gas turbine engine 中文意思是什麼

gas turbine engine 解釋
燃氣輪機
  • gas : n （pl gases ）1 氣，氣體，氣態 〈cf fluid; solid〉 2 可燃氣，煤氣，沼氣；【礦物】瓦斯。3 【軍事...
  • turbine : n 【機械工程】（渦）輪機，葉輪機，汽輪機，透平機。 a hydraulic [water] turbine 水輪機。 a steam t...
  • engine : n. 1. 機械，機器。2. 引擎，蒸汽機，發動機。3. 機車，車頭。4. 工具；〈古語〉方法，手段。vt. 給…安裝發動機。
  1. Cutaway of the pw 4000112 - in ( 284. 48cm ) gas turbine engine, showing fan bypass section

    渦輪發動機剖面圖，展示風扇旁路部分。
  2. Experimental studies on s1a - 02 gas turbine with water injection into compressor interstage / inlet as well as that on turbocharger self - loop test rig with inlet water injection are introduced. test results are in good accordance with simulation results, wet compression can lower compression work and increase engine power output so engine performance is enhanced, if engine power output is not changed, efficiencies of compressor and this engine become higher and turbine inlet temperature and fuel consumption become lower and if keeping t4 the same as that before wet compression is used, efficiencies become furthermore higher and engine power output increases greatly

    實驗結果和計算結果同樣表明：濕壓縮減少了壓氣機所消耗的壓縮功，增加了燃氣輪機的輸出功率，提高了燃氣輪機性能，如果保持發動機輸出功率恆定，濕壓縮可以提高壓氣機和整個燃氣輪機機組的效率，與此同時，渦輪進口溫度t _ 3 ~ *和燃油消耗率下降；如果保持渦輪排氣溫度t _ 4 ~ *恆定，壓氣機和燃氣輪機機組效率進一步提高，燃氣輪機輸出功率增加。
  3. Plasma ignition for engine is a new pattern portfire, it firstly lights up the start - up oil and form ignition torch to ignite the main oli in the combustor. lt is a new technolygy, at the present only ukraine have used this technique in marine gas turbine and the ground gas turbine to increase the reliability of retro fires and extend the concentration limit of retro fires

    等離子點火技術是一門新興技術，目前只有烏克蘭將該技術應用到了艦船燃氣輪機和地面燃氣輪機上，由於該項技術主要點火設備具有獨特的放電特性和較大的放電能量，並且能量集中，使發動機的點火可靠性和點火的濃度極限得到了極大的提高。
  4. Accounting for creep and stress relaxation, a long - term life and low cycle fatigue life prediction method for gas turbine engine hot section is established

    摘要建立了考慮蠕變和應力鬆弛的航空發動機渦輪葉片等高溫構件的持久壽命和低循環疲勞壽命預測方法。
  5. Standard test method for determination of contaminants in gas turbine and diesel engine fuel by rotating disc electrode atomic emission spectrometry

    轉盤電極原子發射光譜法測定氣輪機和柴油發動機燃料中雜質的標準試驗方法
  6. Diesel engine, main turbine, generator turbine, main boiler, diesel generators, deck crane, deck machineries, propeller, controllable pitch propeller, switchboard, engine control console, fire extinguishing system, inert gas system, aux. boiler, oil purifier, navigation equipment, life boat, anti rolling system, hatch cover, compressor, fin stabilizers, valves, anchor, chain and scaffolding, control system for lng carrier and various machinery for lng carrier

    主機柴油機，液化氣船主機透平鍋爐貨油泵，機艙泵，發電機，甲板吊機，甲板機械，螺施槳， cpp ，配電盤，主機遙控，消防沒備， igs ，輔鍋爐，分油機，航海儀器，救身艇，減搖裝置，艙口蓋，空壓機，減搖鰭，閥門，錨，錨鏈，船舶腳手架，液化氣船控制系統，液化氣船用各種沒備
  7. Test method for determination of contaminants in gas turbine and diesel engine fuel by rotating disc electrode atomic emission spectrometry

    採用旋轉圓盤電極原子發射光譜法測定氣體渦輪機和柴油機燃料雜質的試驗方法
  8. Plasma ignition technique for engine is a new pattern technique, at the present some developed countries have studied plasma ignition system. ukraine have firstly used this technique in marine gas turbine and pumping station of the gas turbine used for the long distance oil transportation main from siberia to europe which increases the reliability of retrofires and extend the concentration limit of retrofires

    目前，世界上幾個技術發達國家都開展了等離子點火系統的研究，尤其是獨聯體國家更是率先把等離子點火系統用於艦用燃氣輪機以及從西伯利亞到歐洲的遠距離輸油干線的燃氣輪機泵站上，使發動機的點火可靠性和點火的濃度極限得到了極大的提高。
  9. On the contrary, if temperature gradient is relatively low, combustor only undergo low compressive stress at high temperature. the combustor of engine has a longer life length. these results can provide some reference for maintain and design for gas turbine combustor

