渦輪機壓氣機 的英文怎麼說

中文拼音 [guōlúnjīyāqìjī]
渦輪機壓氣機 英文
turbo machinery compressor
  • 渦 : 渦名詞1. （漩渦） eddy; whirlpool; vortex 2. （酒窩） dimple
  • 輪 : Ⅰ名1 （輪子） wheel 2 （像輪子的東西） wheel like object; ring; disc 3 （輪船） steamer; steamboa...
  • 機 : machineengine
  • 壓 : 壓構詞成分。
  • 氣 : Ⅰ名詞1 （氣體） gas 2 （空氣） air 3 （氣息） breath 4 （自然界冷熱陰晴等現象） weather 5 （氣味...
  • 渦輪機 : aeroturbine
  • 渦輪 : [機械工程] turbine; worm wheel渦輪泵 [航空] turbopump; roturbo; 渦輪發動機 turbine engine; 渦輪風...
  1. Each module has a microcomputer with both turbocharged and naturally aspirated calibrations resident in its internal rom.

    每一模件都有一個在其內部Rom中間同時保存有渦輪增壓和自然吸氣計算的微計算機。
  2. The turbine engine has a compressor which turns at high speed.

    渦輪發動機有一個高度旋轉的壓氣機。
  3. 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。
  4. By using harika algorithm, the characteristic of a high - pressure compressor is calculated at different installation angle of the inlet guide vane and the stator vanes ; the characteristics of a high - pressure turbine and a low - pressure turbine are simulated at different installation angles of the guide vane based on ainley method

    本文用harika演算法計算了導流葉片和靜子葉片安裝角度可調的變幾何高壓壓氣機特性；用ainley法計算了渦輪導向器面積可調的高壓渦輪和低壓渦輪的特性。
  5. Testing methods of turbo blowers and compressors for gases by loop arrangement

    渦輪式鼓風機和氣體壓縮機的封閉試驗方法
  6. Touch on developing large - flow and high - pressure ratio impressor and large - enthalpy drop turbine, reducing harmful emission, solving the major problems of high - temperature blade material, cooling, protective coating and single - grain blade casting, and comfirm some important manufacturing techniques

    涉及了開發大流量高壓比壓氣機、大焓降渦輪，降低有害排放量，解決高溫葉片的材料、冷卻、保護塗層及單晶葉片鑄造等主要問題，並確認了一些關鍵的製造技術。
  7. And those characteristics of compressor and turbine are put into the steady - state design and off - design performance program of augmented turbofan engine, to calculate the influence of the geometry changing of single component on the performance of engine

    計算了單個可變幾何部件的調節（包括高壓壓氣機、高壓渦輪、低壓渦輪、混合器進口面積比和噴管喉道面積）對發動機穩態性能的影響。
  8. The precondition of establishing mathematics model of torpedo turbine system in design condition is to fulfill the external conditions ( such as torpedo sailing speed and depth etc. ) and inner conditions ( such as turbine power and efficiency etc. ). after establishing mathematics model of torpedo turbine system in design condition, we compiled simulation program to compute all kinds of inner parameters of turbine engine include engine type, principal layout of turbine, inner structure of turbine and state parameters of gases

    首先分析設計工況時渦輪機動力系統，在滿足魚雷動力系統的各項外部條件（如魚雷航深、航速等）和內部條件（如渦輪機功率、效率，燃燒室壓力、溫度，轉子機械強度等）的前提下，建立起設計工況渦輪發動機的數學模型，編程計算並確定渦輪機內部機械結構和燃氣熱力學狀態各參數。
  9. An interpolation program is used to convert the fluent result data to the ansys load data. it is a new method to analyze turbine tip clearance. in this paper, some research of the numerical computation of the tip clearance of aero - engine is done, the parametric method is used and the research on the flow, heat and structure integration analyses is accomplished

    本文對渦輪機匣氣熱固一體化分析方法做了研究，通過編制了載荷轉換與施加程序，從氣熱計算模型中提取溫度場計算結果，並作為載荷加入到熱固耦合計算模型中，實現了高壓渦輪機匣的一體化計算分析，為實現渦輪葉尖間隙的氣熱固一體化分析打下了基礎。
  10. For turbo - charged engines, due to the high rotating speed of the turbocharger, the air inlet noise is much higher than non - turbo - charged engines

