阻攔機 的英文怎麼說

中文拼音 [lán]
阻攔機 英文
arresting engine
  • : 動詞(阻擋; 阻礙) block; hinder; impede; obstruct
  • : 動詞(不讓通過; 阻擋) bar; block; hinder; obstruct; hold back
  • : machineengine
  • 阻攔 : stop; prevent; tackle; obstruct; bar the way
  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

    本文對飛著陸的技術進行了較深入的研究,主要是針對陸基飛,借鑒艦載飛特性進行了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4具蒸汽彈射器和4條降落索。
  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最優秀的駕駛員之? ? ?是不會被的。
  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

    這種發動將在的動態過程中有效降低索拉力的峰值,並對著艦鉤掛上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. Design of arresting net recovery system for certain unmanned aerial vehicle

    某型無人網回收系統設計
  6. Electro - hydraulic proportional control and nonlinear control methods for aircraft arresting system are discussed theoretically

    對飛系統的電液比例控制及非線性控制方法進行了理論研究。
  7. 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系統的研製中,因此論文有重要的實際應用價值。
  8. 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。
  9. The policy about stopping aircraft once they had landed was erratic, to say the least.

    降落時的辦法,至少可以說變化很大。
  10. Finally, the research on the dynamics loads as well as the effects of the motion of the wheels to the process of arresting gear engaging is conducted

    研究了索在被輪壓縮后對套能力的影響,分析了索瞬間被套時產生的動載荷。
  11. 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

    系統設計的優劣會直接影響到飛承受的過載、安全停距離及帶拉力、剎車壓力的變化狀況,最終影響效果,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。
  12. In technique rebuilding of system, discharge curve of ni - mh battery was measured, and power supplies in uav were improved. the security, adaptability and efficiency of miniature aerial rs systems could be improved obviously by microwave video transmission system and self - regulating blocking net in landing

    在對系統的技術改造中,測定了ni - mh電池組放電曲線,對無人載電源做了改進,配合加裝的微波視頻傳輸系統和自行研製的降落網可以大大提高無人航空遙感系統的安全性、適應性和作業能力。
  13. 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

    著陸裝置是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實施安全,以保障人安全。
  14. 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

    研究了械控制構的控制策略: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;給出了同停距離同撞網速度不同重量飛撞網狀況、同停距離相同重量不同撞網速度飛撞網狀況以及同重量飛同撞網速度不同停距離撞網狀況的控制策略。
  15. 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

    系統是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實施安全,以保障人安全。
  16. 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。
  17. 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;對所設計的系統進行了魯棒性分析及過程模擬,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系統。
  18. Sysadmins typically block ftp access to the web server and often will deny developers access to the production box

    系統管理員們通常會對web服務器的ftp訪問,也常會拒絕開發者們對產品計算的訪問。
  19. Preliminary treatment covers removal of larger suspended solids and heavier inorganic particulates through mechanical bar screening, gravitational sedimentation and flotation to keep the subsequent unit operations and processes from clogging and abrasion and to maintain the designed functions of the equipment

    前處理系指以截、重力沉澱、浮除等方式,將水中體積較大之懸浮固體、較重的無性固體,或是過量的油脂等污染物先行移除,避免造成后續處理單元設備發生塞、磨損等現象,而影響到械設備的原有功能。
  20. 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

    針對系統過程中飛過載、帶拉力、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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