SIZING OF AN AIRCRAFT FUEL PUMP

被引：3
|
作者：
ROHATGI, US
机构：
[1] Brookhaven National Laboratory, Department of Advanced Technology, Upton, NY, 11973
来源：
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME | 1995年 / 117卷 / 02期
关键词：
D O I：
10.1115/1.2817144
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
A need to pump a mixture of two-phase fluid appears naturally in many situations. One example of this situation is aircraft fuel systems, where the pump inlet may have two-phase mixture due to the desorption of the dissolved gases at low pressures at higher altitudes. A simple procedure of selecting proper design conditions for the inlet inducer and a method of sizing the inducer, impeller and volute to meet all the design requirements has been described. This procedure has also been applied to a typical fighter plane boost pump design.
引用
收藏
页码：298 / 302
页数：5
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