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作 者:田江涛[1] 唐方明[1] 邹学奇[1] 王国文[1] 银越千[1] TIAN Jiang-Tao, TANG Fang-Ming, ZOU Xue-Qi, WANG Guo-Wen ,YIN Yue-Qian(AVIC Aviation Powerplant Research Institute, Zhuzhou, China 412002, Chin)
机构地区:[1]中航工业航空动力机械研究所,株洲412002
出 处:《工程热物理学报》2018年第8期1673-1679,共7页Journal of Engineering Thermophysics
摘 要:完成了某双级离心压气机的试验特性录取,在各分级特性满足指标要求的情况下,双级试验设计点性能明显低于设计指标。对比各级在双级中的特性以及在双级中的匹配特征发现:双级中的进口级性能与单独进口级吻合较好,而出口级径向扩压器叶顶与盖板采取的压紧连接方式,因高温、高压变形会产生较大的间隙泄漏损失,使得出口级性能恶化并导致双级离心提前喘振,这在叠加双级特性结果的对比中得到了进一步确认。The test performance of a double-stage centrifugal compressor has been finished, and the double-stage test characteristics in the design point is obviously lower than the design target in the condition of filling the requirement of every single stage. Through the contrast of single-stage performance and the matching relations in the combined compressor, we could get a result that the inlet-stage performance in the double stage primely accords with the single inlet-stage, and because the blade tip in the radial diffuser of the outlet stage was impacted tightly into the cover, a big gap was appeared as a result of serious distortion in the condition of high pressure and high temperature. However, the contrast between the self double-stage performance and the superpositioned results further confirmed that the tip clearance would produce a bigger tip leakage loss, which will worsen the outlet-stage characteristics and push the double stage into the surge state ahead.
分 类 号:TK123[动力工程及工程热物理—工程热物理]
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