飛機出故障了 的英文怎麼說

中文拼音 [fēijīchūgùzhànglē]
飛機出故障了 英文
something has gone wrong with the plane
  • 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...
  • 機 : machineengine
  • 故 : Ⅰ名詞1 （事故） event; incident; happening; accident 2 （原因） cause; reason 3 （朋友; 友情） fr...
  • 障 : Ⅰ動詞（阻隔; 遮擋） block; hinder; obstruct Ⅱ名詞（遮擋物） barrier; block; obstacle
  • 了 : 了助詞1. （用在動詞或形容詞后, 表示動作或變化已經完成） 2. （用在句子的末尾或句中停頓處, 表示變化, 表示出現新的情況, 表示催促或勸止）
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 故障 : hitch; breakdown; stoppage; fault; faulting; accident; blunder; bug; conk; failure; impairment; i...
  1. In this system, we use a computer model to simulate the true aeromodelling ' s wing, and then we simulate the state of aeromodelling ' s wing under the real flying conditions by computer. moreover, we simulate two fault - models for wing ' s model, and then we get the state ' s date of wing ' s model structure when the two faults are happening

    在建立這個健康監控系統中我們採用在計算機上建立的模型來模擬航模飛機的機翼並在計算機上模擬了飛機在真實情況下的飛行受力狀態，接著我們在計算機上針對機翼模型模擬了二個故障，並計算出了在這二個故障發生時機翼結構的受力狀況。
  2. The features of aircraft flight line maintenance expert system were analyzed in this dissertation. decision fault tree ( dft ) based binary decision diagram ( bdd ) was presented, which applied in the expert system in combination with case based reasoning ( cbr )

    本文分析了飛機航線維護排故專家系統的特點，提出了基於二元決策圖的判定故障樹方法，並將該方法和基於事例推理的方法應用於專家系統的開發，給出了這兩種方法的集成診斷模型。
  3. One of the plane 's engines gave out in mid-atlantic.

    飛機在大西洋中部飛行時，其中一個發動機出了故障。
  4. His neighbor always let his chickens loose, and they ran over to reach the garden to dig out the roots and eat the flowers and make a mess everywhere. and he told his neighbor to keep the hens within his fence. but the neighbor said, " i don t believe in this kind of restriction, imprisonment

    有一架飛機發生故障，飛行員就用無線電向機場塔臺求救：呼叫塔臺，呼叫塔臺，緊急求救，緊急求救，我離陸地有300英里，離水面有600英尺，飛機快沒油了，引擎著火，儀錶板也出問題了，副駕駛又心臟病發，請趕快指示我該怎麼辦？
  5. Using artificial neural network, a new approach to process flight dynamic datum is presented, and a fault aircraft flight simulation system is established

    並提出了一種利用神經網路來處理氣動力模型數據的方法，建立了故障飛機模擬系統。
  6. Based on research of theory and methods, this thesis presents design scheme of the dynamic fault tree analysis platform dfta and implement the platform ; practices a dynamic fault tree analysis example of boeing 707 plane engine oil indication system and alarm system on the platform and gets top event occurrence rate 、 minimal cut sequence 、 probability importance sequence 、 structure importance sequence and critical importance sequence and presents system improvement suggestion based on the analysis results

    在理論方法研究的基礎上，本文提出了動態故障樹分析平臺dfta的設計方案，並進行了實現;利用該軟體對波音707飛機發動機滑油壓力指示和警告系統進行了動態故障樹實例分析，得到了頂事件發生概率、最小順序割集、概率重要度排序、結構重要度排序、關鍵重要度排序等分析結果，並根據上述分析結果提出了系統設計改進建議。
  7. We had to cut this flight short because our chase aircraft had a mechanical problem

    由於伴隨飛行的飛機出現了機械故障，我們不得不提前結束了這次試飛。
  8. And matrix equations calculating the responses of coupled vibrations are deduced. a set of software analyzing coupled vibrations is developed. the responses of flexural vibration, torsional vibration and torsional torque are analyzed under some fault cases, including mass escaping of low - pressure and generator rotors

