Attributing to the large flow rate, high efficiency level reaction turbine is adoptive in staged combustion cycle liquid rocket engine.
基于闭式补燃循环液体火箭发动机流量大的特点，欲设计效率水平高的航天反力式涡轮。
At the same time, the quantitative relation, in the proposed cycle, among the gas turbine exhaust flow, the vaporized LNG flow and the CO2 working medium flow, is shown in this paper.
最后文中还给出了在这种循环中，燃气轮机排气流量、汽化的LNG流量和循环工质流量三者之间的定量耦合关系。
The invention relates to a combined cycle of a high-power diesel engine and a divided-flow two-level turbine engine with one pump.
大功率柴油机与分流式一泵两级涡轮发动机联合循环。
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