rotor compressor 中文意思是什麼

rotor compressor 解釋
轉子壓縮機
  • rotor : n 1 【電機】轉子 〈cf stator〉; 動片，轉片。2 【航空】水平旋翼。3 【物理學】旋度。4 （風筒船的）...
  • 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. The results of the experiment show that the synthesized index, unsteady index and steady index inflect the stability margin of the compressor well. and show that the insert - board experiment can get the enough weight in the synthesized index. and also show that the low - press - area of the steady total - press moves along the rotor circumvolving direction

    試驗結果表明，綜合畸變指數，動態畸變指數，穩態畸變指數對壓氣機穩定性有很大作用;同時試驗還表明，插板能夠產生較大的動態畸變指數分量;穩態壓力圖譜低壓區隨著轉子轉動方向轉動;以及其他一些有益的結果。
  2. The calculation of the37 # transonic compressor rotor shows that the simulation results of the author ' s multi - grid scheme fit fairly well with those of professor denton j. d. ' s, however, the author ' s converging speed is faster

    與nasarotor37的計算結果對比表明，本文多重網格演算法的計算結果與dentonj . d .的計算結果十分接近，而在提高計算效率方面比dentonj . d的多重網格演算法更加有效。
  3. 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。
  4. The flow field in the rotor tip of a compressor was numerical analyzed using the calculation method, the result compare well with experimental data

    對某壓氣機轉子項部間隙內的流動進行了詳細的數值模擬，計算結果與試驗結果吻合良好。
  5. Turbo - compressor rotor

    渦輪壓縮機轉子
  6. Epstein ' s microengine only has two parts : a moveable rotor and a stationary structure that together function as the compressor and combustor

    愛匹斯丁的微型引擎只有兩個部分：一個可轉動的的轉子和一個固定的腔室，它們共同成為壓縮機和燃燒機。
  7. 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?靜葉排軸向間距均存在約為0 . 265轉子葉片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。
  8. Abstract : a 3d numerical solution of transonic turbulent flowfield inside a compressor rotor is analyzed with a consideration of blade tip clearance

    文摘:藉助于考慮葉片頂部間隙的壓氣機轉子內跨音速湍流流場的三維數值解，得到了該轉子流場中的復雜渦系與波系結構。
  9. To meet the need of developing the simulator of the whole flow sheet of the mathematical plant, mathematical model and simulation software of the plant is developed. in the process of modeling, thermotical character and mechanical character of centrifugal compressor are emphased. thermotical character is about section parameters and character curves ; mechanical character is about rotor ' s vibration and axial force

    在建模過程中，重點對離心式壓縮機的熱力特性和機械特性做了較深入的研究，其中熱力特性著重於離心式壓縮機中的氣流在各個關鍵截面參數和特性曲線，機械特性著重於壓縮機轉子軸系的振動和軸向力。
  10. Amelioration of automobile detection system of rotor of the air conditioning ' s compressor

    汽車空調壓縮機轉子檢測系統校準方法的改進
  11. Then the effects of the grooved casing treatments on the performance of the compressor rotor have been revealed and some valuable conclusions have been reasoned out

    通過對總性能和基元性能，特別是葉片尖部流動的詳細測量，證明了這種型式的處理機匣可以提高效率，但在穩定裕度上略有損失，並解釋了其影響轉子性能的機理。
  12. The basic p0arameters and sizes of the rotor of screw compressor and timing gear

    螺桿壓縮機轉子和同步齒輪基本參數及尺寸
  13. 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。
  14. Eccentric rotor sliding vane compressor

    偏心轉子滑葉壓縮機
  15. In the compressor construction design, it makes a all - around description and design for the geometry of the compressor ' s every part such as suction and discharge ports etc, the dynamic features such as rotor stress etc, bearing ' s selection, strength check and so on

    在壓縮機結構設計方面，對壓縮機吸、排氣口等各項幾何結構，轉子受力動力特性，軸承選取，強度校核等進行了全面論述和設計。
  16. It was found that the introduce of tip clearance deteriorate the overall performance of the compressor rotor

    數值結果表明葉頂間隙的引入惡化了壓氣機轉子的性能。
  17. 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。
  18. 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。
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