    利用該軟體，分析了低壓缸和發電機轉子發生質量飛脫事故，發電機出口端發生三相、兩相短路故障，發電機非同期並網故障以及電網三相短路重合閘故障時，機組軸系的彎振、扭振及扭矩響應情況。
  9. It mainly discusses the repairing action of direct self - repairing law brought forward in paper [ 33 ] for multiple failures occurring at the same time or in sequence. the problem of parameter selection in direct self - repairing law is also discussed. then, the author do some theory analysis of the linearization problem of aircraft model equation and the modeling problem of buoy failure

    本文在文的研究基礎上，對直接自修復理論進行了豐富和發展：主要研究了文提出的直接自修復律在多個故障同時發生或相繼發生時的修復作用；研究了直接自修復律的參數選取問題；同時，對飛機模型方程的線性化、浮鬆故障的建模問題作了一些理論分析。
  10. Abstract : the control reconfigurable aircraft with multi - surfaces needs robust basic flight control system to support enough time for failure detection and isolation. when partial surface loses, it can keep the damaged aircraft stable. in this paper, multivariable output feedback digital control laws are designed for the control reconfigurable aircraft ( cra ). the method uses fast - sampling digital pi controllers to design digital flight control tracking system. this paper gives the way to design the controller and analyze its robustness characteristics. the simulation results indicate that the controller is very robust and the output responses are fully satisfactory

    文摘:控制可重構飛機要求其基本飛行控制系統對舵面部分缺損故障具有強的魯棒特性，在故障發生后保證飛機的穩定性，提供足夠的時間進行故障的檢測和隔離，為控制系統重構提供條件.本文採用高速采樣pi控制器設計輸出反饋跟隨系統，給出了控制器的設計方法，並分析了它對于控制舵面部分缺損故障的魯棒特性.模擬結果表明，這種控制器具有好的魯棒特性
  11. He flies off with her, an apparent kidnaping, but is forced down in the desert

    禍不單行的是飛機發生故障而在沙漠上迫降，兩個冤家對頭鬧出的笑話就更大了。
  12. In this thesis, on the basis of federated kalman filtering theory and aiming at a certain type of airplane equipped with many navigation equipments such as sins, gps, etc., an integrated navigation system with the fault tolerance property is designed. the thesis is stressed to investigate some new theories and methods of fdi in designing the fault tolerance integrated navigation system

    本論文以carlson提出的聯邦濾波方法作為理論基礎，針對某型飛機裝備的sins 、 gps等多種導航設備設計了具有容錯性能的聯邦濾波組合導航系統，並且在以往三屆研究生論文的研究工作基礎上，著重研究了組合導航設計中有關故障檢測方面的新理論和新方法。
  13. The content includes the study on the fatigue performance of the plexiglas, the compiling of the load spectrum of the canopy, the study on the evaluation of the fatigue life of the canopy glass, the study on the allowable limit of the scratch on the canopy glass and the study on the analysis method of the dynamic response of the bird impact on the aircraft windshield

    所涉及的內容包括:有機玻璃疲勞性能研究、活動艙蓋載荷譜編制、座艙玻璃疲勞壽命估算方法研究、座艙玻璃劃傷故障容限研究、飛機風擋鳥撞動響應分析方法研究等。根據活動艙蓋載荷特性，提出用壓力傳感器測量活動艙蓋載荷的方法，並首次實現了活動艙蓋載荷譜飛行測量。
  14. Based on the analysis of lateral - directional control system of a certain plane, representative fault infecting flying security is specialized ; flying security is evaluated ; it is found that flying security probability can not be content with the flying safety standard

    摘要在對某型飛機橫向操縱系統分析基礎上，列舉出危害飛行安全的典型故障；針對該典型故障，進行了飛行安全評估；計算發現，飛行安全風險概率達不到安全標準。
分享友人
分享到 Line

分享到臉書