爆燃壓縮壓力 的英文怎麼說

中文拼音 [bàoránsuō]
爆燃壓縮壓力 英文
detonating compression pressure
  • : 動詞1. (猛然破裂或迸出) explode; burst 2. (放在滾油里快炒) quick-fry
  • : 動詞1. (燃燒) burn 2. (引火點著) ignite; light
  • : 壓構詞成分。
  • : 縮構詞成分。
  • : Ⅰ名1 (力量; 能力) power; strength; ability; capacity 2 [物理學] (改變物體運動狀態的作用) forc...
  1. A new calculation method for optimizing diesel engine performance, called nonlinear regression - mess method, is put forward. in this paper, 25 groups of simulated values are calculated from the diesel engine working model, specific fuel consumption, peak pressure, rate of pressure rise, nox and peak temperature are fitted into explicit function about compression ratio and fuel injection advance angle

    本文利用柴油機工作過程模型,得出25組模擬計算數據,利用非線性回歸將油耗、最大升高率、 no _ x濃度及最高燒溫度擬合成比和噴油提前角的顯函數,並用網格法進行優化,用c語言編制了優化計算程序,得出最佳的比和噴油提前角,使其優化匹配。
  2. Moreover, it has been pointed out that the hydrogen engine used in ? cylinder injection with high pressure can increase volumetric efficiency and compression ratio, - therefore, the performance indexes in this engine, such as output power, thermal efficiency, range of thickness of mixture with normal operation and nox emission, can be improved, and it is possible for the engine to realize rapid combustion of thin mixture, so abnormal combustion, such as backfire, pre ? ignition, can be controlled effectively

    指出了採用內部混合氣形成方式且高噴射的氫發動機,有利於提高充氣效率和比,從而改善發動機的動性和經濟性;有利於擴展發動機正常工作的濃度范圍;並且有利於實現稀薄混合氣快速燒,從而可以有效地抑制早、回火及等異常燒和no _ x排放量。試驗指出了發動機的點火正時、噴射正時及噴氫量對發動機的性能、異常燒、 no _ x排放量有很大影響。
  3. Based on the variables of inlet length, compression ratio, inlet opening phase and the exhaust closing phase, multi - objective optimization was conducted for power, torque, combustion noise and fuel consumption indicators with constraint conditions of fuel consumption rate and the maximum breakout pressure

    以進氣道長度、比、進氣開啟相位、排氣關閉相位為可變因素;以比油耗、最高為約束條件,針對滿足功率、扭矩、燒噪聲和油耗指標進行多目標優化設計。
  4. Then using kerosene as fuel, oxygen and compressed air as oxidizers, proof - of - principle experiments of pdre were successfully conducted the results show that the measured detonation wave pressures are close to theoretical values it also indicate that using kerosene as the fuel of pdre is feasible

    採用航空煤油為料,氧氣和空氣為氧化劑,分別進行了兩相脈沖震火箭發動機原理性試驗,所測得的震波接近充分發展的理想震波,說明採用煤油作為脈沖震火箭發動機的料是可行的。
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