飛機設計布局 的英文怎麼說

中文拼音 [fēijīshèjìbùjú]
飛機設計布局 英文
aircraft layout
  • 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
  • 設 : Ⅰ動詞1 （設立; 布置） set up; establish; found 2 （籌劃） work out : 設計陷害 plot a frame up; fr...
  • 計 : Ⅰ動詞1 （計算） count; compute; calculate; number 2 （設想; 打算） plan; plot Ⅱ名詞1 （測量或計算...
  • 局 : Ⅰ名詞1 （棋盤） chessboard2 （下棋或其他比賽一次叫一局） game; set; innings 3 （形勢; 情況; 處境...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 設計 : devise; project; plan; design; excogitation; layout; layout work; styling
  1. Such research can lead to a new flight procedure design methodology, which copes with these problems and makes strong economical senses. under the guidance of aviation safety, efficiency, regularity and economy, this thesis applies the principle of the instrument flight procedure, firstly, to research the current vor / dme instrument flight procedure, namely the vor / dme instrument flight procedure ( vor / dmf. ifp ), its holding procedures, departure routes, arrival routes, and approach procedures, cor the terminal airspace

    本文在安全、效率、正常和經濟的原則下，運用儀表飛行程序設計的思想和原則，首先對在vor / dme導航臺上建立儀表進場航線、等待程序、儀表進近程序和儀表離場航線等機場空域內的飛行程序的設計方法進行了研究，總結出不同位置的vor / dme儀表飛行程序的布局形式、適用情況及其優缺點，並首次提出了以vor / dme為基準的封閉圓弧進近程序；其次，研究了基於vor / dme導航臺的區域導航飛行程序的設計方法；最後，研究了在現有的vor / dme儀表飛行程序上建立區域導航飛行程序的設計方法。
  2. Thus the flight dynamic characteristics and control features in the conversion mode are the key technologies in the whole tilt rotor design

    過渡模式飛機的氣動布局改變主要體現在縱向平面內，所以本文主要研究過渡模式下飛機縱向通道的動力學特性和控制系統設計。
  3. Design of innovative control surfaces of flying wing aircrafts with large ratio aspect

    大展弦比飛翼布局飛機新型操縱面設計
  4. Compared with a delta wing aircraft, the double - delta wing configuration has better aerodynamic performance at high angles of attack. an operational analysis was introduced as a method for evaluating training effectiveness of trainer aircraft. approaches to the engineering estimation of aerodynamic characteristics for aircraft with a double - delta wing configuration were studied, and the procedures for determining aircraft performance indices formulated. taking training effectiveness as the objective function and geometric parameters of the wing platform as design variables, through a numerical multivariate optimization arithmetic, the conceptual design optimization for a certain fighter trainer aircraft with double - delta wing configuration was carried out under the constraints of tactical and technical requirements and interrelated geometry. agreement of a calculation example with engineering practice indicates that the optimal design has higher training effectiveness than the baseline design, and in addition, improves the structural force - bearing conditions

    雙三角翼氣動布局比三角翼飛機具有更好的大攻角空氣動力特性.引入了評估教練機訓練效能的作戰分析法，研究了雙三角機翼布局飛機空氣動力特性的工程計算途徑以及飛機性能指標的確定方法.以訓練效能作為目標函數並選取機翼平面形狀的幾何參數為設計變量，採用多變量數值尋優方法，在戰術技術指標及相關幾何約束條件下，對某高級教練機的雙三角機翼氣動布局方案進行了優化選擇.算例表明最優方案不僅比原準方案具有更高的訓練效能，還改善了結構的受力情況，與工程實踐吻合
  5. Finally, the aerodynamic shape optimization design examples for three kinds of reentry vehicles are implemented, which involve a reentry vehicle with cruciform flaps, a variable - bend reentry vehicle and a crew transfer vehicle

    本文的最後，應用智能優化設計系統對帶控制舵機動式再入飛行器、可變彎體再入飛行器以及一種載人返回艙氣動布局這三類工程問題來進行優化設計。
  6. With c + + language, iods is composed of traditional optimization methods, knowledge base, inference machine, knowledge acquisition and graphic user interface ( gui ) in windows 2000. this integrated synthesis system performs the intelligentized optimization design for asrv, including the following items : production deduction strategy, knowledge handling technology, traditional optimization methods, evolutionary algorithms and the object - oriented strategy

    此系統利用c + +語言在windows2000環境下編制而成，由優化演算法庫、知識庫、推理機制、知識錄入和圖形用戶界面等幾部分構成；該系統將產生式推理技術、知識處理技術、基於數學規劃的優化演算法、現代優化演算法以及面向對象程序設計方法綜合成一個有機的整體，形成了一個針對再入飛行器氣動布局優化設計的智能優化設計平臺。
  7. In the thesis, the advanced cad ( computer aided design ) technology was combined with the intersecting knowledge including man - machine engineering, artificial intelligence method, database system, etc. on the base of ibm / catia, the corresponding modules, such as the database of knowledge and rule, the intelligentized suggestion, the various part assembly, the accessibility checkout, have been exploited. and a method of layout design which based on knowledge has been provided

    本文利用先進的計算機輔助設計（ computeraideddesign ）技術，結合人機工程學、人工智慧方法、數據庫知識等邊緣交叉學科知識，在ibm catia平臺上，實現了相應知識與準則的創建與實現、智能化裝配提示、各組件裝配、可達性檢查等功能，初步給出了基於知識與準則的飛機駕駛艙布局設計方法。
  8. That demands a ship design which is sufficiently adaptable ? in terms of deck estate, aviation facilities, power generation and mission systems architecture ? to accept and operate future aircraft that may be substantially different from those they first take to sea

    這就要求航母的設計可以充分進行修改? ?比如甲板布局，飛行設施，發電設備和任務系統體系結構? ?以便接受和使用未來的飛機，它們可能與航母剛製造好時搭載的飛機完全不同。
  9. During the aircraft cockpit layout design, the database of knowledge and rule is reasonable and efficient, and reaches a request of the real - time assembly, and provides the methods by which the designer estimates an aircraft cockpit layout design, and enhances the design efficiency and precision, and improves the level of the aircraft cockpit layout design

    在飛機駕駛艙布局設計的實際應用中，表明了知識與準則數據庫高效、合理，達到了實時裝配要求，提供了飛機駕駛艙布局設計的評估手段，保證了設計效率和精度，提高了飛機駕駛艙布局設計水平。
  10. The layout design of aircraft cockpit, which acts as the man - machine interactive interface, has great research value

    飛機駕駛艙布局設計作為人機交互的關鍵，具有很重要的研究價值。
  11. The fast development of computer science and electron technology make the appearance of virtual aircraft instrument system that highly integrates the digital information from airborne devices possible and the cockpit layout could be easily changed while the pilot can get flight information more quickly and control the aircraft more efficiently

    計算機技術以及相應電子技術的高速發展，以及高度集成機載電子設備信息的多功能虛擬儀表系統出現，改變了以往飛機座艙中儀器儀表紛繁復雜的布局，使得飛行員能快速獲得飛行信息，從而更加有效地操縱和管理整個飛行系統。
  12. The progress of aero - technology improves the level of aircraft cockpit layout design

    航空科技的進步為飛機駕駛艙布局設計水平的提高創造了條件。
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