風葉傳動輪 的英文怎麼說

中文拼音 [fēngzhuàndònglún]
風葉傳動輪 英文
fly driving wheel
  • : Ⅰ名詞1 (空氣流動) wind 2 (風氣; 風俗) practice; atmosphere; custom 3 (景象) scene; view 4 ...
  • : 傳名詞1 (解釋經文的著作) commentaries on classics 2 (傳記) biography 3 (敘述歷史故事的作品)...
  • : Ⅰ名1 (輪子) wheel 2 (像輪子的東西) wheel like object; ring; disc 3 (輪船) steamer; steamboa...
  1. It specializes in producing yy h series 0. 160000kg hard or soft bearing balancing machines and special horizontal or stand balancing machine for automobile motorcycle, crank shaft, transmission shaft, tyre, aircondition, etc. also, we are the sole company in china that can design, produce and sale high speed testing machine of 0 - 65000rpm

    經營通用型0 . 160000公斤yy h系列軟硬支承平衡機及特殊型汽車摩托車曲軸胎空調器上慣流軸流等專用臥式立式平衡機的專業公司。
  2. This thesis gives a brief introduction to basic theory of wind power, construction of wind farm and commissioning and operation of wind turbine by illustrating the 3rd phase extension project of ningxia electric power group co., ltd helanshan wind fram. based on the specific study on the engineering construction and the domestically and globally popular 850kw wtg, further by comparasion of the power output rate of g52 and g58, we can prove that with substitute of new material and new technology, larger capacity wtg will become popular. especially when the running diameter of blades enlarged, more power produced at same wind speed ; and the high efficiency will be further guaranteed if the gearbox, major shafting equipment be checked and maintained regularly

    根據對實際工程建設的具體研究,對我國及國際上主導機型850kw機的具體分析,以及對g52和g58機輸出功率的比較,更進一步證明在新的技術和材料替代下,更大型的力發電機組將會替代現有主導機機型,特別是在直徑增大后,相應的輸出功率在同等速下會有明顯增加,更好的利用能並轉變為電能;齒箱作為機中主要設備,只有按維護要求並根據實踐經驗定期檢查易損部件,才能使機安全高效的運行,提高機的經濟運營效率。
  3. Film cooling of the surface of a gas turbine blade was studied in a large - scale low - speed opening wind tunnel according to actual requirement of the design of aero - engine. the surface of a gas turbine blade was cooled by cylindrical holes in the experiment, with the hole number of fifteen in stator and eight in rotor

    應航空發機設計的要求,在大尺寸低速洞中分別對發機渦導向片和表面的氣膜冷卻特性進行了研究,具體研究在不同氣膜孔出流時,在不同主流雷諾數和吹比情況下片表面局部換熱系數的分佈規律。
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