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INFLUENCE OF INLET PIPING CONDITIONS ON PUMP PERFORMANCE IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM

机译:进气管道条件对飞机发动机润滑系统中泵性能的影响

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This study investigates the influence of the inlet piping on the performance of the oil feed pump. Lubrication systems use geared volumetric pumps and in this case, a gerotor pump is used. The critical performance parameter is the volumetric efficiency. This paper begins with a theoretical description of cavitation, de-gassing and pump operation. Then, an overview of the different experimental investigations conducted on the Universite Libre de Bruxelles (ULB) aeroengine lubrication system test bench is given. This will highlight different sources of performance degradation. A short description of the numerical simulations conducted and results follow. Finally, the paper concludes with a proposition of a first basic model for pump performance.
机译:这项研究调查了入口管道对进油泵性能的影响。润滑系统使用齿轮容积泵,在这种情况下,使用齿轮泵。关键性能参数是体积效率。本文从空化,脱气和泵操作的理论描述开始。然后,概述了在布鲁塞尔自由大学(ULB)航空发动机润滑系统测试台上进行的各种实验研究。这将突出显示性能下降的不同原因。下面简要介绍了进行的数值模拟和结果。最后,本文以关于泵性能的第一个基本模型的命题作为结尾。

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