The Modernization Concept of Aircraft An-26 and An-140 Based on the Use of a Hybrid Power System

Volodymyr Shmyrov, V. Loginov, S. Fil', A. Khaustov, Olexander Bondarchuk, Andrii Kalashnikov, Glib Khmelnitskiy
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引用次数: 3

Abstract

This paper reports a modernization concept of aircraft An-26 and An-140 based on the use of a hybrid basic propulsion system (HBPS). The study object is the aircraft of transport and passenger categories in the weight dimension from 20 to 25 tons. The analysis of the ways of modernization has shown that under the new market conditions two directions in the development of light aircraft «Antonov» become relevant. The first is the modernization of the existing fleet of An-26, the second is the construction of an An-140T ramp transport variant based on the An-140 aircraft. One of the considered ways of such modernization is to equip the aircraft with hybrid basic propulsion systems consisting of the gas-turbine and power electric motors, which drive the rotation of the propeller. The use of HBPS makes it possible to optimize the operation of the gas-turbine engine over a narrow traction-speed range ‒ only for the cruising section of the flight. This makes it possible to design a GTE with high fuel and weight efficiency. In this case, noise and harmful emissions could be significantly lower. The analysis has been given of existing aviation hybrid propulsion systems with recommendations on the choice of the optimal scheme to modernize aircraft An-26 and An-140. It is proposed to solve the task by choosing the option of a basic propulsion system with a moderate degree of hybridization, based on the well-established engine TV3-117VMA-SBM1. That improves the flight range of An-26 and An-140 with a payload capacity of 4.5‒5 tons by 1.4‒1.7 times, respectively. The results obtained confirm the correctness of the proposed modernization concept. The analysis results demonstrate a significant improvement in the flight characteristics of the aircraft, as well as compliance with current and projected environmental standards. The results reported could be recommended for the practical modernization of aircraft An-26 and An-140
基于混合动力系统的安-26和安-140飞机现代化构想
本文报告了基于使用混合基本推进系统(HBPS)的飞机安-26和安-140的现代化概念。本研究的对象是飞机的运输和客运类别在重量维度从20到25吨。对现代化方式的分析表明,在新的市场条件下,“安东诺夫”轻型飞机的发展有两个方向是相关的。第一个是对现有的安-26机队进行现代化改造,第二个是在安-140飞机的基础上建造安- 140t坡道运输机。这种现代化的考虑方法之一是为飞机配备混合动力基本推进系统,包括燃气轮机和驱动螺旋桨旋转的动力电动机。HBPS的使用使燃气涡轮发动机在狭窄的牵引力-速度范围内优化运行成为可能-仅适用于飞行的巡航部分。这使得设计具有高燃油效率和重量效率的GTE成为可能。在这种情况下,噪音和有害排放物可能会大大降低。对现有航空混合动力推进系统进行了分析,并对安-26和安-140飞机的现代化优化方案的选择提出了建议。为了解决这一问题,提出了在TV3-117VMA-SBM1发动机的基础上,选择适度混合的基本推进系统的方案。这将4.5 ~ 5吨的安-26和安-140的飞行距离分别提高了1.4 ~ 1.7倍。所得结果证实了所提出的现代化概念的正确性。分析结果表明,飞机的飞行特性有了显著改善,并且符合当前和预计的环境标准。报告的结果可以推荐给安-26和安-140飞机的实际现代化
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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