試飛發動機 的英文怎麼說

中文拼音 [shìfēidòng]
試飛發動機 英文
flight test engine
  • : 名詞(古代占卜用的器具) astrolabe
  • : 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...
  • : 名詞(頭發) hair
  • : machineengine
  • 試飛 : test flight; trial flight試飛 (駕駛)員 test pilot
  1. The evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    敘述了20世紀50年代以來中國航天固體火箭推進技術的展歷程,介紹了9種最具代表性的固體火箭的技術特徵、研製過程、地面驗和行情況,這些分別應用於中國的探空火箭、運載火箭上面級和應用衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的展水平
  2. Abstract : the evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    文摘:敘述了20世紀50年代以來中國航天固體火箭推進技術的展歷程,介紹了9種最具代表性的固體火箭的技術特徵、研製過程、地面驗和行情況,這些分別應用於中國的探空火箭、運載火箭上面級和應用衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的展水平
  3. Starting with the invention of the bicycle, going on to sports cars, cars with jet engines, rocket - powered cars, attempts to break the sound barrier, and rocket - engine airplanes

    明自行車開始,一直到賽車,噴氣汽車,火箭力汽車,嘗突破聲障和火箭
  4. Method of test data processing for missile used turbojet - part3 : flight test

    彈用渦輪噴氣驗數據處理方法第3部分:
  5. In order to determination the thrust, the thrust definition and many control parameters are analyzed discussed, which mass flow rate and flight altitude are involved. it is difficult to measure the flight thrust of solid rocket ramjet directly

    通過討論高空行推力與地面可測參數的關系,得到了固體火箭沖壓高空行狀態下推力折算方法,並開相應的計算程序。
  6. Bauer howden, inc. is a designer and manufacturer of aircraft airframe and engine components and accessories test equipment

    設計與製造身、零件與附件測設備。
  7. When it becomes necessary to examine the altitude performance of an aircraft engine, three types of facilities may be usedaltitude wind tunnels, altitude test beds and flying test beds.

    當需要考察一臺航空的高空性能時,可以利用三種型式的設備,即高空風洞、高空驗臺和驗臺。
  8. The engine cracked on the first test flight.

    在首次時,生裂紋。
  9. Aircraft engine test facilities

    驗設施
  10. Tuesday, british pilot andy green put the pedal to the middle in an experimental car and shattered the world land - speed record for a car powered by diesel engines

    周二,英國行員安迪.格林在一輛驗車中將腳踏板放在中間,並以這輛柴油助力的汽車打破了車陸地行駛的世界紀錄。
  11. This paper presents a simulation test control system of an airplane engine operating system, which control motor to simulate the force and velocity of throttle lever and the torque on axis

    本文闡述了某型操縱系統地面模擬驗控制系統,它主要控制力矩電去模擬油門桿上的速度和力以及模擬輸入軸的力矩。
  12. The simulation experiment has been done on a turbofan aeroengine. simulation results indicate that the neural network controller has quick response and has good performances in the full envelope

    對某型渦扇行包線內不同狀態點進行了模擬驗,模擬結果表明,控制器響應速度快,魯棒性好,取得了良好的效果。
  13. 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。狀態監測是性能的重要檢測手段,通過狀態監測和車工作可以對進行性能調整、磨合運轉和故障分析,最終達到提高質量的目的。
  14. In order to improve panther ' s performance, various powerplants were tested and experimentally mounted including, aircooled man / argus, modified aircraft bmw and diesel daimler - benz engine

    為了提高黑豹的性能,測驗安裝了不同的力裝置,包括man /阿耳弋斯的空冷,由改進而來的bmw和戴姆勒奔馳的柴油
  15. Standard test method for corrosiveness and oxidation qualility of hydraulic oils, aircraft turbine engine lubricants, and other highly refined oils

    液壓油渦輪潤滑油和其他高精煉油的腐蝕性和氧化穩定性的驗方法
  16. Development for this plane began as early as 1938 and the first prototype made its maiden flight still propulsed by a piston engine in april 1941. the first jet powered version flew in july 1942

    Me262的開始於1938年早期,第一架原形在1941年4月首次,由一臺活塞式推進,第一架使用噴氣式推進的型號於1942年7月首
  17. There are great differences between ground test of a flight vehicle ' s aerodynamics and that of a dual - mode scramjet when ground test facilities are used to do experiments on a dual - mode scramjet engine, the components of incoming flow and its parameters, including total pressure, total temperature ( or total enthalpy ) and velocity must be simulated. at the same time, since the fuel ' s resident time within a combustor is very short, on the order of one millisecond, it is difficult to measure the flow - fields

    進行雙模態沖壓地面驗研究時,必須要求驗設備能模擬實際行條件下來流氣體的組分、總壓、總溫(或總焓)以及來流氣體的流速度;同時由於燃料在燃燒室內駐留的時間很短,一般為毫秒量級,從而使流場物理量的測定顯得非常困難。
  18. The importantance of database in the aero - engine vibration mortoring system is analysed in chapt 5. according to the requirement of vibration mortoring in flight test, a database has been designed with mircrosoft access2000

    最後,本文論述了數據庫系統對和振監測的重要性,分析了數據庫系統的基本原理、振監測數據庫的功能和數據需求,使用access2000針對當前的型號設計了振監測據庫。
  19. Various balance applications and operations on : crankshafts, propshafts, engine balance stands, flywheels, clutch plates, engine pulleys / dampers, torque converters, transmission parts

    廣泛應用於曲軸、傳軸、平衡測臺、輪、離合器片、皮帶輪/阻尼器、扭矩變換器總成及全部傳零部件等。
  20. Simulation results presented here demonstrate that during accelerating flight at constant altitude thrust increases up to approximately 12 percent in the maximum thrust mode, and at subsonic cruise specific fuel consumption decreases up to 2 percent in the minimum fuel consumption mode

    驗結果表明兩種優化模式下,推綜合控制的優化演算法可以顯著提高性能,也驗證了該優化計算設計方案是可行的。
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