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| 1 | Effect of system response on partial surge initiated instability in a transonic axial flow compressor显示文摘Partial surge is a type of instability inception in transonic compressors and occurs in the form of axisymmetric low-frequency disturbances localized in the hub region.Previous studies illustrate that the frequency of partial surge is set by the Helmholtz frequency of the entire system,which motivates to propose a hypothesis that the system response performs an important role in the formation of partial surge.For further verification,a series of experiments are conducted to explore the link between the propagating of the partial surge and the system feedback in this study.In the first case,an additional test point is set on the wall of the plenum to detect the system response.Combining the flow behaviors inside the plenum with the disturbances in the rotor tip and stator hub/tip regions,the effects of the system feedback on the occurrence of the continuous disturbances and the rotating stall cells are illustrated.In the second case,a screen is mounted at the compressor outlet to prevent positive feedback from the plenum.The experimental results demonstrate that in the absence of system feedback,it is the occurrence of spike-type stall inception that leads to the flow instability instead of that of partial surge.In addition,three flow phenomena in the second case are discussed,including the occurrence of the single pulse,the unstable process during the stall evolution and the switch of instability inception. | Tianyu PAN Zhaoqi YAN Dakun SUN Simin LI Mengzong ZHENG Qiushi LI | 2022 | Chinese Journal of Aeronautics2022，35，2： | 2 |
| 2 | 转子叶尖间隙形状对跨声速轴流压气机性能影响机理分析显示文摘为研究转子不同叶尖间隙形状对跨声速轴流压气机性能的影响机理,分别对平行式叶尖间隙进行渐变式和阶梯式改型优化,并利用商业软件NUMECA进行数值模拟。结果表明:对平行式叶尖间隙进行渐变式和阶梯式改型优化后,压气机性能有较大提高,改型后0.204-0.408的各类间隙压气机性能优于0.408-0.204间隙的。相比较平行间隙PTC 0.204-0.204,渐变式TTC0.204-0.408和阶梯式STC 0.204-0.408的失速裕度分别提高1.12%和1.61%,峰值效率基本不变,同时近失速工况下的总压比和效率也略有提高。叶尖泄漏涡得到抑制,间隙处的流体低速区明显减小,流动损失减小,流场得到较大改善。转子通道的总压比在85%叶高处明显提高,分别提高了1.01%和3.13%。阶梯式叶尖间隙压气机的静子通道40%叶高处总压损失系数减小达75.4%。对平行式叶尖间隙进行改型处理能够有效提高压气机性能,且阶梯式叶尖间隙比渐变式的对压气机性能提高的效果更加显著。 | 张成烽 张国臣 徐志晖 孙丹 刘鹏程 | 2023 | 航空发动机2023，49，3： | 0 |
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