飛機攔阻 的英文怎麼說

中文拼音 [fēijīlánzǔ]
飛機攔阻 英文
aircraft arrestment
  • 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
  • 攔 : 動詞（不讓通過; 阻擋） bar; block; hinder; obstruct; hold back
  • 阻 : 動詞（阻擋; 阻礙） block; hinder; impede; obstruct
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 攔阻 : block; hold back; hinder; obstruct; barrage; interdiction
  1. On the basis of the research on the arresting behavior of the carrier aircraft, the arresting model of the continental rise aircraft as well as its motion analysis is presented in the paper

    本文對飛機著陸攔阻的技術進行了較深入的研究，主要是針對陸基飛機，借鑒艦載飛機的攔阻特性進行了攔阻鉤的建模及其運動學分析。
  2. The flight deck measures 333 x 77m and is equipped with four lifts, four steam - driven catapults and four arrester wires

    飛行甲板有333米長， 77米寬，裝備有4部升降機4具蒸汽彈射器和4條降落攔阻索。
  3. None of the other p1 - lots present would have thought of going up, but hamel one of the finest of all pilots of the beriot monoplane was not to be stopped

    其他在場的飛行員都沒有想到要起飛，但是哈梅爾? ?這個布雷里奧式單翼飛機最優秀的駕駛員之? ? ?是不會被阻攔的。
  4. The company has been working with the usn to identify areas where ship complementing can be reduced, with the new nuclear propulsion plant and the new aircraft launch and recovery systems offering the main opportunities

    這種發動機將在阻攔的動態過程中有效降低阻攔索拉力的峰值，並對著艦鉤掛上阻攔索的整個過程以及飛行最終停止的位置進行準確的控制。
  5. Electro - hydraulic proportional control and nonlinear control methods for aircraft arresting system are discussed theoretically

    對飛機攔阻系統的電液比例控制及非線性控制方法進行了理論研究。
  6. Research results are used in the manufacturing of our new type aircraft arresting system, so the dissertation has significant value of practical application

    研究成果已應用於我國新型飛機攔阻系統的研製中，因此論文有重要的實際應用價值。
  7. The dissertation summarizes the application, development and study status quo of aircraft arresting system. the significance and background of the study are presented

    對飛機攔阻系統的應用、發展及研究現狀進行了綜述，明確了論文的研究意義及背景。
  8. The policy about stopping aircraft once they had landed was erratic, to say the least.

    飛機降落時的攔阻辦法，至少可以說變化很大。
  9. The performance of the system designed will directly affect the overloading that an aircraft can bear, the safe overrunning length of runway as well as the changes of tensile force of belt and braking pressure of oil, and ultimately has influence on the arresting effects. so in the process of developing a system, we should study the system in order to define the optimal configuration parameters or more effective control methods

    攔阻系統設計的優劣會直接影響到飛機承受的過載、安全攔停距離及帶拉力、剎車壓力的變化狀況，最終影響攔阻效果，因此在研製系統過程中，要對系統進行分析研究，以確定最佳的結構參數和更有效的控制方法。
  10. Aircraft arresting gear is one kind of important safeguard equipment for airports. it is used to arrest an aircraft going beyond the range of a runway at normal landing or by accident to guarantee safety of the pilot and aircraft

    飛機著陸攔阻裝置是機場重要的常務保障設施，用來對正常降落和因意外原因沖出跑道的飛機實施安全攔阻，以保障人機安全。
  11. The dissertation also does a research on the control strategies of mechanical control parts. the theoretical expression among needle valve throttle area, cam - control valve throttle area and the equivalent throttle area of combining control is given, and the principle of combining control of the two valves is analyzed. the arresting control strategies under various engaging conditions are presented, namely the engaging condition of same overrunning length and same engaging speed but different weight, the engaging condition of same overrunning length and same weight but different speed as well as the engaging condition of same weight and same engaging speed but different overrunning length

    研究了機械控制機構的控制策略：從理論上推導出了針閥節流面積、凸輪控制閥節流面積及聯合控制的當量節流面積三者之間的關系表達式；分析了針閥與凸輪閥聯合控制的控制原理和方法；給出了同攔停距離同撞網速度不同重量飛機撞網狀況、同攔停距離相同重量不同撞網速度飛機撞網狀況以及同重量飛機同撞網速度不同攔停距離撞網狀況的攔阻控制策略。
  12. Aircraft arresting system is a kind of important safeguard equipment for airports. it is used to arrest an aircraft going beyond the end of a runway at normal landing or by accident to provide safety for pilot and aircraft

    飛機攔阻系統是機場重要常務保障設施，用來對正常降落和因意外原因沖出跑道的飛機實施安全阻攔，以保障人機安全。
  13. The mathematical model of new type aircraft arresting system is established in detail, and the unique solution of differential equation and the stability and the motion and control characteristics of the system are proved and analyzed

    詳細建立了新型飛機攔阻系統的數學模型，並對微分方程解的唯一性、系統的穩定性及運動特性、控制特性進行了證明、分析。
  14. The electro - hydraulic proportional control law is given. the laws of tracking control of displacement and speed of aircraft as well as tracking control of angle and angular speed of belt wheel are designed by means of state feedback linearization and quadratic performance index linear optimal control method. the robustness of the designed systems is analyzed, and arresting processes are simulated

    給出了電液比例控制規律；利用狀態反饋線性化及二次型性能指標線性最優控制方法分別設計了系統跟蹤控制飛機位移與速度以及跟蹤控制帶輪轉角與角速度的非線性控制規律；對所設計的攔阻系統進行了魯棒性分析及攔阻過程模擬，模擬結果表明，通過選取適當比例系數或控制權系數，兩種控制系統的控制效果及魯棒特性均優于新型飛機攔阻系統。
  15. As to the multiple - index restricted problem that overloading of aircraft, tensile force of belt, overrunning length and braking pressure cannot exceed the bounds of indexes, the dissertation analyzes it in detail

    針對攔阻系統攔阻過程中飛機過載、帶拉力、攔停距離、剎車壓力不能超過指標要求這一多指標限定問題，論文給予了詳細分析。
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