    分析也表明，若在起動過程中筒壁的溫度梯度較為平緩，火焰筒的氣膜唇邊在起動完成後始終受微小的壓應力作用，火焰筒的壽命可以大大延長。
  10. Abstract : the paper presents the development and applications of thermal barrier coating, seal ( clearance control ) and wear resistance coating for aero gas turbine engine

    文摘:介紹了在現代航空燃氣渦輪發動機上熱噴塗熱障、封嚴、耐磨塗層的開發應用實例。
  11. Aviation gas turbine engine

    航空燃氣輪機發動機
  12. The proportion of natural gas in consumption of energy is constantly rising. gas turbine and engine cogeneration is one of the rational ways in utilization of natural gas. using index system evaluating thermodynamic performance of energy utilization systems on the basis of electricity, the allocation models of the fuel consumption for the gas turbine and engine chp plant were deduced

    本文根據以電量為基準的熱力性能評價思想，研究燃機熱電聯產煤耗分攤問題，並給出了燃機燃氣蒸汽聯合循環熱電聯產、燃機簡單循環熱電聯產系統的電、熱兩種產品生產的煤耗分攤模型。
  13. The program software and design hardware realize the control of the digital governor of n6136 turbocharged diesel and speed adjust system of sla - 02 gas turbine, they can control the rotating speed of the diesel and gas turbine in the forward experiment and can make the main engine changeover processes of the codog physical analog experiment rig possible to be controlled through computer, therefore to set up a solid foundation for the research of possible projects in the changeover processes

    通過軟體編程和硬體設計實現了對n6135柴油機的電子調速器和s1a - 02甲燃機的調速系統進行控制，能夠在實驗前和實驗中實時的對柴油機和燃氣輪機的轉速變化進行設定和控制，使codog物理模擬實驗臺主機切換過程實現計算機控制，為實現多方案切換過程研究打下堅實的基礎。
  14. Finally, in order to solve the problems encountered in experiment, an improved design, including gas path, mechanism and controller design, is proposed. experiments are accomplished in the improved system platform, and the results demonstrate that the improved system can meet the requirement of simulating the turbine outlet temperature of aero - engine

    最後，針對試驗中遇到的問題，從氣路部分、機械部分以及控制器三個方面對溫度模擬系統進行了改進設計，並在改進的系統平臺上進行了試驗，試驗結果表明改進后的系統能基本滿足對發動機渦輪出口溫度信號模擬需求。
  15. Employing gas engine to drive heat pump is better choice compared to stirling engine, turbine and gas turbine under today ' s condition

    對斯特林、汽輪機、燃氣輪機和內燃機幾種熱機熱泵的動力選擇分析結果表明：採用燃氣機驅動熱泵是一個比較好的選擇。
  16. In the paper, the structure type of torpedo turbine engine and the three - speed system states of work gas were researched. the work process of torpedo turbine engine was analyzed

    本文對魚雷渦輪機結構類型、魚雷渦輪機的三速制工況進行了計算研究，對渦輪發動機的工作過程進行了分析。
  17. Sac has become a national aeroengine production base and one of top 5 motorcycle enterprises at home. sac had a splendent achievement in the past years, for example, it manufactured firstly aeroengine, heavy motorcycle engine and light industrial gas turbine. we are sincerely welcome businessmen at home and abroad to come for business

    現已形成由一個上市公司6個事業部5個中外合資企業11個全資子公司9個控股參股企業組成的母子公司構架，是一個以資本為主要聯結紐帶以航空發動機和摩托車為主導產業，集科工貿為一體面向國際國內兩個市場的大型集團公司。
  18. Film cooling of the surface of a gas turbine blade was studied in a large - scale low - speed opening wind tunnel according to actual requirement of the design of aero - engine. the surface of a gas turbine blade was cooled by cylindrical holes in the experiment, with the hole number of fifteen in stator and eight in rotor

    應航空發動機設計的要求，在大尺寸低速葉柵傳熱風洞中分別對發動機渦輪導向葉片和動葉表面的氣膜冷卻特性進行了研究，具體研究在不同氣膜孔出流時，在不同主流雷諾數和吹風比情況下葉片表面局部換熱系數的分佈規律。
  19. The combustor of gas turbine engine operates under inhomogeneous high temperature, which causes very complicated mechanical behavior of combustor ' s material, and makes combustor failure

    燃氣渦輪發動機火焰筒在非均勻溫度場的作用下，材料會呈現復雜的力學行為，導致使用過程中出現裂紋而造成故障。
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