渦輪發動機 的英文怎麼說

中文拼音 [guōlúnfādòngjī]
渦輪發動機 英文
cropped-fan engine
  • 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...
  • 發 : 名詞（頭發） hair
  • 機 : machineengine
  • 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.

    渦輪發動機有一個高度旋轉的壓氣機。
  2. 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。
  3. Greep resisting nickel and iron base alloys have been linked inexorably with the development of gas turbines.

    燃氣渦輪發動機的發展同抗蠕變鎳基和鐵基合金的發展緊密聯系在一起。
  4. The turboprop engine is very much like the turbojet.

    渦輪螺槳發動機與渦輪發動機十分相似。
  5. Standard specification for aviation turbine fuels

    航空渦輪發動機燃料的標準規范
  6. Designs and manufactures turbine engine test cells and wind tunnels

    設計生產渦輪發動機測試單元和風洞。
  7. Standard test method for peroxide number of aviation turbine fuels

    測定航空燃氣渦輪發動機用燃料過氧化值的試驗方法
  8. The company manufactures a range of components for aerospace gas turbine engines

    公司生產燃氣渦輪發動機的系列部件。
  9. Valve, starter control, pneumatic, aircraft engine general specification for

    飛機燃氣渦輪發動機空氣起動機控制活門通用規范
  10. Based on detailed analyze on turbine engine and ramjet, a new conceptive internal - rotor burnt rotating ramjet ( irbrr ) with an rotating cylinder in the center of rotor in which the revolved stream can be ram - compressed and burnt has been proposed and some primary research have been done as below : the scheme of structure, principles, thermodynamic cycle and performances of the new conceptive engine has been studied in the paper

    本文通過對燃氣渦輪發動機和航空沖壓發動機的原理結構進行詳細分析並進行融合創新，提出了一種利用內置旋轉汽缸進行旋轉氣流沖壓壓縮和旋流燃燒的新概念內置燃燒室旋轉沖壓發動機，並進行了一些前期的基礎性探索研究，具體研究內容有:對旋轉沖壓發動機進行了總體方案設計、工作原理分析、氣動熱力循環和性能分析等概念性研究。
  11. 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。
  12. In order to execute this research, the experimental equipment that can fulfill the requirements of the regions of reynolds numbers in mte was built. two new measurement techniques, mini - size static pressure hole and mini - type pressure probe were presented

    本文針對微型渦輪發動機流動問題研究的需要，發展了壁面微靜壓孔和微型單管總壓探針測量技術。
  13. 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。
  14. Standard test method for corrosiveness and oxidation qualility of hydraulic oils, aircraft turbine engine lubricants, and other highly refined oils

    液壓油飛機渦輪發動機潤滑油和其他高精煉油的腐蝕性和氧化穩定性的試驗方法
  15. An increase in the specific work and cycle efficiency of gas turbines can be achieved through higher turbine entry temperatures. maintaining adequate life at these high temperatures requires the development of materials and efficient cooling methods

    提高渦輪發動機效率的重要途徑是提高其入口溫度，而高溫下渦輪發動機的壽命取決于相關零部件的材料特性和冷卻方法的效率。
  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. In simulation theory terms, torpedo turbine engine system is a complicated system. especially at non - design condition, the works of matching and controlling inner parameters of system is more difficult

    魚雷渦輪發動機屬于復雜系統，特別是變工況條件下，系統各參數的匹配與控制則更為復雜。
  18. This paper is based on the theory of engineering thermodynamics. the research object is unclosed - cycle - form partial - flow two - stage impulse torpedo turbine. first we study the design condition of torpedo turbine

    本文以工程熱力學為理論基礎，以魚雷開式循環部分進氣純沖動式復速級渦輪發動機為研究對象。
  19. Ge aircraft engines is a world leader in the design, manufacture and servicing of gas turbine engines

    Ge飛機發動機集團在燃氣渦輪發動機的設計、生產及維修方面處於世界領先地位。
  20. The characteristics of flow in mini - channels at low reynolds numbers are one of the essential components for the design of mte ( micro turbine engine )

    微小通道內低雷諾數流動特性研究是微型渦輪發動機基礎技術研究的重要組成部分。
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