旋轉機翼 的英文怎麼說

中文拼音 [xuánzhuǎn]
旋轉機翼 英文
rotor blade
  • : 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...
  • : 轉構詞成分。
  • : machineengine
  • : 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...
  • 旋轉 : revolve; gyrate; rotate; spin ; revolution; revolvement; rotation; circumgyration; circulation
  • 機翼 : [航空] wing; wing unit; aerofoil; airfoil
  1. Standard practice for continued airworthiness system for light sport gyroplane aircraft

    輕型運動自的持續適航系統的標準實施規程
  2. Copter rotors really spin, and cockpit and doors really open

    直升,駕駛艙門可關開!
  3. The stability of the tiltrotor in the heli copter mode is analyzed aiming t a semi span soft - inplane tiltrotor model with an elastic wing

    集成了非定常動態人流方程與傾過渡狀態的多體動力學力程,建立了傾時域非定常氣彈耦合分析模型。
  4. Standard specification for design and performance of light sport gyroplane aircraft

    輕型運動自的設計和性能的標準規范
  5. The rotor / wing aerodynamic interactions of the tilt rotor vehicle in hover is described in this dissertation

    本文主要研究的是傾飛行器懸停狀態時,之間的氣動干擾問題。
  6. When the tilt rotor vehicle is in hover, the aerodynamic download of the rotor flowfield imposes on the wing. in this time, the rotor / wing interaction is severe

    飛行器懸停時,的下洗流剛好作用在上,此時,間的氣動干擾非常劇烈。
  7. 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

    尖安裝可以傾的發動短艙和系統,可以在飛行中根據需要在固定模式和直升模式之間換,充分發揮直升垂直起降、懸停及固定高速巡航的優點。
  8. 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

    由電動全速運帶動主軸,經主軸動乳化框槽內之乳化片,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葉片;連續使乳化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。
  9. The aerospace indu * * * y is the complex of manufacturing concerns engaged in the production of flight vehicles, including unpowered gliders and sailplanes, lighter than air - craft, ground - effect machines, heavier than air craft of both fixed - wing and rotary - wing varieties, military missiles, space launch vehicles, and manned or unmanned spacecraft ; propulsion systems and other thrusting devices ; on board equipment essential to the design purpose of the flight vehicle ; and ground - based support equipment needed for the operation and maintenance of the flight vehicle

    航天工業是一個綜合製造行業,從事各種飛行器的生產,包括:各種無動力滑翔,輕于空氣的飛行器,地面效應械設備,重於空氣的各種固定和旋轉機翼飛行器,軍用導彈,太空發射器,載人或無人飛行器,推進系統或其他助推設備,對飛行器的設計至關重要的艙內設備,控制和維護飛行器的地面設備。
  10. Standard specification for rotary wing basic life support, advanced life support, and specialized medical support air ambulances

    旋轉機翼的基本生命保障高級生命保障和專業醫療保障救護飛的標準規格
  11. An aircraft powered by a conventional propeller and supported in flight by a freewheeling, horizontal rotor that provides lift

    在飛行中以常規的螺槳來驅動並靠慣性滑行支持的,提供升力的水平
  12. Frequency tests of helicopter rotating rotor blade

    直升狀態下槳葉固有頻率的測試
  13. The problems with the wing and the rotating joint could delay future missions. the parts are needed to generate the power to support new equipment

    結合器的問題會延遲將來的任務完成。零件需要發電來提供更多的儀器使用。
  14. Furthermore, because rotors are mounted on the tips of the wing, the rotor / pylon / wing aerodynamic interactions are also included in the model. such factors reflect the unsteady and nonlinear characteristics in the model

    此外,傾安裝在尖,/發動短艙/之間的氣動干擾是建模的一個難點。
  15. Numerical simulations demonstrate that the multi body analytical model can analyze the aeroelastic stability of the tiltrotor aircraft in the helicopter mode

    數值計算表明:建立的多體動力學模型能夠快速分析直升模式下傾復雜的氣彈耦合動力學特性。
  16. The aerospace industry is the complex of manufacturing concerns engaged in the production of flight vehicles , including unpowered gliders and sailplanes , lighter than air - craft , ground - effect machines , heavier than air craft of both fixed - wing and rotary - wing varieties , military missiles , space launch vehicles , and manned or unmanned spacecraft ; propulsion systems and other thrusting devices ; on board equipment essential to the design purpose of the flight vehicle ; and ground - based support equipment needed for the operation and maintenance of the flight vehicle

    譯文航天工業是一個綜合製造行業,從事各種飛行器的生產,包括:各種無動力滑翔,輕于空氣的飛行器,地面效應械設備,重於空氣的各種固定和旋轉機翼飛行器,軍用導彈,太空發射器,載人或無人飛行器,推進系統或其他助推設備,對飛行器的設計至關重要的艙內設備,控制和維護飛行器的地面設備。
  17. The aerospace industry is the complex of manufacturing concerns engaged in the production of flight vehicles, including unpowered gliders and sailplanes, lighter than air - craft, ground - effect machines, heavier than air craft of both fixed - wing and rotary - wing varieties, military missiles, space launch vehicles, and manned or unmanned spacecraft ; propulsion systems and other thrusting devices ; on board equipment essential to the design purpose of the flight vehicle ; and ground - based support equipment needed for the operation and maintenance of the flight vehicle

    航天工業是一個綜合製造行業,從事各種飛行器的生產,包括:各種無動力滑翔,輕于空氣的飛行器,地面效應械設備,重於空氣的各種固定和旋轉機翼飛行器,軍用導彈,太空發射器,載人或無人飛行器,推進系統或其他助推設備,對飛行器的設計至關重要的艙內設備,控制和維護飛行器的地面設備。
  18. 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

    本文重點推導了帶葉間減擺器(減擺器帶三個外伸量:展向,垂向和方向)的/體耦合系統的非線性動力學方程,針對該方程提出了一種改進的多槳葉坐標變換方法。
  19. Study on dynamics mechanism of landslide with locked flank in plane rotation

    鎖固平面式滑坡動力學理分析
  20. In order to understand the rotor / wing interaction each other, firstly, the change of the isolate rotor thrust with the collective pitch and rotate speed is tested, secondly, the change of the rotor thrust with the collective pitch, rotate speed and the wing / rotor distance is scaled, when the wing is placed underside the rotor, lastly, the pressure on the wing due to the rotor wake is scaled

    為了搞清楚它們之間的相互影響,本文首先測量孤立的拉力隨總距和速的變化;再測量有的拉力隨總距及速的變化以及隨間的距離變化;最後測量尾流對表面壓力的影響。
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