飛升主機 的英文怎麼說

中文拼音 [fēishēngzhǔ]
飛升主機 英文
lift engine
  • : Ⅰ動詞1 (鳥、蟲等在空中活動) fly; flit 2 (利用動力機械在空中行動) fly 3 (在空中飄浮遊動) fly...
  • : Ⅰ動詞1 (由低往高移動) rise; hoist; go up; ascend 2 (等級提高) promote Ⅱ量詞1 (容量單位) lit...
  • : machineengine
  1. The heng zhong group is in the light of innovation, serve, the business enterprise spirit of responsible and common development, will promote the service capital of ability, high quality of expand of the development ability, market of the operation ability, product of capital strategy ability, property further, powerful administration management ability, around main industry development, grow of core ability and whole advantage of exertive, make the heng zhong brand to be more greatly and stronger, contribute our strength for the tool machine manufacturing industry

    恆重集團本著創新、服務、盡責、共同發展的企業精神,將進一步提資本的運籌能力、資產的運作能力、產品的開發能力、市場的拓展能力、高質量的服務能力、強有力的行政管理能力,圍繞業發展、核心能力的培育和整體優勢的發揮,把恆重品牌做大、做精、做強,為床製造業的騰貢獻力量。
  2. Flying boat is a controllable aircraft that can flying in the air, the flotage provided by the helum - filled bag inside the flying boat can support the boat and it s load in the air, motor pushing it forward ; the direction is guided by the device on it s tail, going down of the boat is made by escaping the gas inside, it can rise or fall straightly or stay in the air, no necessity of special site for taking off

    艇是一種可操縱的浮於空中的行器。在行中要依靠內部充滿氦氣的氣囊提供的浮力,將艇及其載荷支持在空中,發動為其提供前進的動力,通過操縱尾翼上的降舵和方向舵控制艇的俯仰和方向運動,艇的下降是通過排放氣來實現的。艇可以垂直起降空中懸停,不需要有專用設備的起降場。
  3. This paper also tested each model and system - the second loop of qinshan nuclear power station ( the second term ) , computed the balance point , tested the performance of step disturbance and runback loads for system ( no adding adjustment system ) , analyzing the factors effecting the first tiptop rotate speed of turb and time which the rotate speed reach the tiptop

    在模擬模型上,完成了穩態計算、系統階躍擾動試驗、甩負荷試驗(未加調節系統)等測試,要監控和分析了汽輪動態特性中兩個重要參數:汽輪第一轉速、時間。
  4. Their primary purpose is to enable the efficient transition of departing aircraft from the airport to the upper level airways

    行程序要目的是幫助離港航迅速地從場爬到指定的航道。
  5. During helicopter slung - load flight, the main flight quality modes include : phugoid, dutch roll, longitude and latitude slung - load oscillation. according to the ads - 33e - prf specifications, the flight stability qualities had been evaluated

    外吊掛行過程中,體現行品質的運動模態要為荷蘭滾模態、縱向浮沉振蕩模態,以及吊掛物橫向、縱向振蕩模態。
  6. The main factors which affected the flight stability quality included : forward flight speed, slung - load and helicopter mass ration, slung - load aerodynamic forces and cable length, etc. through adjusting the above structure and performance parameters, rational flight parameters can be decided, which can ensure the safe helicopter mission operations of the slung - load flight

    影響行品質穩定性要求的要因素為:直行速度、吊掛物/直質量比、吊掛物氣動特性、吊掛鋼索長度等。通過對上述結構參數、性能參數的調節,可確定合理、經濟的行參數,保證安全、高效的完成直外吊掛行運輸任務。
  7. There are incidents in which flying model aircraft in the vicinity of main flight paths have endangered the safety of helicopters operating there

    以往曾經有模型在直要航道行的事例,影響直的安全。
  8. 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行,當直在操控者的正前方時,將降舵拉舵,控制旋翼的螺距使直保持固定的高度及前進速度,向後翻滾一圈完畢。
  9. 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行,當直在操控者的正前方時,瞬間加大旋翼的螺距,同時將降舵打降舵,控制旋翼的螺距使直保持固定的高度及前進速度,直到直向前翻滾一圈完畢。
  10. A helicopter is used to install a guide wire. the cables, which will be the bridge & acute ; s main support, are strung from tower to tower

