以極短之時間即可完成均質乳化之處理。
  3. Fly straight and level form left to right as the helicopter is just about in front of the pilot, pull back cyclic, adjust the collective to maintain constant altitude and speed and hold the back cyclic as the helicopter completes one ( 1 ) full traveling tumbling back flip to upright

    由左至右保持水平直線飛行，當直升機在操控者的正前方時，將升降舵拉升舵，控制主旋翼的螺距使直升機保持固定的高度及前進速度，向後翻滾一圈完畢。
  4. Fly straight and level from left to right at a moderate speed as the helicopter is just about in front of the pilot, add extra collective momentarily, then simultaneously push forward cyclic, and adjust the collective to maintain constant altitude and speed and hold the forward cyclic until the helicopter completes one ( 1 ) full traveling tumbling front flip to upright

    由左至右保持適當速度的水平直線飛行，當直升機在操控者的正前方時，瞬間加大主旋翼的螺距，同時將升降舵打降舵，控制主旋翼的螺距使直升機保持固定的高度及前進速度，直到直升機向前翻滾一圈完畢。
  5. Such planes could fly to their destinations with the speed of their short wings, then extend their inflatables to burn less fuel while they loitered or slowed down for landing

    這麼一來，這類飛機可用較短的機翼提高速度飛到目的地，並在盤旋或減速準備降落時，拉長充氣式機翼，以減少燃料消耗。
  6. With the helicopter flying sideways nose - out straight and level from right to left, tumble the helicopter forward while traveling sideways, use collective to maintain altitude and speed across the ground, complete at least one ( 1 ) tumble

    保持機尾朝向操控者，由右向左開始橫向水平飛行，將升降舵打降舵，控制主旋翼的螺距，使機體能保持固定的高度及橫向速度，至少完成一個前滾翻。
  7. With the helicopter flying sideways nose - out straight and level from right to left, roll the helicopter to the left ( the same direction as the helicopter is flying ), use collective to maintain altitude and speed across the ground, complete at least one ( 1 ) roll

    保持機尾朝向操控者，由右向左開始橫向水平飛行，將副翼打左舵（與橫向飛行的方向同向） ，控制主旋翼的螺距，使機體能保持固定的高度及橫向速度，至少完成一個側滾。
  8. Application of rotor autoratation to lift transfer

    旋翼自轉狀態在高速直升機升力轉移過程中的應用
  9. At last, pointing to the temporal characteristics and the spectral characteristics, this paper discussed the methods for estimating the maximal line velocity ( vmax ) and the glint periods ( tp ) of the hovering helicopter, and then fulfilled the recognition of hovering helicopter using these two message. in chapter 5, the summary of all the works in the paper and related conlusions are presented, and the defects are analized at last, at last this paper demonstrated the d

    最後，本文針對懸停直升機旋翼回波的時頻域特點，探討了從回波信號中提取旋翼回波最大線速度v和旋翼回波閃爍周期tp的方法，在綜合利用這兩種信息的基礎上完成了彈載高重頻脈沖多普勒體制雷達對懸停直升機回波信號的識別。
  10. I strongly advise you not to do this trick at all. if you do it, do it over water. this trick is also called death spiral : for a reason ! !

    首先：不建議做這個動作；其次如果你要做，那就在水面上作。在50米的高度上進入螺旋，螺旋速度不要太快，只需要你自己的水平位置比內側翼尖稍高，然後接近地面。
  11. Time the input of the cyclic & collective commands such that the helicopter maintains constant altitude, direction & speed

    安排副翼、升降舵及主旋翼螺距的打舵時機，使得直升機能保持固定的高度、前進方向及速度。
  12. Emulation results show that the supposed attack system can rapidly trace the motion target to satisfy the launching condition, attack the target successfully and display the launch process under the wing down wash. it offers better emulation foundation for improving the percentage of hits and fight accurately

    模擬結果表明，本文建立的攻擊系統，能夠快速的跟蹤目標，實現目標攻擊，並反應了有旋翼下洗影響的導彈發射過程，為提高命中率精確作戰提供了較好的模擬基礎。
  13. Fixed - wing attack types share some similarities with their rotary - wing counterparts, but due to the speed at which the aircraft moves and the differences of fw compared to rw aircraft, they are distinctly different attack types that must be mastered separately

    固定翼飛機的部分攻擊方式與旋翼機相似，但由於其飛行速度與旋翼機不同，另外個別的攻擊方式明顯不同並且高明許多。
  14. The comparison showed that : ( l ) farassat 1a formula is the simplest one and work well for the subsonic rotor. ( 2 ) both kirchhoff formula and k - fwh formula can predict the nonlinear noise generated by transonic rotor ; ( 3 ) when the surface is not positioned in the linear region, kirchhoff approach for rotating integration surface could lead to substantial error, but k - fwh formula can still work well

    數值研究表明： farassat1a公式在預測線性噪聲方面簡單有效，適用於亞音速旋翼的噪聲預測； kirchhoff公式和k - fwh公式均能夠預測跨音速旋翼聲場，並且具有較高的精度；當聲源面位於流動非線性時， kirchhoff公式會導致很大的計算誤差，而k - fwh公式不存在這樣的問題。
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