靜葉片 的英文怎麼說

中文拼音 [jìngpiān]
靜葉片 英文
fixed-blade
  • : Ⅰ形容詞1. (安定不動; 平靜) still; calm; motionless 2. (沒有聲響; 清靜) silent; quiet Ⅱ名詞(姓氏) a surname
  • : 片構詞成分。
  1. There was a ridge of ploughed land, with a plough upon it where it had been left last night when the horses were unyoked ; beyond, a quiet coppice - wood, in which many leaves of burning red and golden yellow still remained upon the trees

    窗外有一條翻耕過的地畦,上面有一部昨夜除去馬軛后留下的鏵犁。遠處是一的雜樹叢,還殘留著許多火紅的和金黃的樹
  2. And when the hurly - burly of daytime is overcastted by darkness of night with solitude, i am sometimes at a loss in dim lamplight till i clap eyes on this old maple leaf which puts me into my role as bending over the desk quietly to read, write or ponder

    謐的夜覆蓋了白晝的喧囂,在昏黃燈火下的我有時會不知所措,直到看見這歷經歲月滄桑的楓,才的伏在桌上,或讀,或寫,或思,進入了角色。
  3. Abstract : the main features, the key points of design, material selection and test method of international metal and ceramic hybrid type multilayer stator vane are reviewed in this paper

    文摘:評述了國外金屬和陶瓷多層混合式的主要特點、設計要點、材料選擇和試驗方法。
  4. 4 ) in a pre - swirl rotator - stator cavities with discrete pre - swirl nozzles and blade - cooling entry holes, the influences of pre - swirl angle and flow parameter on the flow and heat transfer characteristics were numerically investigated. the correlation for average nusselt number vs rotating reynold number or non - dimensional mass flowrate were established. the results show that : advantage of per - swirl inflow is the effect of cooling the blade - cooling entry holes ; pre - swirl inflow increases heat transfer in rotating disk of pre - swirl chamber ; as pre - swirl angle increases, local nusselt number decreases in pre - swirl chamber ; the temperature of stator of inner rotator - stator chamber and per - swirl chamber decreases as rotating reynold number increases ; when the axial mass flowrate maintains constant, heat transfer in the rotating disk of inner rotator - stator cavities does n ' t change as per - swirl mass flowrate increases, while heat transfer in the rotating disk of per - swirl chamber increases ; when the pre - swirl mass flowrate maintains constant, change of the axial mass flowrate has effect on the whole cavity

    結果表明,預旋進氣的優點在於增強了冷卻孔附近的對流換熱效果,局部努謝爾數隨預旋角的增大而有所減小;隨旋轉雷諾數的增加,不論是內轉腔室還是預旋腔室的盤上的溫度都不同程度的降低:當軸向中心進氣質量流量不變時,隨預旋進氣的質量流量增加,內轉腔室的轉盤盤面上的換熱基本沒有變化,而預旋腔室的轉盤盤面上的換熱效果增強;當預旋進氣質量流量不變時,軸向中心進氣的質量流量的改變對整個盤腔都有影響。
  5. 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。
  6. In order to investigate the unsteady flow frequency domain performances of an axial flow compressor at different mass flow, rotating speed and blade row spacing, plus inlet flow distortion, and considering aerodynamic characteristics and stability of the compressor, the low speed research compressor ( lsc ) at college of energy and power in nuaa is used to carry out the experiment studies. a large amount of test data has been gained through dynamic pressure transducers embedded in the stator blades at the tip, middle and hub section, then fast fourier transform algorithm ( fft ) is applied to calculate the frequency data

    為探討軸流壓氣機在工作流量、工作轉速及動?排軸向間距變化時的排流場非定常頻譜特性變化規律,並耦合進氣畸變的影響,同時與壓氣機氣動性能和氣動穩定性相關聯,作者利用南京航空航天大學能源與動力學院的低速大尺寸軸流壓氣機( lsc )試驗器,採取在表面埋入動態壓力傳感器的實驗方法,對尖、中和根三個截面的動態壓力進行了測量,獲得了大量的可靠的實驗數據。
  7. The result indicates that the maximum stress on the runner is mainly in proportion to the turbine output

    結果表明在大部分工況下該轉輪最大應力基本上與水輪機功率成線性關系。
  8. Abstract : by using the self - regulating electrostatic drying equipment, theelectrostatic drying for plant leaves is studied. the equipment is a surface silent discharge ozone generator. the electrostatic drying and natural drying are compared experimentally. the result shows that the electrostatic field is more effective for plant drying. the polarity characteristics of the electrostatic drying is discovered during the experiment and discussed. for accelerating drying, the polarity characteristics should be considered in the drying equipment design

    文摘:在自製的沿面式無聲放電臭氧發生裝置上,對植物進行了乾燥實驗.通過對植物電乾燥和自然乾燥的比較,證實電場對植物有明顯的乾燥效果.發現了電乾燥中的極性效應,即當管狀電極的極性為負時,乾燥速度較快.對極性效應進行了探討和分析.實驗結果表明:沿面式無聲放電臭氧發生裝置可以有效地對植物進行電乾燥.研究結果對有效地利用電乾燥和極性效應來合理設計電乾燥裝置的結構具有重要意義
  9. The steam path of the steam turbine through which steam flows consists of nozzles, and the moving blade, fixed blade and other auxiliary equipment

