Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (5): 529666-529666.doi: 10.7527/S1000-6893.2023.29666
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Guoning QI1,2,3, Baohai WU2,3(), Jiangfeng FU4
Received:
2023-09-28
Revised:
2023-10-08
Accepted:
2023-10-18
Online:
2024-03-15
Published:
2023-11-01
Contact:
Baohai WU
E-mail:wubaohai@nwpu.edu.cn
Supported by:
CLC Number:
Guoning QI, Baohai WU, Jiangfeng FU. Comparative analysis on relief grooves of high-speed and high-pressure aeroengine fuel gear pumps[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529666-529666.
Table 4
Statistics of simulated outlet flow rate results
卸荷槽类型 | 流量最大值/(kg·s-1) | 流量最小值/(kg·s-1) | 流量平均值/(kg·s-1) | 供油量不均匀系数/% |
---|---|---|---|---|
卸荷槽A | 5.555 56 | 4.945 49 | 5.259 7 | 11.60 |
卸荷槽B | 5.498 99 | 5.139 37 | 5.300 5 | 6.78 |
卸荷槽C | 5.706 62 | 4.738 98 | 5.215 1 | 18.55 |
卸荷槽D | 5.552 68 | 4.909 87 | 5.258 3 | 12.22 |
卸荷槽E | 5.748 75 | 4.558 65 | 5.236 0 | 22.73 |
卸荷槽F | 5.482 81 | 5.204 60 | 5.304 2 | 5.25 |
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