ESTIMATION OF GAS-DYNAMIC PARAMETERS AT THE EXIT OF THE IMPELLER DURING MODERNIZATION OF MI-2MSB FAN INSTALLATION

T. Tatarchuk, Yu. Kravchuk, V. Pelukh
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Abstract

Purpose. Analysis of methods to increase the efficiency of the cooling system of theAI-450M engine units of the Mi-2MSB helicopter and evaluation of gas-dynamic parameters at the impeller outlet, fan installation MI-2MSB Research methods: finite element method (FEM). Results. It was shown that the use of a centrifugal fan as the main element in the system of air injection, cabin air conditioning and cooling systems and engine units provide the following opportunities and improvements: - at constant speeds and without changes in the transmission system to increase the amount of running air by 200…300 %;  - reduce the temperature of heated units to the values recommended by the operation manual; - to increase the service life of complex-loaded elements of the system of connection of free turbine shafts with the shaft of the main gearbox;  - reduce the risk of accidents due to poor air conditioning in the cockpit and passenger seats. The analysis of possible types of C.S modernization was carried out, the estimated estimation of gas-dynamic parameters at the exit of the impeller - to the sub-radiator space was carried out. The problem was solved by changing the type of impeller from axial to centrifugal. Scientific novelty. The problem of creating an efficient and reliable cooling system for internal systems and units of the Mi-2MSB light multi-purpose aircraft, which has been modernized with the replacement of old GTD-350 engines with newer ones, AI-450 series - urgent, in the absence of similar light helicopters of domestic production. An important component of the safety and reliability of all components of the helicopter is to maintain the correct thermal regime of its components. Practical value. The obtained results are important in the further process of production and modernization of the Mi-2 helicopter of all modifications with the latest engines, as well as for helicopter development projects in Ukraine - SME-2 “Hope”, SME-6 “Otaman”, SME-8 and others. The ability to increase cooling efficiency, air conditioning and reduce engine load increases the life, reliability of components and improves comfort and performance for pilots and passengers.
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mi-2msb风机现代化安装过程中叶轮出口处气体动力参数的估算
目的。Mi-2MSB直升机ai - 450m发动机机组冷却系统效率提高方法分析及叶轮出口、风机安装Mi-2MSB气动参数评估研究方法:有限元法。结果表明,在空气喷射系统、客舱空调和冷却系统以及发动机单元中使用离心风扇作为主要元件提供了以下机会和改进:-在恒定转速和不改变传动系统的情况下,将运行空气量增加200%…300%;-将被加热机组的温度降低到操作手册推荐的值;-增加自由涡轮轴与主齿轮箱轴连接系统的复杂负载元件的使用寿命;-减少因驾驶舱内和乘客座位空调不良而发生事故的风险。分析了c.s.现代化的可能类型,对叶轮出口至副散热器空间的气体动力参数进行了估计估计。将轴向叶轮改为离心式叶轮,解决了这一问题。科学的新奇。在没有国内生产的类似轻型直升机的情况下,为米- 2msb轻型多用途飞机的内部系统和单元创建高效可靠的冷却系统的问题迫在眉睫。米- 2msb轻型多用途飞机已经现代化,用新的AI-450系列发动机取代了旧的GTD-350发动机。直升机所有部件的安全性和可靠性的一个重要组成部分是保持其部件的正确热状态。实用价值。所获得的结果对米-2直升机的生产和现代化的所有最新发动机改装的进一步进程以及乌克兰的直升机发展项目- SME-2“希望”,SME-6“奥塔曼”,SME-8和其他项目都很重要。提高冷却效率、空调和降低发动机负荷的能力增加了部件的寿命和可靠性,并提高了飞行员和乘客的舒适度和性能。
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