高壓渦輪 的英文怎麼說

中文拼音 [gāoguōlún]
高壓渦輪 英文
high pressure turbine (hpt)
  • : Ⅰ形容詞1 (從下向上距離大; 離地面遠) tall; high 2 (在一般標準或平均程度之上; 等級在上的) above...
  • : 壓構詞成分。
  • : 渦名詞1. (漩渦) eddy; whirlpool; vortex 2. (酒窩) dimple
  • : Ⅰ名1 (輪子) wheel 2 (像輪子的東西) wheel like object; ring; disc 3 (輪船) steamer; steamboa...
  • 高壓 : 1 (殘酷迫害; 極度壓制) high handed 2 [氣象學] (高氣壓) high pressure3 (高電壓) high tension...
  • 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. The turbine engine has a compressor which turns at high speed.

    發動機有一個度旋轉的氣機。
  2. The turbine is spun by the high-pressure gases.

    燃氣驅動旋轉。
  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:濕縮減少了氣機所消耗的縮功,增加了燃氣機的輸出功率,提了燃氣機性能,如果保持發動機輸出功率恆定,濕縮可以提氣機和整個燃氣機機組的效率,與此同時,進口溫度t _ 3 ~ *和燃油消耗率下降;如果保持排氣溫度t _ 4 ~ *恆定,氣機和燃氣機機組效率進一步提,燃氣機輸出功率增加。
  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氣機特性;用ainley法計算了導向器面積可調的高壓渦輪和低的特性。
  5. Based on an engineering background, through numerical simulation of the flow field in the hp turbine of the energy efficient engine ( e3 ), the article research the unsteady flow in a transonic turbine stage, the unsteady phenomena in the stage include the shockwave, wake, shedding vortex, endwall vortex, passage vortex and leakage vortex, etc. there are two shockwaves generated on the vane the tailing edge, one on suction side is named moving shockwave, and name another on pressure side steady shockwave

    本文首先對于研究的意義和國內外研究的現狀做了簡要的介紹,再從某工程背景出發,通過對e3發動機高壓渦輪內流場的數值模擬,研究了干涉的周期性的問題,以及級內常見的非定常現象:激波、尾跡、脫落、根腳、通道、漏流。導向器尾緣會出現兩道激波,在吸力面的激波可稱為「運動」激波,力面的激波可稱為「定常」激波。
  6. On the engine, turbocharging can boost power 30 to 40 percent.

    在發動機上採用,可使其功率提3040。
  7. 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

    涉及了開發大流量氣機、大焓降,降低有害排放量,解決溫葉片的材料、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。
  8. To the steam generator a heat exchanger, which converts the feed water in the secondary circuit to high - pressure steam at about 67 bar or 6 700 kpa and deliver it to the " conventional island " via steam pipe for driving the turbine and generator

    內的水帶到蒸汽發生器即熱交換器,蒸汽發生器會將二迴路給水轉化為約67巴或6 700千帕的蒸汽,再經過蒸氣管送到常規島,以推動發電機。
  9. To the steam generator ( a heat exchanger ), which converts the feed water in the secondary circuit to high - pressure steam at about 67 bar ( or 6 700 kpa ) and deliver it to the " conventional island " via steam pipe for driving the turbine and generator

    內的水帶到蒸汽發生器(即熱交換器) ,蒸汽發生器會將二迴路給水轉化為約67巴(或6700千帕)的蒸汽,再經過蒸氣管送到常規島,以推動發電機。
  10. 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(包括氣機、高壓渦輪、低、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。
  11. Areas of application : used for temperature monitoring on generators and high - power electric motors, electric systems, turbines, windings, etc

    應用領域:發電機、電動機、電力系統、機、線圈等的溫度監測。
  12. The turbocharger noise is formed by the rotation noise resulting from the periodical air cutting of the fan blade and the turbulent noise of high - speed gas flows. as a continuous high frequency noise, it mainly falls between the 500 to 10 000 hz range

