Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (5): 529666.doi: 10.7527/S1000-6893.2023.29666
• Articles • Previous Articles Next Articles
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.
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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