    用來設置導線。作為大橋的要支撐,繩索被繃在塔之間。
  11. This thesis, which is devoted to the research on the smart rotor with actively controlled trailing - edge flap for hub oscillatory load reduction, offers a potential approach for the vibration reduction of helicopter

    本文對帶有動控制后緣附翼的智能旋翼用於降低槳轂交變載荷進行探索性的研究,為降低直行中體振動水平提供一條有效的新途徑。
  12. Because of the periodicity of the hub oscillatory load and the nonlinearity of the i / o relationship of the smart rotor, the neural control methods with both off - line and on - line modeling in frequency domain on the smart rotor and their realization procedures are presented

    行中直的槳轂交變載荷以周期性的為,而智能旋翼的輸入輸出關系具有非線性特徵。據此,本文提出離線建模的和在線建模的智能旋翼頻域神經控制方法,並給出實現的具體方案細節。
  13. With the helicopter upright flying sideways straight and level from left to right, as the helicopter passes in front of the pilot, apply collective and right cyclic to complete an outside loop

    保持尾朝向操控者,由左向右開始橫向水平行,當直通過操控者的前方時,加大旋翼的螺距並且將副翼打右舵完成一個外浸斗。
  14. With the helicopter upright flying sideways tail - in straight and level from left to right, as the helicopter passes in front of the pilot, apply collective and left cyclic to complete an inside loop

    保持尾朝向操控者,由左向右開始橫向水平行,當直通過操控者的前方時,加大旋翼的螺距並且將副翼打左舵完成一個內浸斗。
  15. 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

    保持尾朝向操控者,由右向左開始橫向水平行,將降舵打降舵,控制旋翼的螺距,使體能保持固定的高度及橫向速度,至少完成一個前滾翻。
  16. It is one of the hottest international research topics for the small unmanned helicopter to be controlled, whose flight mode currently is limited mainly by remote controlled, while the research of automated flight control is on the rise

    對小型無人直行控制目前是國際上的一個研究熱點。無人直的控制方式要局限於遙控行,對自行控制的研究則方興未艾。
  17. The flight control system of attack helicopter and the influence of disturbance during noe flight are studied in this dissertation. and the use of h robust control and dynamic inversion schemes in flight control system are discussed

    本文要對貼地行時武裝直行控制系統進行深入的研究和探索,討論了貼地行時氣流擾動對直系統的影響,研究了h _魯棒控制和動態逆控制在直控系統中的應用。
  18. Then the development pattern of foreign successful aviation industry is referenced. i t is put forward that yan liang should adopt the industry clustering strategy to improve its dominant industry, including corresponding principles and emphases, and meanwhile yan liang should adopt the industry expanding strategy to the boost its urban comprehensive development

    同時在參考了國外成功產業的發展模式之後,指出了閻良應採取產業集群發展模式提產業的戰略,並提出了相應的戰略目標、原則和重點,繼而指出了閻良同時應採取導產業帶動城市全面發展的戰略。
  19. This orientation allows the fuel tank to be closer to the main shaft reference line ? providing a consistently balanced helicopter throughout the entire flight

    這種傾向使油箱為接近軸參考線提供了一種持續的平衡直在整個行過程
  20. As the terrain falls away moderately sharply at the end of the 50 metre run, the helicopter became airborne again and travelled a horizontal distance of approximately 100 metres whilst falling through a vertical height of some 100 feet before impacting with terrain for a second time in a nose high attitude at an elevation of 1150 feet amsl. the main body of the wreckage finally came to rest after travelling forward for a further 30 metres

    在直沖前接近50公尺處,山勢頗為陡峭向下,直因而再度離地,在半空中沖前約100公尺,而下墜的垂直高度為100尺左右,然後在高出平均海平面1 , 150尺以仰角撞向另一山坡,繼而再沖前30公尺后停下,現場遺留體殘駭。行員和空勤員喪生。
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