飛機干擾機 的英文怎麼說

中文拼音 [fēijīgānrǎojī]
飛機干擾機 英文
aircraft jammer
  • 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
  • 干 : 干Ⅰ名詞1 （事物的主體或 重要部分） trunk; main part 2 （幹部的簡稱） short for cadre Ⅱ動詞1 （做...
  • 擾 : Ⅰ動詞1 （擾亂; 攪擾） harass; trouble 2 （客套話 因受人款待而表示客氣） trespass on sb s hospital...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  1. On the basis of introducing the principle of the tf / ar radar, this paper analyzes the conditions of effectively jamming the tf / ar radar in typical tactical act of hedgehopping, which include the disposition and quantity of electron reconnaissance / jammer, calculates the capability request of equipments in the method of sensor / hand - emplaced jammer, and concludes that it is difficult to jam tf / ar radar at the present time

    摘要在介紹地形跟隨迴避雷達工作原理的基礎上，通過設定典型超低空突防飛機的戰術行動，分析了對雷達實施有效干擾所必須具備的條件，包括偵察干擾機的部署、數量要求等；並計算了在傳感器擺放（投擲）式干擾機模式下對裝備的性能要求，得出了在目前技術條件下，對地形跟隨迴避雷達實施干擾在技術和戰術上都是困難的。
  2. Nowadays with the booming development of microelectronic technique, the functions of the components of machinery, electricity, magnetism, optics, acoustics and thermotics have been improved rapidly. and the micromation of components, the integration of electronic equipments, the worse working environment, the increasing requirement and emi, all of these make the structural design of electronic equipments more and more important

    在微電子學高度發展的今天，促使機、電、磁、光、聲和熱等元器件功能飛速提高，隨著元器件微型化，電子設備趨向集成化，再加上一些日趨惡劣的工作環境，各種使用要求的提高，空間電磁環境的干擾，以及由於裝填密度高，產生的內在干擾等，使得電子設備的結構設計變得越來越重要。
  3. The rotor / wing aerodynamic interactions of the tilt rotor vehicle in hover is described in this dissertation

    本文主要研究的是傾轉旋翼飛行器懸停狀態時，旋翼機翼之間的氣動干擾問題。
  4. When the tilt rotor vehicle is in hover, the aerodynamic download of the rotor flowfield imposes on the wing. in this time, the rotor / wing interaction is severe

    傾轉旋翼飛行器懸停時，旋翼的下洗流剛好作用在機翼上，此時，旋翼機翼間的氣動干擾非常劇烈。
  5. Many mncs have even their own airboat advertising system ; some other companies would like to make advertise by hiring ; airboat advertise featuring good promotion effect, sound attractiveness, large area, vivified image, especailly when appearing in the endless sky, it can remind so much people feeling the interest ; the best result but the lowest cost make it more suitalbe for every enterprise ; it can used on many cases like ceremony, celebration, memory activity, amusment, lottery drawing and sports games, it is truly the best choice for a company to make a impressed product promotion

    空中飛艇廣告具有宣傳性好，吸引度高，刺激力強，受眾面廣，渲染氣氛，視覺鮮明的特點，尤為重要的是在毫無視覺干擾的一望無際的天空中，它的突出性極度地增強了人們的好奇心與注意力，正是由於此種獨特的廣告傳播方式產生的明顯的廣告視覺效果，高強度的廣告效果更體現了較其他廣告形式的低成本價格，因此，擅於掌握商機的企業可將此種廣告方式作為重要選擇。
  6. Thus, we can construct high performance airplane optic fiber control system on the basis of it. the existing avionic system has already set higher standard of the exchanging capability the data information

    As1773總線具有可靠性高、抗電磁干擾能力強、重量輕、組網方式靈活等優點，可在它基礎上組成高性能的飛機光傳操縱系統。
  7. This dissertation presents how to use the ultrasonic motor as an actuator to suppress the flutter of a two - dimensional airfoil section with a control surface. the ultrasonic motor, which features simple structure, high torque at low speed, small size, low weight and no electromagnetic contamination, is a promising actuator for the flutter suppression of small aircraft

    超聲電機以其結構簡單緊湊、轉矩/質量比大、低速大扭矩、直接驅動，動態響應快、斷電自鎖和不產生磁場且不受外界磁場干擾等優點，有望成為一種非常有前途的作動器，用於小型飛機的機翼顫振主動抑制。
  8. Then, the connected flying, stage separation, signal being sheltered process is simulated in computer, the influences imposed by working conditions and interfering factors for separation process are analyzed. furthermore, if the missile is controlled non - rolling, the stage separation process is simulated in another model. some of conclusions derived from above analysis are checked in theory

    本文就某些可選分離方案進行了對比分析，對地空導彈一體飛行、級間分離、信號遮擋過程進行了計算機模擬，分析了影響條件和干擾因素對分離過程帶來的影響，進一步研究導彈若受控無滾時的級間分離過程，並從理論基礎出發驗證上述研究的部分結論。
  9. Furthermore, because rotors are mounted on the tips of the wing, the rotor / pylon / wing aerodynamic interactions are also included in the model. such factors reflect the unsteady and nonlinear characteristics in the model

    此外，傾轉旋翼飛機的旋翼安裝在翼尖，旋翼/發動機短艙/機翼之間的氣動干擾是建模的一個難點。
  10. Screening of hold baggage is one of the important security control measures in ensuring that no restricted articles that are used for unlawful interference are carried on board, " mr lam said

    檢查寄艙行李，是確保沒有乘客攜帶違禁物品上飛機作非法干擾的一項重要保安控制措施。
  11. By adopting the full state feedback approach and using the modeling aerodynamic interference as feedback nonlinearities, a new autopilot for uav close formation flight is designed

