• The way to improve total pressure efficiency by appropriate inclined cut of airfoil blade tip was studied.

    分析了对后拖式机翼型叶片叶尖进行适当切割可以提高效率的原因。

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  • The measurements show that the airfoil blade fan prevails over the plate one in the aspects of total pressure efficiency, stable operation range and high efficient operation range.

    试验结果表明机翼叶片效率稳定运行范围高效运行范围相应型叶片具有优越性;

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  • After optimization, the total pressure loss of the turbine vane was reduced by 0.95%, and the efficiency of the overall compressor was increased by 2.1%.

    优化后透平高压级静损失系数减少0.95%;多级压气机整机效率提高2.1%。

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  • It is shown that the U-bottom orifice has higher total pressure drop and (thermodynamic) efficiency.

    结果表明,U型弧节流具有更高的热力学效率。

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  • The expander can reduce exergy loss in pressure reducing process, and the utilization of cryogenic exergy of air-powered engine exhaust is useful to improve the total energy efficiency.

    能量转移系统,应该采用容积膨胀减压方式减少减压环节可用损失;合理利用低温排气的冷量可以提高气动发动机能量转移系统能量效率

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  • The total efficiency and volumetric efficiency are analyzed based on the flow rate and pressure measured, and their impact factors are discussed.

    根据测试流量压力数据,分析了液压变压器效率容积效率的变化规律,并讨论了影响总效率和容积效率的因素

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  • The total efficiency and volumetric efficiency are analyzed based on the flow rate and pressure measured, and their impact factors are discussed.

    根据测试流量压力数据,分析了液压变压器效率容积效率的变化规律,并讨论了影响总效率和容积效率的因素

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