Особливості теплогідравлічних процесів у маслорадіаторі авіаційного газотурбінного двигуна

Taras Mykhailenko, Oleksandr Goridko, Illia Petukhov
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Abstract

The modern gas turbine engines (GTEs) development is associated with an increase in the compressor pressure ratio and the gas temperature at the turbine inlet with a simultaneous reduction in the size and weight of the engine. The reliable operation of the GTE largely depends on the oil system excellence. In circulating oil systems, to ensure the lubrication and cooling of engine friction units, a high multiplicity of oil circulation is necessary. The preparation of oil for the next lubrication cycle is related to its cooling, cleaning of mechanical impurities formed during operation, and air separation. Oil coolers are used to cool the oil in GTEs. Air or fuel can be used as the cooling medium. Regardless of the cooling medium choice, a two-phase mixture (oil-air) and not a single-phase oil, as is considered when designing oil coolers, affects the course of thermo-hydraulic processes. Therefore, the subject of this paper is thermohydraulic processes in two-phase media. The goal of this study is to determine the specific aspects of thermohydraulic processes during the oil-air mixture cooling in an aviation gas turbine engine to further improve oil cooler design approaches. This paper aims to show the differences in the course of thermohydraulic processes in two-phase media from single-phase media and to emphasize the importance of considering them when designing oil coolers. The main results are as follows. For a two-phase flow, changes in temperature and pressure change not only the thermophysical properties of the phases but also the gas content, density, and speed of the mixture, which affects the course of thermohydraulic processes in the oil cooler. Under certain combinations of parameters, the structure of the two-phase flow may change. A low value of the equilibrium speed of sound can lead to unpredictable operation of the oil cooler and the oil system as a whole. In addition, the presence of an oil-air mixture reduces the heat transfer capacity of the oil cooler compared with the results of calculations using standard methods. In conclusion, it can be stated that to increase the efficiency of the oil system, it is extremely important to establish the regularities of thermo-hydraulic processes for the two-phase flow of the oil-air mixture and consider this during the design of oil coolers.
飞机燃气涡轮发动机油冷却器的热液压过程特点
现代燃气涡轮发动机(gte)的发展与压气机压力比和涡轮入口气体温度的增加有关,同时减小了发动机的尺寸和重量。GTE的可靠运行在很大程度上取决于油系统的优良性。在循环油系统中,为了保证发动机摩擦装置的润滑和冷却,需要高的油循环倍数。为下一个润滑循环准备油,涉及到它的冷却,清洗运行中形成的机械杂质,以及空气分离。油冷却器用于冷却gte中的油。空气或燃料可作为冷却介质。无论选择何种冷却介质,在设计油冷却器时所考虑的是两相混合物(油-空气)而不是单相油,都会影响热-液压过程的进行。因此,本文的主题是两相介质中的热液过程。本研究的目的是确定航空燃气涡轮发动机油气混合冷却过程中热液过程的具体方面,以进一步改进油冷却器的设计方法。本文旨在说明两相介质和单相介质中热水力过程的差异,并强调在设计油冷却器时考虑这些差异的重要性。主要结果如下:对于两相流,温度和压力的变化不仅会改变相的热物理性质,还会改变混合物的气体含量、密度和速度,从而影响油冷却器内热水力过程的进行。在一定的参数组合下,两相流的结构可能发生变化。低的平衡声速值会导致油冷却器和整个油系统的不可预测的运行。此外,与使用标准方法计算的结果相比,油气混合物的存在降低了油冷却器的传热能力。综上所述,为了提高油系统的效率,建立油气混合气两相流的热液过程规律,并在油冷却器的设计中加以考虑,是非常重要的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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