    器的噪聲是由於葉片周期性地切割空氣產生的旋轉噪聲和速氣流形成的湍流噪聲而形成的,是一種連續性的頻噪聲,主要分佈在500 ~ 10000hz的頻率范圍。
  13. 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,為實現葉尖間隙的氣熱固一體化分析打下了基礎。
  14. Suitable for demanding to use high load, high - power, four strokes, gush out directly, the cold type diesel engine in turbine pressurizations of the api cf - 4 sg grade oil, include various kinds of domestic and importing the heavy - duty transportation vehicle of the new - type diesel engine and engineering machinery working under various kinds of harsh operating modes, lubrication of mine equipment, diesel oil generating set

    用途適用於要求使用api cf - 4 sg級油的負荷大功率四沖程直噴中冷式柴油發動機,包括各種國產或進口新型柴油發動機的重型運輸車輛及在各種苛刻工況下作業的工程機械礦山設備柴油發電機組的潤滑。
  15. The result of the calculation for tip clearance is reasonable when it is compared with theory. two ways are put forward for convention of dimension of the turbine components from high temperature to low one, which is related with tip clearance, a simple example is used to illuminate that the two ways are useful, using the method of design optimization, axiisk and a blade of a certain turhine is analysed, it showes that the method of design optimization is feasible to be used for convertion of dimension of the turbine components. finally, ansys software is used to analyzed the variation of tip clearance with the method of cyclic symmetry analysis when engine works under the conditions of temperature and rotational speed, am using a new method to deal with thermal contact resistance in the calculation

    本文完善了計算葉尖間隙的簡化演算法程序,增加了程序的計算功能,並將其應用於某高壓渦輪進行葉尖間隙分析,所得結果與理論結果進行了對比,得出修改後的程序用於葉尖間隙計算是合理的;同時提出了與葉尖間隙相關的典型部件的冷、熱態的尺寸兩種換算方法,使用優化設計的方法進行了實例分析,說明了所提出的計算方法是可行的;最後應用ansys有限元軟體利用循環對稱的方法分析了某型發動機高壓渦輪在溫度場及離心力作用下的葉尖間隙在發動機工作過程中變化情況,並分析了計算中的接觸熱阻的處理問題。
  16. Turpa - a series of highly refined base oils which possess wccellent demulsibility, anti - foad and air release properties. containing antioxidant and anti - rust additives to impart high resistance to oxidation ant high temperature and to acid formation. turpa is specially recommended for steam, gas and water turbine, turpa fufills the most severe operating conditions imposed by modern heavy duty gas turbine as other general applications, such as vacuum pump, air compressor and hydraulic system, where the qualities of turbine oil are required

    德霸-度精煉礦物油,具備了優良的抗乳化性、抗泡性及空氣釋放性,配合抗氧化劑及防銹劑,在溫時不易氧化及產生酸性,推薦應用於蒸汽、烯氣及水機,德霸能滿足新式燃氣機的嚴苛操作環境,也能應用於需要一般透平機油特性的操作,如真空泵、空氣縮機及液系統等。
  17. To investigate the aerodynamic design ideas and concrete methods of high performance low pressure turbine ( lpt ) at low reynolds number condition, a new lpt of high load, large chord and proper velocity distribution was designed

    摘要為了探索空低雷諾數情況下性能低部件的氣動設計思路和設計方法,通過採用負荷、大弦長的葉片設計和選擇恰當的葉片表面速度分佈形式設計了一臺新低
  18. A simplify high pressure turbine ( hpt ) tip clearance model is analyzed with the cyclic symmetry method. research on the flow, heat and structure integration analyses is achieved in this paper. flow / heat analysis is done by fluent software, and heat / structure analysis is done by ansys software

    針對部件的結構特點,進行了適當的簡化,利用參數化設計思想建立了葉尖間隙計算模型,用循環對稱的方法分析了某型發動機高壓渦輪葉尖間隙在工作過程中變化的情況。
  19. The results of 3d viscous numerical simulation show that the efficiency of new lpt decreases 2. 3 percent under the low reynolds number condition, which was compared with that of design point

    三維粘性數值模擬的結果顯示新低效率在空低雷諾數情況下比設計點下降2 . 3個百分點。
  20. The main work of this paper is the heat transfer experiment in rotating cavity of an advanced aero - engine of rrd company

    本文工作圍繞rrd公司某型先進發動機高壓渦輪盤腔內換熱實驗進行。
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