Development challenges of distributive propulsion systems for advanced aeroplanes

被引：1

作者：

Isyanov, Alik ^{[1
]}

Lukovnikov, Alexander ^{[1
]}

Mirzoyan, Artur ^{[1
]}

机构：

[1] CIAM, Prop & AC Matching Dept, Moscow, Russia

来源：

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY | 2014年 / 86卷 / 06期

关键词：

Distributed propulsion system; Outboard fan; Engine core; Mechanical drive; Transmission; Fuel efficiency;

D O I：

10.1108/AEAT-06-2014-0089

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Purpose - This paper aims to consider main challenges of development of advanced architectures of propulsion systems, i.e. distributed propulsion systems (DPS). Design/methodology/approach - This paper is a comparative analysis of different types of DPS. Findings - Mechanical driving DPS seems as more feasible in near-term outlook, and turboelectric and full electric DPS are imagined feasible in mid- and far-term outlook. Research limitations/implications - Additional comprehensive numerical and experimental researches are needed to approve the efficiency of DPS. Practical implications - Possible impact of installation of DPS on aeroplane fuel efficiency are shown. Originality/value - Application of DPS on long-range aeroplanes is new a engineering solution, which may allow to meet future advanced efficiency goals.

引用

页码：459 / 463

页数：5

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