engine geometry 中文意思是什麼

engine geometry 解釋
發動機幾何學
  • engine : n. 1. 機械，機器。2. 引擎，蒸汽機，發動機。3. 機車，車頭。4. 工具；〈古語〉方法，手段。vt. 給…安裝發動機。
  • geometry : n. 1. 幾何學。2. 幾何形狀。3. 幾何學著作。
  1. By adjusting many variable geometry components of the engine, bypass ratio can be changed during large range ( the most 0. 25 of military fighter ). the high specific thrust characteristic of turbojet engine and the low specific fuel consumption characteristic of the turbofan engine can be realized during different flight phase by the usage of vce technology

    變幾何變循環發動機是應用於第四代多用途戰斗機的理想動力裝置，通過多個部件幾何的調節在較大范圍內改變涵道比，能夠使發動機在不同航段分別實現渦噴發動機的高單位推力性能和渦扇發動機的低油耗性能。
  2. Finally, the inlet port and combustion chamber designed and machined is tested on 4100qb. the paper mostly investigates the change of performance targets of the engine that three different grooved chambers including two different re - entrant model and one w model match with various intake port and nozzles, in order to realize the influence of chamber geometry on combustion process. the results analyzed have indicated that re - entrant grooved chambers can enhance the turbulent intension in the chamber, improve the combustion proces of diesel engine on the altiplano, being groove, re - entrant and convex, and have the farther developing potential

    著重研究兩種縮口、一種直口矩形環槽燃燒室與不同進氣道、噴油嘴的組合方案發動機的動力性、經濟性及排放指標的變化，確定燃燒室的幾何形狀對燃燒過程的影響。分析結果表明，由於有矩形環槽、燃燒室縮口以及燃燒室底部凸臺，縮口矩形環槽燃燒室中的紊流得以加強，改善了高原柴油機的燃燒過程，這種燃燒室有進一步發展的潛力。
  3. And those characteristics of compressor and turbine are put into the steady - state design and off - design performance program of augmented turbofan engine, to calculate the influence of the geometry changing of single component on the performance of engine

    計算了單個可變幾何部件的調節（包括高壓壓氣機、高壓渦輪、低壓渦輪、混合器進口面積比和噴管喉道面積）對發動機穩態性能的影響。
  4. These variable geometry components include high pressure - compressor, high - pressure turbine, low - pressure turbine, inlet area ratio of mixer and main nozzle throat area. the results of calculation show that the adjusting of low - pressure turbine and mixer has a remarkable effect on the performance of engine and bypass ratio

    計算結果表明，低壓渦輪和混合器的調節對發動機的性能和涵道比的影響尤為顯著；在其它部件幾何結構不同時，單個部件幾何調節后，發動機性能的變化趨勢是不同的。
  5. By the methodology of separating the math model and geometry model of unmanned helicopter, a geometry model is singly built and is processed with our 3d engine and customized math model

    本文中採用直升機的幾何模型與數學模型分開的方法，單獨建立幾何模型，利用開發的三維渲染引擎並結合自定義的數學模型進行渲染和控制。
  6. The physics engine manages a considerable amount of data, such as tyre temperature, chassis torque, weight distribution, suspension geometry, wheelbase, track, braking system characteristics and so on, in order to generate a precision never before experienced in a simulator

    物理引擎管理著相當數量的數據，如輪胎溫度，底盤扭矩，重量分佈，懸浮幾何，軸距，田徑，剎車系統的特點等對，為了產生一個精確以前從未經歷過在一個模擬器。
  7. In order to improve performance of truck diesel engine, we can from intake system, fuel injection system and combustion chamber geometry three aspects to commence

    提高車用自然吸氣直噴式柴油機的性能，可以從進氣系統，噴油系統以及燃燒室形狀等三個方面入手。
  8. Visualize geometry engine

    可視化幾何引擎
  9. But there are some problems in normal turbocharger, for example, the low speed engine torque is deficiency, the engine ca n ' t works with full capacity when in part load, the transient response remains slow, to improve all the above, the variable geometry turbocharger ( vgt ) comes out to be an effective way

    由於常規渦輪增壓存在低速轉矩不足、部分負荷經濟性差和瞬態響應遲緩的問題，而採用可變幾何截面渦輪增壓是解決這些問題比較有效的方案。本文以vgt60增壓器和yn4100qbz柴油機為研究對象，開發了可變幾何截面增壓器電控系統硬體。
  10. And then based on a surface - to - air missile that satisfies the requisition nearly, by means of reconstructing its geometry size, subsystems such as engine, the interceptor model used to continue the following studies is established. then the trajectory - control jet or attitude - control jet is added to the interceptor based on the analysis of the relationship between the missile performance and the thrust and configuration of the side jet

    然後以基本滿足方案要求的某型防空導彈為基礎，對其幾何尺寸、發動機等分系統進行改進，並通過分析導彈性能與側噴發動機參數之間的關系，增加了姿控或軌控側向裝置，這樣得到了本文的研究工作所需的導彈模型。
  11. This thesis presents a method about geometry modeling and kinematics simulation of vmt based on opengl geometry engine. in term of the method modeling and simulation of any kinds of nc machine tool can be constituted

    本文論述了基於opengl三維圖形引擎實現機床幾何建模和運動模擬的方法，本文所述方法可以實現任意數控機床的幾何建模和運動模擬。
  12. In divergent duct, adding heat can substitute the usage of geometry structure whatever mach number is. from force and thermodynamic cycle aspects, the effect of every components on engine performance was discussed

    結果認為，對於後體為純擴張構型的引射火箭，不論發動機通道內的馬赫數是多少，都可以通過加熱（改變加熱位置）代替常規幾何構型所起的作用。
  13. With stkconnect, qualnet sends commands in real time to the stk computation and geometry engine, adding network analysis and communication effects to the visually rich 2 or 3 - d animations

    計算和幾何引擎實時發送指令，將網路分析和通信效果添加於可視且豐富的二維或三維動畫。
  14. It indicates that thermal throat can substitute geometry throat, so structure integration can be achieved in ejectrojet mode. in addition, it showed that thermal throat will increase engine thrust and decrease specific impulse

    另外還得到熱力喉道取代幾何喉道后對發動機性能的影響，它可以提高發動機的推力，卻要降低比沖。
  15. Taking ti alloy tc11 electron beam welded work - piece as research object, which is the conventional material of aero engine compressor blisc, the fatigue damage evolution law of fatigue damage action in the area of welded joint based on damage mechanics theory is analysed, and fatigue damage model, which macro - parameter and micro - damage characteristics are related, with fractal geometry - a new conception of modern mathematics is set up in this paper. it tries to research the measuring method of fatigue fracture fractal dimension and the relationship of fractal damage variable with fatigue life. it also sets up the welded joint fatigue damage fractal evolution equation

    本課題以航空發動機壓氣機葉盤常用材料鈦合金（ tc11 ）電子束焊構件為研究對象，對焊接接頭的疲勞破壞行為，基於損傷力學理論分析其疲勞損傷演化規律，應用現代數學的新概念? ?分形幾何學理論，建立宏觀參量與細觀損傷特徵相聯系的疲勞損傷模型，研究疲勞斷口分維數測量方法以及分形損傷變量與疲勞壽命之間的關系，建立焊接接頭疲勞損傷分形演化方程。
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