    對于採用渦輪增壓的發動機，由於渦輪增壓器的轉速一般較高，因此其進氣噪聲明顯高於非渦輪增壓的發動機。
  11. Test method for evaluation of the aeration resistance of engine oils in a direct - injected turbocharged automotive diesel engine

    直接噴射式渦輪增壓汽車柴油發動機的機油的抗混氣性能的評價試驗方法
  12. Measurement and control systems for a turbocharger compressor performance test rig

    渦輪增壓器壓氣機性能試驗臺測控系統
  13. Of high speed four - stroke turbocharging or getter - ion style engine where oils of performance up to api sf cd are recommended

    適用於要求使用api sf cd規格油品的普通化油器式汽油發動機和高速四沖程渦輪增壓或自然吸氣式柴油發動機。
  14. The imperfection and fuzziness affecting the vibration reliability of structural components is analyzed, the concept of fuzzy safety state on vibration of structural components is developed, the fuzzy failure district of the resonant vibration of structural components and its membership function is constructed, the fuzzy failure district of the intensity is also constructed, the fuzzy model to assessment the vibration reliability of structural components is built and is applied to the vibration reliability assessment of the turbine blades and the compressor blades of the aero - engine

    摘要分析影響構件振動可靠性的不確定性和模糊性因素，定義構件振動模糊安全狀態，構建構件振動的模糊共振失效區域及相應的隸屬函數、模糊強度失效區域及相應的隸屬函數，建立構件振動可靠性計算的模糊模型，並將其應用於某航空發動機壓氣機、渦輪葉片的振動可靠性計算。
  15. Based on the exhaust heat data of the iurbine ( 6160a - 12 ) and the micro gas turbine produced in japan, parameters of test - bed such as deferent thermal flow temperature and pressure are defined by the calculation of design parameter in method of combined theory and experience data

    以柴油機（ 6160a - 12 ）和日本的微型燃氣渦輪機尾氣參數為設計基礎，通過理論和經驗數據相結合的方法進行設計參數計算，確定了模擬實驗臺熱流量、出口溫度及壓力等參數。
  16. Secondly, the paper analyzes abnormal performance in diesel engine according to engine structure model and function model. the system of diesel engine is divided into several subsystems, such as inlet tube, cylinder, exchange tube, turbo charger. all these subsystems are zero - dimension system

    其次，根據柴油機的功能模型和結構模型，對柴油機熱工故障作了較深入的分析，把柴油機系統劃分為進氣管、氣缸、排氣管、渦輪增壓器等零維子系統，建立了一個較通用的柴油機熱工故障的零維模擬模型。
  17. Suitable for demanding to use generalizing oil device type four stroke turbine pressurization of gasoline engine and high speed or the breathing in type diesel engine naturally of specification oil of api sf cd

    用途適用於要求使用api sf cd規格油品的普通化油器式汽油發動機和高速四沖程渦輪增壓或自然吸氣式柴油發動機。
  18. Standard test method for evaluation of aeration resistance of engine oils in direct - injected turbocharged automotive diesel engine

    直噴式渦輪增壓汽車柴油發動機中機油透氣阻力評價的標準試驗方法
  19. Some of the air is used for cooling the turbine blades and nozzle guide vanes, and part of it is employed to cool and seal the turbine discs

    在現代航空發動機中，從壓氣機引出的壓縮空氣一部分用來冷卻渦輪葉片和渦輪導向葉片，另外一部分用來冷卻和密封渦輪盤。
  20. With ms6001 gas turbine as an investigative object, an intelligent simulation and monitoring system was developed, which provides a good method to display and handle monitoring data of ms6001 gas turbine

    摘要以法國引進的ms6001燃氣輪機發電機組為研究對象，針對它開發了一套以燃氣輪機循環計算、壓氣機和渦輪特性計算及燃氣輪機變工況計算為基礎的工況監測顯示系統軟體。
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