飛機機體部件 的英文怎麼說

中文拼音 [fēijījītǐbùjiàn]
飛機機體部件 英文
airframe components
  • 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
  • 體 : 體構詞成分。
  • 部 : Ⅰ名詞1 （部分; 部位） part; section; division; region 2 （部門; 機關或組織單位的名稱） unit; mini...
  • 件 : Ⅰ量詞（用於個體事物） piece; article; item Ⅱ名詞1. （指可以一一計算的事物） 2. （文件） letter; correspondence; paper; document
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 機體 : 1. [生物學] （有機體） organism 2. [航空] airframe
  • 部件 : component; unit; parts; assembly; subsystem; secundina （pl. secundinae）
  1. The combine harvester is overall 3 packets of period of efficacy are 1 year ; 3 packets of period of efficacy are main part 2 years, main part is to point to internal - combustion engine airframe, cylinder housing of casing of lid, flywheel, frame, gear - box, clutch, change gear case of machine, final drive to body

    聯合收割機整機三包有效期為1年；主要部件三包有效期為2年，主要部件是指內燃機機體、汽缸蓋、飛輪、機架、變速箱箱體、離合器殼體、轉向機、最終傳動齒輪箱體。
  2. 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。
  3. The thermal wave nondestructive testing technology based on emissivity of the object, it can find surface and subsurface flaws in the composites of airplane through measuring difference in temperature between flaws and materials by active heating methods and inspection system

    摘要紅外熱波無損檢測基於物體的熱輻射特性，利用主動加熱技術，通過相關的檢測系統記錄試件表面缺陷和基體材料由於不同熱特性引起的溫度差異，進而判定飛機復合材料表面及內部的損傷。
  4. Then we explicate the hardware design in details, including implementing ad convert, extending multiple serial communications and external memory, and using cpld do some logic controls. thereby we implement abundance simulation interface, flexible digital interface and serial communication interface. at last we describe the software design, including software design of cpld basing on vhdl and software design of dsp

    本文首先介紹飛行模擬訓練系統的主要組成；接著說明飛控計算機整體系統方案的設計；然後詳細說明飛控計算機硬體平臺的設計，包括ad轉換、多串口通信、外部存儲器的擴展以及採用可編程邏輯器件cpld實現電路的邏輯控制等幾部分，體現了系統豐富的模擬介面、方便靈活的數字介面和串列通信介面；最後是軟體部分的編程，包括cpld部分的硬體描述語言程序設計，和dsp部分相關的程序設計。
  5. Sunvo company has launched the domestic and international advanced process technologies continuously, and developed hundreds of different types of small - scale, single - slot, multi - slot standard and non - standard ultrasonic cleaners using imported and domestic high - quality components, applicable to bearing parts, automobile parts, magnetic materials, musical instruments, aircraft parts, electroplating parts, optical components, circuit boards, watch components, semiconductors, polyester filtering cores, medical equipment, military products, nuclear industry and precision instruments and so on

    山河不斷引進國內國際先進工藝技術，採用進口及國內優質元器件，開發出幾百種規格的小型、單槽、多槽等標準和非標的超聲波清洗機，適用於軸承零件，汽車零部件，磁性材料，樂器零件，飛機零件，電鍍零件，光學零件，電路板，鐘表零件，半導體，滌綸過濾芯，醫療器械，軍工產品，核工業，精密儀器等等行業。
  6. Main part is to point to internal - combustion engine airframe, air cylinder housing of casing of lid, flywheel, frame, gear - box, axle shaft, steering gear housing, poor fast implement housing of hub of casing of housing, final drive - box, apply the brake, towing plate, promotion

    主要部件是指內燃機機體、氣缸蓋、飛輪、機架、變速箱箱體、半軸殼體、轉向器殼體、差速器殼體、最終傳動箱箱體、制動轂、牽引板、提升殼體。
  7. 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。
  8. Applying the above - mentioned method, the author developed an approximate developing - mapping system based on catia v5 using vb, realized the development computing of panel surface and auto - drawing of developed shape in catia, dealt with the problem : getting mesh data from analysis & simulation module of catia, picking up structure information data in iges, showing 2d developed model in catia

    應用上述幾何展開演算法，作者基於windowsnt 2000 xp系統和catiav5平臺用visualbasic開發了一套「不可展曲面近似展開和內部結構信息映射系統」軟體，簡稱demaps系統，實現了飛機壁板類零件的展開計算和展開圖形自動繪制。
  9. Based on the monte - carlo simulation, optimization of shielding layer material and their thicknesses were obtained for implementing partial shielding of semiconductor devices in space vehicles

    針對我國空間飛行器中對半導體器件較常用的局部屏蔽加固的方法，在m - c計算機模擬的基礎上對屏蔽層材料及其厚度進行了優化設計。
  10. Better base treatment for following coating adhesive parts, such as coating of airplane parts, car parts, electric appliances cases and home decoration, besides, it can make

