試驗直升機 的英文怎麼說

中文拼音 [shìyànzhíshēngjī]
試驗直升機 英文
experimental helicopter
  • 試 : 名詞（古代占卜用的器具） astrolabe
  • 驗 : 動詞1. （察看; 查考） examine; check; test 2. （產生預期的效果） prove effective; produce the expected result
  • 直 : Ⅰ形容詞1 （成直線的; 硬挺的） straight; stiff 2 （跟地面垂直的; 從上到下的; 從前到后的） erect; v...
  • 升 : Ⅰ動詞1 （由低往高移動） rise; hoist; go up; ascend 2 （等級提高） promote Ⅱ量詞1 （容量單位） lit...
  • 機 : machineengine
  • 試驗 : trial; experiment; test
  • 直升機 : air horse
  • 直升 : helicopter
  1. There are over 80 sets test apparatus in tech - innovation centre, including : anechoic chamber, vibration tester, vibration measurement analysis, impact instrument, constant temperature and humidity facilities. salt spary test case, circle insulation withstand voltage tester, insulation resistance tester, withstand voltage tester, electric lead tester, electrical leakage tester, earth resistance tester, chassis dynamometer, chassis dynamometer control system, high stability dc resistance tester, electrical capacity tester, temperature rise test system

    中心擁有各類分析測試儀器和試驗裝置80餘臺套，包括：消音室振動臺噪聲振動測試分析系統沖擊儀恆溫恆濕實驗儀鹽霧試驗箱匝間耐壓分析儀絕緣電阻分析儀對地耐壓分析儀泄露電流測試儀對地電阻測試儀測功機測功機控制系統高精度直流電阻測試儀電參數測試儀帶電溫升測試儀復合式三坐標測量儀萬分投影儀及電功測試分析系統等。
  2. A depth sampler is strapped to the running board of the helicopter.

    把深水取樣器固定在直升機的試驗臺上。
  3. Energy consume, electric strength, insulation resistance, ground conductivity, leakage current, microwave leakage, power input, normal temperature, humidity treatment, glow wire, horizontal flame, vertical flame, tracking, ball pressure, rainproof, water splash, dustproof, salt fog, endurance, motor load test, cord flexing, cord pulling, pull & torque test, lamp replacement, construction check etc

    能耗、電氣強度、絕緣電阻、接地連續性、泄漏電流、微波泄漏、功率、溫升、濕熱試驗、灼熱絲、水平燃燒、垂直燃燒、漏電起痕、球壓試驗、防雨淋、防濺水、粉塵、鹽霧、耐久性（壽命）試驗、電機負載試驗、電源線彎折、電源線提拉、拉扭力測試、燈頭互換性、安全結構檢查等。
  4. In chapter 5, the uh - 1 model rotor, the model rotor measured in the present work and the helicopter z - 8 rotor are taken as numerical examples, the calculations on rotor noise under different flight conditions are carried out for validation purposes

    應用該模型，分別以uh - 1模型旋翼、本文試驗的模型旋翼以及z - 8直升機旋翼為算例，對不同飛行條件下的旋翼氣動噪聲進行了計算，驗證了本文的計算方法。
  5. It is important to evaluate accurately the longevity of the part by advance the efficiency of using ae method on detecting crack in fatigue test

    改進及提高聲發射技術對疲勞試驗狀態下的裂紋檢測效率和精度，是準確評估直升機各重要構件壽命的關鍵。
  6. Flight test investigation of helicopter vortex - ring state boundary

    直升機渦環狀態邊界的飛行試驗研究
  7. The china helicopter research and development institute is the only professional scientific research organization for helicopters design, research and experiment. it is the leader of the chinas helicopter development in this industry. the xbrothers security and facility control system has been applied in its computer room

    中國直升機設計研究所是我國唯一一家專門從事直升機設計研究試驗工作的綜合性大型科研單位，在新型號和改進改型設計新技術攻關先進技術預研項目中，充當著中國直升機工業陣營中的「革命軍中馬前卒」 。
  8. Rotating electrical machines - equivalent loading and super - position techniques - indirect testing to determine temperature rise

    旋轉電機.等效加載和過定位技術.測定溫升的直接試驗
  9. Problems appearing at work and tackling methods are both presented. recently, the research result has been applied to the helicopter airscrew harmony loading test. the results of harmony loading test show that it has high performance

    目前，論文的研究成果已經成功地應用在某型直升機旋翼載荷模擬加載試驗系統中，實際加載試驗表明，該加載控制系統能很好的完成加載試驗控制，保證系統的控制性能指標。
  10. His initial hong kong private pilot s licence ( helicopters ) licensing flight test was carried out on robinson r22 helicopter on november 6, 2004, in hong kong