    汽輪機的通流部分即蒸汽流過並做功的部分,其中包括噴嘴,隔板以及動、靜葉片以及相應的汽封裝置。
  10. The propose of this project is to develop a three - dimensional, compressible navier - stokes solver for detailed study the flow inside transonic turbine and compressor ' s stator in the airplane turbomachinery

    摘要本研究的目的在發展一系列飛機滑輪引擎之的計算流體力學方法與程式,計算程式方面包括三維格點的建立與黏性流程式開發及撰寫等,程式發展完成後將進行一系列外形及氣流條件計算模擬。
  11. The compressor exists about 0. 265 rotor blade converted frequency near stall point, its intensity increases with rising of rotating speed and reducing blade row spacing. the blade row spacing would exert influences on rotor - stator interaction, stability and stall mode

    在臨近失速點處,不同工作轉速、不同動?排軸向間距均存在約為0 . 265轉子摺合頻率的特徵頻率擾動,強度隨轉速的上升和軸向間距的減少而增大。
  12. This paper uses the theory of design on parameters to achieve the software package of bss and the stator vane ’ s vibration and fatigue analysis software, which realize the process of stator vane ’ s vibration and fatigue use a key to control

    本文還採用了參數化的設計思想開發了盲源分離的軟體包。同時課題期間還開發了振動與疲勞分析平臺軟體,實現了整個振動、疲勞特性分析的過程的「一鍵控制」 。
  13. To meet the needs for wider surge margin of the turbofan engine, a new model was developed to predict the characteristics of the fan / high pressure compressor and turbine in this thesis. several ways, including, variable inlet guide vanes of the fan, variable guide vanes of the high pressure compressor, the variable inlet area ratio of the mixer and the nozzle areas, were presented to enlarge the surge margin of the turbofan engine. meanwhile, a method of combined variable geometries for optimizing controls of inlet guide vanes of the fan, guide vanes and the first two stators of high pressure compressor, area ratio of mixer and noz zle areas was established

    為了滿足下一代作戰飛機對推進系統的性能和穩定性要求,本文建立了壓縮系統特性和渦輪特性的新模型,並分別採用改變渦扇發動機風扇進口導流、壓氣機導流和前兩級靜葉片、混合室進口處內、外涵面積比和尾噴管面積,研究了其對發動機性能和穩定性的影響,進而得出了渦扇發動機變幾何擴穩的方法,為發動機變幾何擴穩研究打下理論基礎。
  14. The software can show the surface and section ' s graph of contour and color contour, the static and dynamic graph of displacement, and so on

    本文開發的軟體能夠實現表面及截面的等值線圖和雲圖的繪制、態變形和動畫等功能。
  15. The outlet flowfield and static pressure on blade surfaces of the classical turbine stator cascades with straight and - 10 、 - 20 bowed blades were measured in the linear cascade wind tunnel

    摘要在平面透平柵風洞中,測量了一種典型透平型直柵和彎曲角分別為- 10 、 - 20的反彎曲柵的出口流場和表面壓。
  16. In order to eliminate the brittle fracture of the stator blade, using the orthogonal experiment, the brittle problem of the stator blade was studied

    為了消除靜葉片的脆性斷裂,採用正交試驗對脆性問題進行了研究。
  17. Coupled with the curved heat exchanger, the york cooling king is also designed to operate at the lowest noise level - 29dba at low speed fan

    結合彎曲的熱氣轉換器, york cooling king的噪音也是最低的只有29dba 。它具備安操作和寬敞空氣擴散系統的低噪音風扇
  18. Abstract : large horizontal axis wind turbine ( hawt ) runs in complicated environment, the load it endured is also very complicated. as the wind turbine become larger and because of the usage of the flexible tower and the glass fiber blade in hwat, the static and the dynamic problems of the hwat and it ' s component become more and more important

    大型水平軸風力發電機組運行在復雜的自然環境中,所受載荷情況非常復雜,而且隨著風力機組的大型化發展,柔性塔架的出現、玻璃鋼的應用,使得風力機及其零部件的動態問題更加突出。
  19. Measured hole mass flows and a constant static pressure mixing analysis, together with the measured losses, allowed the decomposition of the losses into three distinct entropy generation mechanisms : loss generation within the hole, loss generation due to the mixing of the coolant with the mainstream, and change in secondary loss generation in the " blade passage

    論文還進行了冷卻孔質量流的測量與常壓氣流混合分析,結合前述氣動力損失和冷卻空氣損耗的測量結果表明,端壁氣膜冷卻的綜合損失明顯地由三個部分組成:冷卻孔內產生的損失;由於冷卻空氣與主流熱空氣的混合產生的損失;二次流的變化產生的損失。
  20. The radial, circumferential and axial distributions of static pressure amplitude under post - stall conditions are measured and compared. the experimental results have proved the feasibility of using one - dimensional model to analyze the post - stall behavior and recoverability of compression systems. at the same time, the results of experiment have provided the first - hand data for analyzing and calculating vibrating response of blades under post - stall conditions

    以單級軸流壓氣機實驗器為對象,研製了兩種型式的壓動態探針?梳形針和圓盤針,詳細測量了過失速狀態下流道中壓力沿徑向、周向和軸向分佈,驗證了用一維模型分析壓氣機過失速性能和失速可恢復性的可信度,同時為過失速狀態下的振動響應分析計算提供了第一手實驗數據。
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