    採用全狀態量反饋，同時將氣動干擾作為非線性反饋，設計出一套適用於無人機近距離編隊飛行的自動駕駛儀。
  12. " the amendment ordinance introduces seven new offences relating to unruly or disruptive behaviour committed on board civil aircraft, including offences relating to obstruction of crew members in performing their duties ; failure to comply with instructions given by crew members ; disorderly behaviour ; tampering or interfering with aircraft component, apparatus, equipment or systems ; intoxication by alcohol, drug or other intoxicating substances ; smoking and the operation of electronic devices in the aircraft when it is prohibited, " a spokesman for the civil aviation department said

    民航處發言人說： 《修訂條例》就在民航飛機上的難受管束或擾亂秩序行為訂定七項新的罪行，包括妨礙機組成員履行其職責；不遵從機組成員發出的指令；擾亂秩序行為；干預或干擾飛機組件、儀器、設備或系統；因酒精、藥物或其他減低清醒程度的物質而致神智不清；在禁止吸煙的情況下吸煙或在禁止操作電子器材時操作該等器材。
  13. In consideration of the special mission characteristics and technical requirement of high altitude long endurance unmanned aerial vehicle, an authentic real - time and space - time windfield integrated model is accomplished to take atmosphere environment influences into account. at the same time, we should analyze the dynamics the uav encounters dispersedly, so the " finite scale " aircraft concept is quoted

    根據長航時無人機的特殊飛行任務特點和技術要求，在飛行試驗階段，有必要綜合考慮飛行環境中各種大氣干擾因素的影響，為無人機設計與模擬提供一個真實、適時的風場時空分佈模型。
  14. Through it the author made a deep study of the satellite attitude control subsystem, verified several sorts of disturbance torques and realized satellite three - axis attitude stabilization control and attitude maneuver under different conditions

    本文在simulink下對衛星姿控系統作了比較深入的研究，對各種干擾力矩進行了驗證，同時在不同的模擬條件下實現了衛星三軸穩定控制、姿態機動和飛輪的磁卸載。
  15. Aeroengine is the most important part of plane, it ' s structure is most complex, it require the highest precision and reliability, at the same time, the requirement on performance is strictest because of the worst work condition, engine condition monitor is the important measure to examine the engine performance, through the measure, we can do the performance adjustment and failure analyses to engine to improve quality of engine

    航空發動機是飛機的重要組成部分，其結構復雜，精度和可靠性要求很高，同時其工作環境極其惡劣，容易受到各種干擾，因此對其性能要求非常嚴格。狀態監測是發動機性能的重要檢測手段，通過狀態監測和試車工作可以對發動機進行性能調整、磨合運轉和故障分析，最終達到提高發動機質量的目的。
  16. Based on the mechanism of slipstream interaction, described in this thesis is firstly the interaction of the propeller slipstream with the wing 、 fuselage and horizontal tail. subsequently, the changes in lift 、 drag and pitching moment are derived, giving an engineering model for the prediction of the increments in the aerodynamic characteristics caused by the interference between the propeller slipstream and the other parts of aircraft. this method offers a powerful means to the calculation of the aerodynamic interaction between the propeller and the aircraft, providing reliable data for the design of and aerodynamic calculation on propeller - powered aircraft

    本文以滑流干擾的機理為出發點，研究了螺旋槳滑流與飛機機翼、機身、平尾組合體之間的相互影響，推導出滑流引起的飛機升力、阻力和俯仰力矩的變化，給出了滑流干擾對機體氣動特性影響的工程估算方法，為研究螺旋槳與飛機部件之間的相互干擾提供了有力的工具，為以螺旋槳發動機為動力的飛機的設計和氣動計算提供可靠的依據。
  17. According to flight dynamics, a particle model and an attitude model in launching coordinate system and in quasi missile body coordinate system are established, the influence imposed by constant wind, thrust bias of the motor and connection bias are analyzed

    應用飛行動力學理論，建立了發射坐標系與準彈體系下助推段和分離過程質點運動和姿態動力學模型，分析常風干擾、發動機推力偏差和裝配誤差影響等。
  18. Development of an antiradiation sam, most likely intended to target awacs aircraft and standoff jamming platforms

    研發一種反輻射面對空導彈，最有可能是針對awacs飛機和抵銷型干擾平臺。
  19. We have great variety on the production series : cl11 series metallized polyester film capacitor, x2y2 series emi suppression capacitor, x2 series anti - interference metallized polyester film capacitor, cbb88 series polypropylene film capacitor and cbb65 anti - explosion design metallized polyester film capacitor for ac, cbb6 - 11 series polypropylene film capacitor - high temperature. cbb60 61 series metallized polypropylene film capacitor for ac, cbb21 series metallized polyester film capacitor - box, cl20 cbb20 axial type capacitor, minibox capacitor. electrolytic capacitor and ceramic capacitor, besides the mentioned capacitors, we also have philips and panasonic etc. famous brand capacitor

    主要產品有cl11聚酯膜滌綸電容器， x2y2抗干擾電容器， x2系列抑制電源電磁干擾電容器， cbb88電磁爐專用電容器和cbb防暴電容器， cbb6 - 11高溫型燈具電容器， cbb60 cbb61交流電機用電容器， cl21金屬化聚酯薄膜電容器， cbb21金屬化聚丙烯薄膜電容器， cl20 cbb20金屬化軸向電容器，盒式小型化minibox電容器，並代理飛利浦松下等品牌電容器， l . e . d發光二極體， smd .貼片二三極體。
  20. 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。
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