航空燃氣渦輪 的英文怎麼說

中文拼音 [hángkōngránqìguōlún]
航空燃氣渦輪 英文
aerogas turbine
  • 航 : Ⅰ名詞（船） boat; shipⅡ動詞（航行） navigate （by water or air）; sail
  • 空 : 空Ⅰ形容詞（不包含什麼; 裏面沒有東西或沒有內容; 不切實際的） empty; hollow; void Ⅱ名詞1 （天空） s...
  • 燃 : 動詞1. （燃燒） burn 2. （引火點著） ignite; light
  • 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 : 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...
  • 航空 : aviation; voyage
  • 燃氣 : gas燃氣發電廠 gas power plant; 燃氣鍋爐 gas fired-boiler
  • 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. Test method for the determination of the aromatic content and polynuclear of diesel fuels and aviation turbine fuels by supercritical fluid chromatography

    超臨界流體色譜法測定柴油燃料和航空燃氣渦輪燃料中芳香烴含量和多核芳香烴的試驗方法
  2. Gte spares no effort in self - innovation with basis on work force, operates in a factual and realistic way to achieve a rapid, comprehensive and sustainable development in aeronautical research, non - aero product and service industry

    中國燃氣渦輪研究院堅持以人為本、自主創新、求真務實，航空科研、非航空產品開發和第三產業正全面、健康、協調發展。
  3. 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
  4. Jftot test method for thermal oxidation stability of aviation turbine fuels jftot procedure

    航空燃氣渦輪機燃料熱氧化穩定性的試驗方法
  5. 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。
  6. And the finite element method ( fem ) was used to simulate the stress and deformation of the outer casing and the bearing chock. on the basis of the experiments and fem analysis, the strength and fatigue lifetime, the interaction of creep and fatigue lifetime, the creep lifetime of outer casing and bearing chock have been analyzed, at the end of trail, sem analyses of failure section has been conducted

    同時對航空發動機燃氣渦輪外機匣和軸承座進行了有限元模擬計算，得到外機匣和軸承座的焊接處的強度和變形情況的模擬結果。根據試驗數據和有限元的計算結果，對發動機燃燒室外機匣和軸承座兩種結構（包含焊縫）進行靜強度分析、疲勞壽命分析、蠕變壽命分析、蠕變疲勞交互作用壽命分析以及斷口的金相分析。
  7. 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。
  8. The work of this thesis is financially supported by the aero fund project. the main purpose is to study the aerodynamics design technology of counter - turbine, to find the question differing from the aerodynamics design of general turbine, and to provide theoretical basis for development of aeroengine. first, the design method for the counter - turbine meridional flow is developed in the present thesis, and one 1 + 1 type counter - turbine is designed using this method

    本論文的工作來源於航空科學基金項目，主要是研究對轉渦輪的氣動設計方法，並通過對對轉渦輪的氣動設計與分析，搞清對轉渦輪設計的關鍵問題、發現區別于常規渦輪設計的特殊性，為今後先進軍用戰斗機發動機燃氣渦輪設計與研製奠定理論基礎。
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