airplane configuration 中文意思是什麼

airplane configuration 解釋
飛機布局型式
  • airplane : n. 〈美國〉 飛機〈英國說 aeroplane〉。2. vi. 坐飛機。
  • configuration : n. 1. 結構；構造；圓形，外形。2. 組合，布置；配置。3. 地形；【天文學】（行星等的）相對位置，方位；【化學】（分子中原子的）組態，排列；【物理學】位形；組態。
  1. Ask your cfi to take you to an airport where a long runway is available, preferably over 6000 ft. and to start a normal approach in normal configuration, descend to the normal round - out / flare hight, then keep the power or whatever power setting needed, so that you can fly the airplane, using ground effect. keep flying the runway center line for about 500 - 1000 feet

    要求教官帶你去降長跑道（ 6000尺以上） ，降至平飄高度后拉平，不減油門，也許在多給點油，利用地效沿跑道中線平飛500 - 1000尺，在這段時間內快速目測左，前，右，前，體驗此時飛機與跑道面的高度，然後收油門。
  2. Abstract : problems existed in using combined jig to assemble airplane are analyzed and the principle of how to select integral structure configuration of jig for airplane assembly is introduced. correct setting of three supporting points of the integral jig is discussed in the paper as well

    文摘:分析歸納了飛機裝配中採用組合式型架存在的問題；介紹了飛機裝配中型架總體結構形式的選擇原則；討論了整體式型架3個支承點應如何正確設置。
  3. Because of the complicated structure and the long life cycle, the airplane r & d project needs configuration management much more

    航空工業中的型號產品研製由於其結構復雜、研製周期長，尤其需要進行技術狀態管理。
  4. During the procedure, the airspeed continues accelerating ( or decreasing ) and the aircraft configuration is rapidly changing. the aerodynamic interactions are complex and lead to dynamic instabilities. the shift between helicopter and airplane flight modes necessitates a change in control strategy

    過渡模式下，飛機速度不斷增加（或減小） ，氣動布局不斷改變，飛機動力穩定性差且氣動干擾嚴重，直升機控制和固定翼控制切換，因此過渡模式動力學特性和控制系統研究是整個傾轉旋翼飛機研製的主要難點。
  5. Main system parameters " requirements are evaluated and the bistatic sar radar equation is derived. this dissertation also analyzed the range ambiguity caused by ill geometric configuration arrangements for the transmitter and receiver when the airplane platforms fly on the opposite side of the mapping swath, and achieved the requirements to avoid this ambiguity

    論文分析了主要系統參數之間的約束關系，推導了雙基地sar的雷達方程，並給出了收、發平臺位於觀測場景兩側時避免測繪帶內有用回波信號本身產生混疊的條件，為今後進行系統的分析與設計提供了重要的理論依據。
  6. The fuel filling control project for a system of ground pressure fuel filling in a certain airplane was introduced ; the configuration, control principium and methods of realization for the control system of ground pressure fuel filling in a certain airplane were expatiate detailedly ; at last, the prominent economic value and important meaning for military fairs were narrated after some examination

    摘要介紹某型飛機地面壓力加油系統加油控制方案；詳細說明飛機地面壓力加油控制系統的組成和加油控制原理及實現方法，通過試驗證明，該系統的加裝有著顯著的經濟價值和重要的戰略意義。
  7. Along with the development of science and technology, the modern airplane systems are becoming more and more complex. for ensuring the product quality, it ' s necessary to carrying out configuration management in the development process

    隨著科學技術的發展，現代飛機的技戰術指標和復雜程度迅速提高，為保證飛機研製過程的有序進行，確保產品質量，必須對飛機技術狀態進行科學管理。
  8. At first, configuration method of stabilization of los and survey of development of aoep in the world are summarized in this paper, and then principal of how movement of airplane can be isolated by a two - axis - platform is analyzed theoretically. requirements of stabilization of los to servo system are put forward. it provides the basis of theory for designing servo system

    本文首先概述了國內外光電平臺的結構和視軸穩定方法以及光電平臺的發展概況，介紹了常用的穩定與跟蹤控制方法；進而從理論上分析了兩軸光電穩定平臺隔離載體角運動的原理，總結並提出了視軸穩定對伺服系統的性能要求，從而為伺服系統的設計提供了理論依據。
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