氣動裝彈 的英文怎麼說

中文拼音 [qìdòngzhuāngdàn]
氣動裝彈 英文
gas loading
  • 氣 : Ⅰ名詞1 （氣體） gas 2 （空氣） air 3 （氣息） breath 4 （自然界冷熱陰晴等現象） weather 5 （氣味...
  • 裝 : Ⅰ名詞1 （服裝） dress; outfit; attire; clothing 2 （演員的化裝品） stage makeup and costume Ⅱ動詞...
  • 彈 : 彈名詞1. （彈子; 小球形的東西） ball; pellet 2. （內裝爆炸物, 具有破壞和殺傷能力的東西） bullet; bomb
  1. Therefore, a new design of the flexible joint is herein assumed by replacing the spring / damper system by a hydropneumatic system in which a horizontal hydraulic cylinder only is needed to be fitted between the two bell cranks and the rest of the hydro - pneumatic system which are the throttle valve and the accumulator can be suspended on the vehicle frame at any convenient place

    因而，此處採用新型撓性連接設計，用液壓氣動系統替代彈簧減振器裝置，液壓氣動系統兩曲柄間只需安裝一個臥式液壓缸，而其他部件（即減壓閥和蓄能器）可懸置於車架的適當位置。
  2. 5 ) the 3 - d geometry and finite element model of the assembly of the optimized obturator of the breech mechanism is set up in terms of the optimized structural parameters. quasi - static and dynamic finite element analysis of stiffness, strength and obturating performance of the optimized obturator of the breech me chanism is performed

    利用優化后的結構參數建立了優化后炮閂閉氣結構的裝配體三維幾何實體模型和有限元模型，對優化后的炮閂閉氣結構剛強度和閉氣性能進行了準靜態及動態多體接觸彈塑性有限元分析。
  3. In this thesis, based on pershing ii surface to surface missile, a new kind of ballistic missile was designed with an additional rocket engine, which can be ignited twice. firstly, aerodynamic computational models of missile body and warhead which reentry with supersonic are built according to the task requirements ; secondly, the propulsion system model of missile is built whose first two stages are solid rocket engines and the third stage is liquid - solid combined rocket engine. the nozzle and the shape of the engine are designed to meet the needs of the populsion project ; thirdly, the trajectory model of the mass point is built and a wavy trajectory is designed & optimized ; finally, the ability of a missile ' s breaking through defence is analyzed

    以美國潘興導彈為原型，增加可兩次點火的末級發動機，改裝成具有跳躍能力的地地彈道導彈；首先，根據任務需求，建立了導彈的氣動模型，並建立了彈頭再入時高超聲速氣動模型；其次，建立了導彈推進系統模型，前兩級採用了固體火箭發動機，第三級採用了固?液組合火箭發動機，並在總體方案要求下，對發動機噴管和外形進行了設計；第三部分，建立了導彈質點彈道模型，設計了一條跳躍式彈道，並對跳躍式彈道進行了優化設計；最後，對導彈進行了突防能力分析，從分析的結果可以看出，跳躍式彈道的突防能力比常規的拋物線彈道要強。
  4. Perry's slingshot device consisted of a fast moving hollow piston or capsule which contained the test section gas.

    培里的彈射裝置由一個快速運動的中空活塞或密封容器組成，其中包含試驗用的氣體。
  5. Electro - hydraulic servo loading system ( ehsls ) is used to simulate the aerodynamic torque acting on the rudder of missiles, and it is one of the main simulation equipments in hardware - in - loop flight simulation laboratory

    電液伺服加載系統是導彈武器系統半實物模擬中模擬作用在導彈舵面上氣動載荷的加載裝置，它是導彈在實驗室內進行半實物模擬的主要設備之一，是飛行器大迴路模擬中的重要組成部分。
  6. Electric strikes and frame mounted actuators

    裝有撞針和彈體的電氣致動器
  7. Abstract : this paper introduces briefly the control principle of trajactory correction technique and analyzes the structures and application areas of several typical trajectory correction mechanisms such as paddle type ring and d - ring etc. moreover, it makes the aerodynamics simulation and dynamics simulation of trajectory correction mechanism as paddle type damping ring. the simulation result proves the correctness and feasibility of the design

    文摘:簡要介紹了彈道修正技術的控制原理；分析了槳式、 d型環等幾種典型彈道修正裝置的結構特點和應用范圍；並對其中的槳式阻尼環彈道修正裝置分別進行了空氣動力學模擬和運動學模擬，驗證了設計的可行性和正確性。
  8. 3 ) a 3 - d geometry and finite element model of the assembly of the obturator of the breech mechanism is established. quasi - static and dynamic finite element analysis of stiffness, strength and obturating performance of the obturator of the breech mechanism is carried out, based on elastoplastic theory and multi - body contact algorithm, and the simulation results coincide with experimental results, further, th e effect of friction factor on its obturating performance is investigated

    建立了炮閂閉氣結構的三維裝配體幾何實體模型和有限元模型，對炮閂閉氣結構剛強度和閉氣性能進行了準靜態及動態多體接觸彈塑性有限元分析，分析結果與試驗結果相吻合，進一步研究了摩擦系數對其閉氣性能的影響。
  9. It solved successfully long - term existent issues in pneumatic speed limiters of high idle speed, large power loss, and swinging of speed at home by means of designing the brand - new - in - structure valve - located device ? am - spring mechanism