    該名飛行員在二四年十一月六日于香港以robinsonr22型直升機，進行他的香港私人飛行員執照（直升機）的首個牌照的飛行試驗。
  11. Synchronous generator temperature arising test research using energy direct feedback method

    能量直接回饋進行同步發電機溫升試驗的研究
  12. It is important to soft developing. the topic of the paper has been listed in the basic research project for national defence of the " tenth - five project " by the commission of science technology and industry for national defence. one is " distribution experimentation and test technology ", the other is " mathematic helicopter and test technology ". base on the research of literature of the world, we will research the technology of measurement and control system

    本文結合十五國防預研項目「分散式協同綜合虛擬試驗與測試技術」和個五航空預研項目「直升機飛行載荷全數字加載控制和數據採集技術」的研究，在分析了國內外研究現狀和技術發展趨勢的基礎上，對其共性的關鍵技術之一? ?系統開發支持平臺（通用測控平臺）技術展開了深入研究。
  13. Along with development of tiltrotor vehicle ’ s research some theoretical productions have been appeared in some project ( aerodynamic behavior of rotor, kinetic behavior of rotor, rotor / wing aerodynamic interactions, etc. ). in order to carry on further research and experimentation of these project, national - defence science and technology helicopter rotor kinetic lab of our school begin to building tiltrotor model bench. base on need of this bench, this paper study / design pitch control system on it

    隨著對傾轉旋翼飛行器的深入研究，傾轉旋翼的氣動特性、動力學特性、旋翼/機身間的氣動干擾等課題方面已有一定的理論成果出現。為了對這些課題進行深入研究和試驗驗證，我校直升機旋翼動力學國防科技重點實驗室著手建造了傾轉旋翼模型實驗臺。
  14. The flight test of ec155 tells us that inter - blade dampers can work very well in stabilizing the system ; another advantage of this configuration is it can make the hub system simpler and reduce the drag of air to the hub which is very important for helicopters with 4 or more than 4 blades

    Ec155的飛行試驗證明，這種減擺器布置方式對提高穩定性效果明顯;這種布置方式的另外一個優點是可以簡化槳轂，降低其氣動阻力，對多槳葉（四片和四片以上）直升機有重要意義。
  15. During the design of new type attack helicopter, we need to assembly the engine, the gear box, the driving shaft and the rotor system together on the ground, so that we can use it to test its performance and try whether they work in harmony

    在某新型武裝直升機的研製過程中，需要把發動機、減速器、傳動軸和旋翼系統在地面進行裝配，做地面試驗，以檢驗各子系統的性能和相互間的協調性。
  16. The pilot s conversion to the ec155b1 helicopter type was conducted in hong kong during january and february 2003, by technical and flying instructors from eurocopter, the helicopter manufacturer. his initial licensing flight test and operator proficiency check were carried out on 6 february 2003. the pilot was in current flying practice on both the as332l2 super puma and ec155b1 as aircraft commander

    該名飛行員在二三年一、二月期間，通過直升機製造商歐洲直升機公司的技術及飛行教官之考核，于香港獲準轉為駕駛ec155b1型直升機機種，他于同年二月六日通過同類型直升機首個牌照的飛行試驗及操作人員能力測試。
  17. This dissertation mainly studies how to eliminate extra force to finish loading test of a certain helicopter roll booster wear test - bed

    本文主要討論某型直升機槳葉助力器壽命試驗臺的液壓伺服加載系統的研製及其消除多餘力的方法。
  18. In order to adapt well to the development of the overhaul with the locomotive, the article introduces a digital auxiliary motor test - bed based plc and touch screen technology, being an updated product of routine manual switch and relay - controlled test - bed, it can accomplish the functions such as testing, checking and other manipulations to d. c engine, a. c engine and phase converter through hmi - touch screen

    為適應機車檢修水平現代化的發展步伐，本文研究設計了基於plc和觸摸屏技術控制的機車數字化輔機試驗臺，作為常規的手動開關和繼電器控制試驗臺的升級換代產品，通過人機界面（ hmi ） ? ?觸摸屏完成對直流電機、交流電機、劈相機的試驗檢測操作。
  19. Second, taking the characteristics of the mrfd and its matching with blades into consideration, the squeeze mode mrfd was designed. after that, the mechanical characteristics of the squeeze mode mrfd was tested to tell us that, compared with those mrfd work in other modes, the squeeze mode is advantageous for its compact structure, less displacement and higher strength. third, with the test data, we get the force model which use imitatation

    其次，考慮磁流變阻尼器自身特點與直升機旋翼的匹配因素，設計了以擠壓模式為工作方式的磁流變減擺器，並對磁流變減擺器進行了力學特性試驗，試驗結果表明擠壓式磁流變阻尼器與其他工作模式的磁流變阻尼器相比具有結構緊湊、位移小、出力大等優點。
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