Numerical study on the ejector structure of deaerator

Qiang Tian, Zhen Xia Liu, Jian Ping Hu

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Aeroengine oil systems typically have a deaerator to reduce the amount of air in the oil. Modern aircraft may not be able to draw oil when flying under multi-attitude conditions, so consider designing a deaerator with an ejector structure to ensure that the aircraft continues to supply oil during multiple conditions. A deaerator with an ejector structure was designed to analyze the feasibility of the ejector function based on the Bernoulli principle. The CFD method was used to simulate the two-phase flow of the oil and air mixture in the ejector structure of the deaerator. Firstly, it was analyzed whether the structure can achieve the ejector function. In addition, the influence of oil-gas ratio on the ejector mass flow rate and the ejection coefficient was studied. Finally, this paper studied the influence of the area ratio at the diffusion section on the ejector effect. It can draw the following conclusions from this research:1. The pressure drop at the ejector nozzle can overcome the influence of the oil's gravity and achieve the ejector function. 2. The oil-gas ratio has a greater influence on the ejector effect under different working conditions.3. The structure of the ejector with an area ratio of 1.5 is superior to the others in the ejector effect.

源语言英语
主期刊名2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
出版商Institute of Electrical and Electronics Engineers Inc.
475-481
页数7
ISBN(电子版)9781728155357
DOI
出版状态已出版 - 7月 2019
活动10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 - Brussels, 比利时
期限: 22 7月 201925 7月 2019

出版系列

姓名2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

会议

会议10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
国家/地区比利时
Brussels
时期22/07/1925/07/19

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