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从非定常效应看对旋风扇/压气机的工程实现 总被引:5,自引:0,他引:5
首先利用全隐格式的非稳态压力修正求解方法;计算对旋风扇级间流场非定常流动情况,并与实验结果进行了有益的对比;在动态实验研究中则通过单斜丝热线风速仪对对旋风扇级间速度场进行了详细分析,并揭示其级间非定常效应的独特规律:下游转子的非定常位势流作用在对旋级间流场的周期性非定常影响中占主导地位,级间径向速度的大小则主要与前级转子叶尖区和叶根区的二次流动旋涡强度有关.上述结果表明:对旋风扇/压气机的非定常效应对其性能有很大影响,如果很好地组织对旋叶轮的非定常流动气动布局,可进一步提高增压系统的压比、效率和稳定工作范围。 相似文献
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轴流压气机旋转失速的预示研究 总被引:1,自引:0,他引:1
大量的研究表明,旋转失速现象的发生不仅与压气机工作状态的气动参数有关,而且与压气机几何参数有直接关系。本文的目的是用实验的方法找出影响压气机旋转失速发生的主要因素,通过对实验数据分析研究获得判别失速发生的准则。文中首先对十个低速转子进行试验,其主要几何参数为稠度τ=1.5,轮毂比为0.815,安装角γ分別为45°和60°,弯角θ分别为0°,15°,34°,45°,60°。试验表明:具有各种不同几何参数(弯 相似文献
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Non-axisymmetric wake impact experiments were carried out after the best exciting frequency for a low speed axial compressor had been found by axisymmetric wake impact experiments. When the number and circumferential distribution of inlet guide vanes (IGV) are logical, the wakes of non-axisymmetric IGVs can exert beneficial unsteady exciting effect on their downstream rotor flow fields and improve the compressor's performance. In the present paper, four non-axisymmetric wake impact plans were found working better than the axisymmetric wake impact plan. Compared with the base plan, the best non-axisymmetric plan increased the compressor's peak efficiency, and the total pressure rise by 1.1 and 2%, and enhanced the stall margin by 4.4%. The main reason why non-axisymmetric plans worked better than the axisymmetric plan was explained as the change of the unsteady exciting signal arising from IGV wakes. Besides the high-frequency components, the nonaxisymmetric plan generated a beneficial low-frequency square-wave exciting signal and other secondary frequency components. Compared with the axisymmetric plan, multifrequency exciting wakes arising from the non-axisymmetric plans are easier to get coupling relation with complex vortices such as clearance vortices, passage vortices and shedding vortices. 相似文献
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