高壓壓氣機 的英文怎麼說

中文拼音 [gāoyāyāqìjī]
高壓壓氣機 英文
high pressure compressor
  • 高 : 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 : 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...
  • 機 : machineengine
  1. High - pressure airless spraying machine

    高壓無氣噴塗機
  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. High pressure air for homogenizing is supplied by roots blower under homogenizing silo

    均化所用高壓空氣由庫底羅茨風機提供。
  4. 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。
  5. New and improved nickle - base, iron - nickle - cobalt - base superalloys were available for use in high - pressure turbine airfoils in aircraft gas turbines

    新改進的鎳基、鐵鎳鈷基超耐熱合金可用在飛機燃氣輪中的高壓透平機翼上。
  6. High pressure air is brought through the strut and simulates the engine air flow.

    高壓空氣通過支板引入並模擬了發動機的氣流。
  7. Exploring mechanism of stall margin enhancement of subsonic axial - flow compressor through steady micro tip injection

    定常微量噴氣提高軸流壓氣機穩定工作裕度機理探討
  8. 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。
  9. Compress disk is the very important rotational component in the areoengine. when the compress disk is working, the grads of temperature and stress between the rim and the center of the disk are great. in order to raise the thrust - weight ratio of the disk and reduce oil consumption. the best prospective way is the dual alloys disk used

    壓氣機盤是航空發動機上一個很重要的轉動部件，壓氣機盤工作時，輪緣和輪轂溫度梯度和應力梯度較大，為了提高飛機發動機推重比、減低耗油量，要求壓氣機盤的工作溫度、使用性能更高，雙合金盤製造是最有發展前景的技術。
  10. Particles are captured on filter surface ; the frequency of the filter is controlled by a timer. cleaning is done by shaking particles off the filter bag surface, which is enabled by injection of high - pressure air into the funnel. dusts are collected into the barrel underneath for regular removal

    來控制清潔濾袋的頻率，清潔方式為把高壓空氣噴入濾袋中，將濾袋表面的粉塵震落至集塵機灰斗內，再收集至灰斗下方的收集桶並定時清除。
  11. 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。
  12. Medical electrical equipment - particular requirements for safety - specification for high voltage generators of diagnostic x - ray generators

    醫用電氣設備.安全性專門要求. x射線診斷裝置的高壓發電機規范
  13. Abstract : the hot spinnig process of forming high pressure c ylinder which using home - made numerical control machine, is introduced. this proc ess has the advantage of the higher material utilization and production officien cy

    文摘:介紹用國產數控機床加工高壓貯氣瓶的熱旋壓成形新工藝，對國內氣瓶生產提出了1種具有較高材料利用率，較高生產效率的數控化加工方法。
  14. Numerical investigation to small high speed centrifugal compressor

    小型高速離心壓氣機級內部的三維流場分析
  15. 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。
  16. This new technology changes from the traditional method by which the induced and compressor wheel separately are designed and produced to a new one by which the one - piece compressor is designed. on the basis of this new technology and the optimum blade profile, the performance of both the compressor and the turbocharger is largely improved. through the heating power calculation of the compressor, the analysis of the surge and the block of the compressor, the test - bed performance test of the turbocharger, the matching test of turbocharger and diesel engine, the propulsion test of the turbocharger on plateau condition, it is proved that the newly - designed compressor not only has high efficiency, but also improves the flow distribution in the high efficiency area so that the propulsion line can run through the high efficiency area

    主要內容包括：提出一種全新的壓氣機葉輪技術和概念，這種技術將傳統的導風輪和壓氣機分開設計、單獨加工改為整體設計、整體加工的單體葉輪；從增壓器與柴油機配機計算所得出的基本參數出發，通過對壓氣機進行熱力計算，確定壓氣機的基本結構參數；再對葉型以及葉輪輪廓與葉輪罩殼的配合間隙進行優化，對新設計的壓氣機進行喘振和堵塞分析；通過增壓器平臺性能試驗，驗證了新設計的壓氣機的性能水平得到了較大的提高，達到了提高增壓器的整體性能水平的目的；通過增壓器與柴油機配機試驗、以及增壓器用於高原條件下的牽引試驗，驗證了新設計的壓氣機不但具有高效率，還改善了高效率區的流量分佈，使牽引特性線貫穿高效率區。
  17. This system uses dispersion inertial impact, shielding, and gravity to achieve dust capturing. this filter facility employs high - pressure air to continuously flush out particles without halting up operation, offering high stability and screening efficiency

    利用擴散慣性沖擊、遮攔及重力等作用，達到粉塵捕集效果，本集塵機使用高壓空氣，連續式高壓空氣逆洗，粉塵震落時不須停機，性能穩定，集塵效率高。
  18. The outcome of theory and experiment proved that spraying water on the inlet of supercharger can improve the working condition ( reduce the thermal loads ), extend operation period and enhance the reliability of diesel engine

    理論分析和實驗結果都證明了：在壓氣機進口噴水，可以改善增壓柴油機的工作條件，減少油耗率，提高有效效率。
  19. The advanced turbocharger makes air - compressing efficiency upto 80 per cent

    採用高性能增壓器，便壓氣機效率達到80 %以上。
  20. The high - temperature properties of ti3al matrix alloy can satisfy the request of the exit temperature of the areoengine compress. but the room temperature plasticity of ti3al matrix alloy is very low, hard to shape, and manufacture ' s cost is very expensive

    Ti _ 3al基合金高的高溫性能可以滿足飛機發動機壓氣機出口溫度的要求，但由於ti _ 3al基合金室溫塑性差，成形困難，製造成本高；而tc11兩相鈦合金可以在500以下溫度長時間工作，用於壓氣機盤已比較成熟。
分享友人
分享到 Line

分享到臉書