起飛載荷 的英文怎麼說

中文拼音 [qǐfēizǎihé]
起飛載荷 英文
take-off wing loading
  • 起 : 起Ⅰ動詞1 （站起; 坐起） rise; get up; stand up 2 （取出; 取走） draw out; remove; extract; pull 3...
  • 飛 : 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...
  • 載 : 載Ⅰ名詞（年） year : 一年半載 six to twelve months; six months to a year; 三年五載 three to five ...
  • 荷 : 荷名詞（蓮） lotus
  • 起飛 : （of aircraft） take off; lift-off; launch; hop off
  • 載荷 : load; loading載荷變化 load fluctuation; variation in load; 載荷裝置 load device
  1. The bird strike is similar to adding a high velocity rate loading to the aircraft wndshield, and thus results in the wndshield ' s high stain rate deformation

    飛鳥對于風擋的撞擊，類似於對于風擋施加一高速率的載荷，從而引起風擋材料以很高的應變速率變形。
  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

    飛艇是一種可操縱的浮於空中的飛行器。在飛行中主要依靠內部充滿氦氣的氣囊提供的浮力，將飛艇及其載荷支持在空中，發動機為其提供前進的動力，通過操縱尾翼上的升降舵和方向舵控制飛艇的俯仰和方向運動，飛艇的下降是通過排放氣來實現的。飛艇可以垂直起降空中懸停，不需要有專用設備的起降場。
  3. Electro - hydraulic servo loading system ( ehsls ) is an important simulation system in hard ware - in - loop flight simulation laboratory, which can simulate aerodynamic loads acting on flight vehicle, such as missiles, planes. its performance of test is important on the design of flight vehicle

    電液伺服負載模擬器是半實物模擬試驗室中模擬飛行器在飛行中舵面所受空氣動力載荷的重要設備，它的試驗能力高低對飛行器設計起著重要作用。
  4. Finally, the author analyzed the results of the dynamic simulation and given a rough conclusion about the distribution of the ground loads of the aircraft researched among its different landing gears

    對模擬結果進行對比分析，定性地給出該飛機在對稱著陸過程中飛機所受地面載荷在各個起落架緩沖支柱上的分佈關系。
  5. The research on the ground load of landing gear with multi - wheels and multi - struts has been conducted for a long time and the research is quite successful at abroad. however, due to the blockage of the developed countries in technical information as well as the number of aircraft with multi - wheels and multi - landing gear keeps growing

    然而，由於外國在該方面的對中國實行技術資料封鎖，加之我國現有的多輪多支柱起落架飛機數量在不斷增加，因此開展多輪多支柱起落架地面載荷研究有較大的實際意義。
  6. It supports the aircraft during parking and endures the loads during ground maneuvers. most of the vertical and horizontal kinetic energy are absorbed and dissipated by landing gear. it plays an extreme important role in preventing the airframe from vibration and excessive impact forces, improving passenger comfortable characteristics and increasing aircraft flight safety

    飛機起落架作為飛機結構的一個重要部件，承受著飛機與地面接觸時產生的靜、動載荷，吸收和消耗飛機在著陸撞擊、跑道滑行等地面運動時所產生的能量，在減緩飛機發生振動，降低飛機地面載荷，提高乘員舒適性，保障飛機飛行安全等方面發揮著極其重要的作用。
  7. During its storage, transportation, maintenance and service, the solid rocket motor ( srm ) may encounter many incidents such as being dropped onto the ground while being hoisted up, crashing when vehicle turns over during transportation, being struck heavily in takeoff or landing accident while being carried by airplane, impacting with launch platform or buildings when there is abnormality during launch of multiple - stage rocket. impact of great intensity takes place in such accidents, which will lead to srm ignition or explosion