    由於設計了結構新穎的閥門定位裝置? ?凸輪-彈簧機構，解決了國內現有氣動式限速器長期存在的空載轉速高，功率損失大，游車等問題。
  10. The design undertaken mainly from the following aspects : 1, mechanism ddesign : included the base and the joints : 2, trasmission mechanism design : adopted a synchronous toothelike transmission bell ; 3, balance system design : adopted springs and a brake and a lay air cylinder ; 4, design parameter and verify alculation ; 5, established motion equation by d - h method ; 6, simulated the motion locus by matlab software ; 7 ^ mapping out the part drawing or asesembly drawing

    本設計主要是從以下幾個方面入手： 1 、機構設計：包括底座和臂關節的設計； 2 、傳動機構設計：將驅動電機安裝在底座上，利用同步齒型帶、離合器傳遞手臂的動力；利用齒輪傳動帶動底座回轉； 3 、平衡系統設計：採用了彈簧平衡系統、電磁式制動器和單向延時氣缸； 4 、設計參數和校核計算； 5 、用d ? h法建立運動學方程； 6 、利用matlab軟體對手臂的運動空間進行模擬； 7 、利用autocad2000繪圖：包括零件圖和裝配圖。
  11. The dj - a gynecological examination bed is uses the electrically operated lead screw to make the surface of bed fluctuation the power supply, when use so long as inserts the power source, controls the surface of bed with the foot the fluctuation, the seat back cushion and the cushion adjustment is uses was mad the spring makes the poweruses the electrically operated lead screw is the power supply, surface of bed fluctuation, the seat back cushion and ( manually controlled ) sits the board the angle adjustment the switch to control by the foot control, easy to operateif must cause to inspect the bed to move the position, blooms a base four feet turn of slightly tight pine, transfers to needs the position afternoon tight foot turn then the foot pad is the add - on component, may conveniently install according to the surgery need or dismount

    型婦科檢查床是採用電動絲桿作床面升降的動力源，使用時只要插上電源，用腳控制床面的升降，靠背和坐墊的調節是採用氣彈簧作動力.採用電動絲桿為動力源，床面的升降，靠背和坐板的角度調節均由腳控（手控）開關控制，使用方便.如果要使檢查床移動位置，將底部四個腳輪的稍緊松開，移到所需位置后稍緊腳輪即可.腳墊是附加裝置，根據手術的需要可方便地裝上或卸下。
  12. Elimination of bracket or connection adopter for directly fitting offers easy and correct installation. please contact us for installation of spring return pneumatic actuators

    直接安裝可避免不必要的連接支架或連接套件，便於現場安裝及減少安裝偏心誤差。安裝彈簧復位式（單作用）氣動執行器請及時和我們聯系。
  13. As the seat rode to the top of the rails, a port opened and gas ignited the rocket, blasting stricklin fully out of the cockpit like a roman candle

    彈射座椅滑行到導軌頂端時，出口被打通，氣體點燃，發動火箭推力裝置，象發射一座羅馬燭臺一樣把斯特里克林完全「炸」出駕駛艙。
  14. This work is useful to the design and analysis of the new ejection mechanism, especially the new cylinder. finally, we gave some clue for further research basing on the summary of this paper

    最後分別分析了不同慣性負載mw 、不同行程s 、不同有效面積ae對作動筒動特性的影響，為設計新的導彈彈射裝置特別是氣壓作動筒提供了理論依據。
  15. The dissertation presents the combined theoretical, numerical and experimental studies on the experimental modeling of the actuator, the design of test rig and control system, the modeling of two - dimensional airfoil aeroelastic system, the control design of active flutter suppression, and the effect of group delay in the digital filter on the stability of aeroelastic closed - loop system

    本文通過理論分析、數值模擬與風洞實驗相結合的方法，研究了超聲電機作動器建模、翼段顫振實驗裝置和控制系統設計、二維翼段氣動彈性系統建模、顫振抑制控制律設計以及數字濾波器群時延對顫振抑制閉環系統穩定性影響等問題。
  16. In this paper, the backward simulation was summarizd at home andabroad, the characteristics of shell nosing were introduced, the theory and scheme of backward simul - ation of shell nosing was constructed, the determined methods of the boundary conditions were put forward in backward simulation for the processes of shell nosing

    論述了推力矢量控制技術是提高空空導彈性能的核心技術，介紹了常用的三類推力矢量裝置，著重討論了燃氣舵式和擾流片式推矢裝置的特點、設計方法、性能及其優缺點.在此基礎上，研究了適用於氣動力/推力矢量復合控制的變結構控制系統及其開關函數的切換條件和飛行控制系統框圖.最後綜述了推力矢量裝置在第四代空空導彈上的應用情況
  17. Use double seal rings ; install hair string and anti - water rubber, and use elastic seal string around the corner of doors and windows, and adopt all dry configurations to achieve excellent seal performance for air, humidity and sound

    雙道環形連續密封結構，滑動部分裝有特殊設計的毛條及防水膠條，門窗四周採用彈性密封條鑲嵌密封，全乾法結構，使窗具有良好的氣密、水密和隔音性能。
  18. This kind so - called aero - optical ( ao ) effect not only has become the bottleneck for development of high - speed interceptor, but also troubles china ' s development of high - speed missile technology and related equipment

    這類氣動光學效應不僅成為高速攔截武器研製的瓶頸，而且困擾著我國導彈技術的發展和裝備研製，這也是世界性的難題。
  19. The primary work of this paper is as follow : three aspects are analyzed in detail as to the characteristics of integral rocket - ramjet, which include : a. the matching for inlet shape and missile configuration ; b. the influence on missile conceptual performance caused by the number and position of inlet ; c

    具體表現在如下幾個方面： （ 1 ）針對整體式沖壓發動機的特點，詳細分析了進氣道型式與導彈總體布局的匹配關系、進氣道數目及其安裝位置對導彈總體性能的影響、沖壓發動機和固體助推器的一體化等彈機一體化設計的問題。
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