Abstract
As the research object of inducer and impeller combination aero fuel centrifugal pumps, the outlet clearance optimization on axial-force of the pump was carried out. Through comparing the axial-force simulation data with theoretical calculation data, the axial-force trends of the two methods were identified similar and the simulation's accuracy was verified by Pumplinx because of the error less than 4%. Then the outlet clearance's influence on axial-force was analyzed. Simulation results show that expanding the clearance to 0.2 mm increases the axial-force value, and reduces the pressure charging; but reducing the clearance to 0.1 mm and 0.13 mm can make optimizations of the axial-force, and the clearance of 0.1 mm is the best. The axial-force performance of the model with clearance of 0.1 mm was analyzed finally, showing that this model's inner performance of different sections is normal and steady; the axial-force value at design point is 3 620 N, so reducing the outlet clearance to 0.1 mm can make a high optimization about axial-force of the inducer and impeller combination centrifugal pump.
| Original language | English |
|---|---|
| Pages (from-to) | 2765-2772 |
| Number of pages | 8 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 31 |
| Issue number | 11 |
| DOIs | |
| State | Published - 1 Nov 2016 |
Keywords
- Aero fuel centrifugal pump
- Axial-force
- Combination
- Inducer and impeller
- Outlet clearances optimization
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