    固體火箭發動機在貯存、運輸、維護及使用過程中可能遇到各種意外機械撞擊激勵，例如:吊裝過程中跌落，運輸過程中因交通事故發生翻覆碰撞，機載固體導彈掛飛時因載機發生起降事故導致高速沖撞，多級火箭發射初期因發射異常與發射架或地面建築物發生碰撞等，固體火箭發動機將受到劇烈機械撞擊載荷作用，導致其著火燃燒甚至爆炸。
  8. How to precisely simulate the landing process of an aircraft and effectively absorb aircraft landing kinetic energy to attenuate the impact loads on aircraft is a problem facing the landing gear community

    如何精確模擬飛機著陸過程起落架和機身的動態響應，並據此設計減小飛機著陸過程中的沖擊載荷的方案，一直是飛機起落架設計和分析中的重要課題。
  9. During aircraft take - off and landing phases, the dynamic loads and vibrations caused by landing impact and the unevenness of runway will result in airframe fatigue, discomfort of passenger and the reduction of the pilot ' s ability to control the aircraft

    在飛機起飛和著陸過程中，由著陸沖擊和跑道不平引起的沖擊載荷和振動，會造成飛機機體疲勞損傷、乘客不適及地面駕駛操縱能力的降低。因此，在設計飛機起落架緩沖器時，必須限制起落架傳遞給飛機的沖擊載荷。
  10. The landing impact has been recognized as a significant factor in structural fatigue damage, dynamic stress on the aircraft airframe, and crew and passenger discomfort

    而這種沖擊載荷被認為是造成飛機及其起落架結構發生疲勞與振動破壞、引起乘員不舒適的重要因素。
  11. In come to the develop requirement of avionics system, we have processed pre - research project in small scale intergrated, it will play an important role on aspect of intergrated functions, and promote military plane " s fight power, on the other hand, it decrease work pressure of pilot

    機載顯示控制系統是新一代航空電子系統實現綜合化、數字化和智能化的核心與關鍵，對實現航空電子系統功能的綜合化、提高飛機的作戰能力和減輕飛行員的任務負荷起著重要的作用。
  12. The uprated engine also allows a possible increase in payload / fuel capability or mtow

    經改進的發動機亦有望令載荷燃料容量或者最大起飛重量有所提升。
  13. In order to possess high reliability, stability and long fatigue life during the landing and taxiing of aircraft, the design of aircraft landing gear is very important

    如何使飛機在著陸和滑跑過程中具有較低的疲勞載荷、較好的穩定性、舒適性和較高的可靠性，起落架的設計至關重要。
  14. To win the prize, teams must demonstrate a rocket - propelled vehicle and payload that takes off vertically, climbs to a defined altitude, flies for a pre - determined amount of time, and then land vertically on a target that is a fixed distance from the launch pad

    為了贏得獎金，參賽隊伍必須證明火箭驅動的運輸工具及其載荷必須垂直起飛，爬上一定高度，飛行一定時間，並筆直的降落在離出發場地一定距離的目標上。
  15. During the process of landing, an aircraft is exposed to a short - duration impulsive impact

    在飛機的著陸過程中，起落架和飛機機身都將承受很大的沖擊載荷。
  16. Due to more and more application of unmanned air vehicles ( uav ) in war, theinteroperabilityand currencybetween uav systems become veryimportant. in 2001. 04, thefirstexperimenttocontrolthetake - offandlandingofamericanavy “ predator ” is carriedoutby the tactical control system ( tcs ), which is developed by america navy. in theexperiment, the launch and recovery, flight control and payload control is finished, and thedata can be received directly from “ predator ”. for investigate the framework, informationcriterionandkeycontroltechniqueoftcs, it ’ snecessarytotesttheprototypeoftcs

    隨著無人機在戰爭中越來越多的應用，無人機系統之間的互操作性和通用性變得尤為重要， 2001年4月，美國海軍研製的戰術控制系統對美海軍「捕食者」無人機進行了首次起飛和降落控制試驗，試驗完成了無人機的發射和回收、飛行控制、載荷控制，並可從「捕食者」飛機直接接收數據。
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