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
相关论文
共 50 条
  • [21] Analyzing well-to-pump emissions of electric and conventional jet fuel for aircraft propulsion
    Yildiz, Melih
    Kale, Utku
    Nagy, Andras
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2022, 94 (10): : 1605 - 1613
  • [22] LOW AREA RATIO AIRCRAFT FUEL JET-PUMP PERFORMANCES WITH AND WITHOUT CAVITATION
    MARINI, M
    MASSARDO, A
    SATTA, A
    GERACI, M
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1992, 114 (04): : 626 - 631
  • [23] FUEL SYSTEM WITH VARIABLE SPEED PUMP TO IMPROVE THERMAL MANAGEMENT ABILITY FOR AIRCRAFT ENGINES
    Oba, Daisuke
    Gonda, Yukinori
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 6, 2014,
  • [24] The impact of sustainable aviation fuels on aircraft fuel line ice formation and pump performance
    Ugbeh-Johnson, J.
    Carpenter, M.
    AERONAUTICAL JOURNAL, 2023, 127 (1314): : 1287 - 1307
  • [25] COMPUTER SIZING OF FIGHTER AIRCRAFT.
    Coen, Peter G.
    Foss, Willard E.
    1600, (23):
  • [26] Effects of Partial Fuel Pump Failure on Center of Gravity Control for High-speed Aircraft
    Li, Haiquan
    Zhang, Jing
    Yan, Jianing
    2016 IEEE/CSAA INTERNATIONAL CONFERENCE ON AIRCRAFT UTILITY SYSTEMS (AUS), 2016, : 146 - 150
  • [27] Formal Refinement and Partitioning of a Fuel Pump System for Small Aircraft in Hybrid Event-B
    Banach, Richard
    2016 10TH INTERNATIONAL SYMPOSIUM ON THEORETICAL ASPECTS OF SOFTWARE ENGINEERING (TASE), 2016, : 65 - 72
  • [28] Design of a Six-Phase Fault-Tolerant Electric Motor for an Aircraft Fuel Pump
    Ismagilov, Flyur R.
    Vavilov, Viacheslav Ye.
    Karimov, Ruslan D.
    Ayguzina, Valentina V.
    Kammermann, Joerg
    Bolvashenkov, Igor
    Herzog, Hans-Georg
    2019 FOURTEENTH INTERNATIONAL CONFERENCE ON ECOLOGICAL VEHICLES AND RENEWABLE ENERGIES (EVER), 2019,
  • [29] Fuel pump
    不详
    GAS ENGINEERING & MANAGEMENT, 1999, 39 (04): : 30 - 30
  • [30] SIZING SMALL STORMWATER PUMP STATIONS
    FROEHLICH, DC
    WATER RESOURCES BULLETIN, 1994, 30 (06): : 1055 - 1062
12345