Experimental investigation of the influence of seal cavity leakage on a compressor performance
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摘要:
以两台单级压气机为试验对象,分别采用调节压气机进口节流比和封严腔供气压力两种方式,开展了封严腔泄漏流对压气机性能影响的试验研究,获取了封严腔泄漏流对压气机性能影响规律。研究结果表明:随着压气机进口节流比的降低或封严腔压力的增加,封严空气泄漏量逐渐增大,但增幅变化逐渐变得缓慢;随着封严空气泄漏量的增加,压气机出口叶根区域主流压力逐渐降低、叶片尾迹区增大,压气机性能逐渐降低;当试验件存在多封严腔供气时,与前封严腔相比,后封严腔空气泄漏对压气机效率影响较大,且随着转速升高影响程度增大。
Abstract:An experimental investigation of the influence of seal cavity leakage on compressor was carried out on two compressors with variable inlet throttle ratio and cavity pressure respectively. The investigation results showed that seal cavity leakage flow rate increased with the decrease of inlet throttle ratio or the increase of cavity pressure. As the seal cavity leakage flow rate increased, the outlet pressure of main flow decreased and the blade wake area expanded near compressor hub, reducing the compressor performance. In a compressor experiment with multiple seal cavities, compared with the front seal cavity, the influence of leakage flow rate at rear seal cavity on compressor efficiency was greater, and the higher rotating speed indicated the greater influence.
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Key words:
- leakage flow rate /
- compressor /
- throttle ratio /
- seal cavity pressure /
- aerodynamic performance
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表 1 封严篦齿参数
Table 1. Sealing grate parameters
试验件 前齿数 前齿间隙/mm 后齿数 后齿间隙/mm 1# 3 1.0 3 2.0 2# 2 0.96 2 0.82 表 2 不同封严压差下的泄漏量
Table 2. Leakage under different sealing pressure difference
试验件 n/% K Δp/kPa 相对泄漏量/% 1# 95 0.931 p1=26.7 W1=0.5 1# 95 0.658 p1=46.3 W1=0.6 1# 95 0.660 p1=46.7 W1=1.9 1# 95 0.506 p1=59.1 W1=2.8 2# 90 0.985 p1=15.0 W1=0.8 2# 90 0.985 p1=31.4 W1=1.4 2# 90 0.985 p1=53.9 W1=2.4 2# 90 0.985 p2=5.5 W2=0.2 2# 90 0.985 p2=51.2 W2=2.3 2# 90 0.985 p2=75.6 W2=3.2 2# 90 0.985 p2=90.4 W2=3.6 2# 60 0.995 p2=17.0 W2=0.8 2# 60 0.995 p2=35.9 W2=2.2 2# 60 0.995 p2=53.9 W2=3.7 -
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