    ，如飛機鋁合金蒙皮汽車鋁合金車體室內裝飾用鋁合金幕墻機電家電通訊等鋁合金部件需塗裝粘接的底層
  11. Equip along with the weapon continuously creative, the sharp weapon also raises continuously in the quantity and the request on the quantities, processing to produce the mode and productions to process the production request that the equipments have already ca n ' t satisfy the long sail company originally possessed. through the common consultation of the company leadership and all employee, decide to throw in the capital, carry on to the company to reform completely, expand the scale, lead quantity and quantities that controls the production line to raise the production into the number, thus satisfy the competition ability that the productivity request combines to raise the business enterprise continuously. this thesis mainly what to study is the long spring aviation liquid to press to control the limited company number to control the degree of progress that the production line installs the item excellent turn, pass to use the item management of theories resolve the problem within actual application

    長春航空液壓控制有限公司前身是中國航空第二集團下屬第133廠，是一個為飛機配套機載設備的軍工企業，成立於1998年，隨著我軍裝備事業的不斷發展，對武器裝備的需要也越來越迫切，大批量的高精尖武器裝備已經成為打贏高科技精裝備條件下局部戰爭的法寶，因此長春航空液壓控制有限公司針對這一嚴峻形勢，果斷地提出利用項目管理的知識體系，引進數控生產線項目，在保證企業正常生產和安裝質量的前提下，縮短工期，節約成本並通過項目管理知識體系的運用，用系統的管理知識，提高管理效率、管理水平，並運用到其他的項目中，從而最終提高企業的生產力和競爭力。
  12. Ballistic composite with outstanding ballistic properties and without twice kill - wound effect has been widely applied in body defence and military arms for the modern high - tech war, for example, ballistic waistcoat, helmets and the components for truck, airplane and marine

    為適應現代高科技戰爭，防彈復合材料在人體防護和軍事裝備的防護方面已得到廣泛的應用，如防彈背心、頭盔，以及坦克、飛機、艦船等的防護部件。防彈復合材料具有優良防護性能，且無「二次殺傷效應」 。
  13. In 2003, a blow from a piece of foam led to the fiery disintegration of the space shuttle columbia as it re - entered earth ' s atmosphere, killing all seven astronauts on board

    2003年，一塊絕緣部件的撞擊導致「哥倫比亞號」航天飛機在重返地球大氣層時解體燃燒，機上7名宇航員全部喪生。
  14. I hope that this meeting will lead to the rapid release of all of the members of the crew back to the united states so they can be returned to their organizations and returned to their families, and i also hope that it also will lead to the rapid return of our airplane. so i am encouraged by the fact that the meeting is taking place

    我希望這是結束這一事件的開端。我希望這次見面將使全體機組人員很快返回美國，使他們能夠返回他們所在的部門，回到家人身邊。我還希望見面還能使我們的飛機很快交還給我們。
  15. A finite element model including full - scale circular arc windshield glass and the relative parts of the plane is established using ls - dyna3d v. 950 code in the computer simulation and is validated using the result from the test

    數值模擬中，建立了包括飛機相關部件的全尺寸有限元模型。鳥體採用ale描述。有限元模型採用ls - dyna進行了分析。
  16. And establishing the model of the thrust vectoring nozzle is the base for researching thrust vectoring technique and engine performance with vectoring nozzle, especially the integration of flight and propulsion system control ( ifpsc ). so thrust vector modeling is very important and meaningful

    矢量噴管是實現推力矢量的關鍵部件，建立其數學模型是推力矢量技術尤其是開展帶矢量噴管的發動機研究以及飛推一體化綜合控制研究的基礎，具有十分重要的意義。
  17. Therefore, this thesis first introduces the relevant regulations and requirements of the quality system, describes the self - audit system and the requirements for the overall repair process of aircraft parts, which includes preliminary inspection, acceptance, repair and release procedure

    因此，本論文首先介紹了航空電子維修站質量體系對這些方面的規定及要求，並描述了航空電子維修站的自我質量審核系統的情況，以及飛機部件從進廠檢查、接收、修理直到放行的全部修理過程的要求。
  18. Specification for general requirements for equipment for use in aircraft - all equipment - environmental conditions - fluid contamination

    飛機設備一般要求規范.第2部分:各種設備.第3節:環境條件.流體污染
  19. Shanghai aircraft manufacturing factory has strong capability for aircraft final installation, excellent aircraft subassembly and join technology, standardized test and calibration equipments, reliable human resources and quality assurance systems

    上海飛機製造廠擁有大型飛機總裝能力精湛的部件對接技術國際規范的測試和校驗設備可靠的人力資源和質量保證體系。
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