axial compressor 中文意思是什麼

axial compressor 解釋
軸流式壓縮機
  • axial : adj. 1. 軸的。2. 成軸的。3. 軸周圍的，軸向的。adv. -ly 在軸的方向，與軸平行地。
  • compressor : n. 1. 壓縮物。2. 壓縮器，壓氣機，壓榨器。3. 【解剖學】收縮肌，壓肌。
  1. 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
  2. Thermodynamic performance test for centrifugal axial blower and compressor

    離心和軸流式鼓風機和壓縮機熱力性能試驗
  3. 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?靜葉排軸向間距變化時的葉片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，採取在靜子葉片表面埋入動態壓力傳感器的實驗方法，對葉尖、葉中和葉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。
  4. The effect of leakage flow due to the upstream hub axial gap on the rotor performance and the mechanism of interaction between the hub leakage flow and the rotor blade passage flow were studied based on the numerical simulations of the flow fields of a transonic compressor rotor with upstream hub leakage

    摘要為研究壓氣機轉子上游葉根軸向間隙泄漏流對轉子性能的影響程度以及泄漏流與轉子流場之間的相互作用機制，對帶有葉根泄漏流的跨聲壓氣機轉子流場進行了數值模擬。
  5. Axial flow type air compressor

    軸流式空氣壓縮機
  6. Experimental study of small perturbation induced rotating stall in axial flow compressor

    軸流壓氣機小擾動誘發旋轉失速的試驗研究
  7. Experimental and numerical investigation of stepped tip gap effects on an axial - flow compressor

    梯狀間隙結構對軸流壓氣機影響的試驗與數值模擬
  8. Experimental research of an axial flow compressor performance with stepped tip gap casing configuration

    梯狀尖部間隙機匣處理對軸流壓氣機性能影響的實驗研究
  9. The effect of tip injection on the performance of an axial - flow compressor was performed numerically

    採用數值模擬方法研究了頂部噴氣對某軸流壓氣機氣動性能的影響。
  10. Exploring attenuation of steady circumferential pressure distortion of axial flow compressor with axial fan stage

    風扇級負荷對其進口總壓畸變響應特性影響研究
  11. Nonlinear bifurcation analysis on post - stall transients of axial - flow compressor

    軸流壓縮系統過失速行為的非線性分叉分析
  12. In this paper, the performance of a multi - spool axial - flow compressor with a fan during operation with water ingestion is investigated

    本文主要研究了多級軸流風扇壓氣機在有水或者其它液相注入時的性能特性。
  13. With the method, the calculation of arbitrary stage characteristics is carried out. in order to verify the method, a example of a 2 - spool, 16 - stages axial - flow fan / compressor is used for characteristics

    文中對一臺多級軸流風扇壓氣機在各種工況下進行詳細的性能特性計算，並對計算結果進行了分析，以驗證方法的可行性。
  14. The experimental results show that the unsteady flow frequency domain performances of the axial flow compressor will be varied with mass flow, rotating speed, blade row spacing and inlet distortion

    實驗結果表明，工作流量、工作轉速、動?靜葉排軸向間距以及進氣畸變均對壓氣機的非定常頻譜特性產生影響。
  15. The multi - stage axial compressor performance was measured using a streamline curvature method based on two - dimension ( axisymmetric ) mathematical model

    摘要採用二維（軸對稱）數學模型，應用流線曲率法求解多級軸流壓氣機特性。
  16. By comparing the calculated results and test data for a multi - stage axial compressor, this method demonstrates that it could assist in predicting the characteristics of multistage axial compressor and spanwise parameter distribution under off design working conditions

    對一臺多級軸流壓氣機的計算結果與試驗數據的對比分析表明，該方法能較好地預測多級軸流壓氣機的特性和非設計工況下級間參數的分佈。
  17. The effects of layout of tip gap clearance on axial compressor rotor performance and stability have been investigated experimentally. a single - stage compressor rotor with no inlet guide vanes was tested under subsonic condition

    本文用實驗的方法對壓氣機轉子尖部間隙沿軸向周向的布局進行了詳細的研究。
  18. The influence of tip clearance on overall performance and detailed flow structure in tip region of an axial compressor rotor was investigated

    研究了頂部間隙對壓氣機轉子總性能及內部流場的影響。
  19. The unsteady surface pressures on the rotor blades of a single - stage low - speed axial compressor were measured by means of mounting micro - sensors on the surface the blades

    摘要為了研究上游葉片尾跡對軸流壓氣機轉子葉片非定常表面壓力的影響，採用在葉片表面埋設微型壓力傳感器的方法，測量了一個單級低速軸流壓氣機轉子葉片的非定常壓力分佈。
  20. By using a reynolds - averaged two - dimensional computation, the effect of upstream wake on unsteady separated flow field of downstream adjacent vanes was investigated in low - speed axial compressor

    摘要利用二維數值模擬研究了低速軸流壓氣機上游尾跡對下游相鄰葉排的非定常分離流場的影響。
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