liquid gas tank 中文意思是什麼

liquid gas tank 解釋
液化器貯罐
  • liquid : n 1 液體。2 【語言學】流音〈如 [l] [r]〉 adj 1 液體的,液態的,流動的。2 清澄的,透明的。3 易變的...
  • gas : n (pl gases )1 氣,氣體,氣態 〈cf fluid; solid〉 2 可燃氣,煤氣,沼氣;【礦物】瓦斯。3 【軍事...
  • tank : n 1 罐,槽;箱;櫃〈盛液體或氣體的大容器〉;(火車頭的)水櫃;(船上的)液體艙;〈美、英方〉水堰...
  1. This device helps vent gas that boils off from the liquid oxygen tank, and also bathes the top of the tank in warmed nitrogen to prevent ice from forming.

    這個裝置有助於排除液氧燃料箱蒸發的氣體,並且它還可以用加溫氮氣籠罩箱頂,以防結冰。
  2. Different equations to corresponding components are presented by analysing and transformating the general equations of fluid routes, then static characteristics mathematical model of liquid propellant space propulsion system is presented. based on the data of static characteristics calculation, mass model of thruster, propellant, propellant tank, gas, gas bottle, pipe and valve is presented using both the method of statistical regression and the method of stress analysis, then corresponding mass model is presented. based on the characteristics of liquid propellant space propulsion systems, analyse the five phases ( concept and definition, design and improvement, manufactureing and arrangement, operation and ma intenance, disposal ) in which life cycle cost of liquid propellant space propulsion systems is cost separately, then discompsed structure of life cycle cost and model of life cycle cost are presented

    將組件分成氣路組件和液路組件,再對氣路組件和液路組件進行相應的分類,然後通過對通用流路方程進行分析和變換對不同類型的組件分別建立不同的方程,從而建立了一個適用於液體推進劑空間推進系統的靜態數學模型;根據靜態計算所得到的數據,應用統計回歸法和應力分析法分別建立推力室、推進劑、推進劑貯箱、氣體、氣瓶以及導管和活門等的質量模型,從而建立相應的質量模型;結合液體推進劑空間推進系統特點,對液體推進劑空間推進系統全壽命周期費用發生的五個階段(概念和定義、設計和改進、製造和安裝、運行和維修、處理)分別進行分析,建立了液體推進劑空間推進系統全壽命周期費用分解結構和全壽命周期費用模型。
  3. The gas - phase inlet, the outlet of the reflux pipe is at above the liquid surface in the cryogenic tank, is presented

    得出了循環預冷技術在低溫液體火箭發動機預冷程序中可以採用的結論。
  4. Comparing to the liquid - phase manner that the outlet of the reflux pipe is below the liquid surface in the tank, the cool - down cycle may last longer and the prestart program may be more simple in using the gas - phase inlet manner

    並建議採用氣相迴流的方法,可以實現更佳的預冷效果,其自然循環預冷可以維持更長時間,同時能更進一步簡化射前程序。
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