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
收藏
页码：459 / 463
页数：5
相关论文
共 8 条
  • [1] Isikveren A.T., 2012, FP7AAT2012RTDL0
  • [2] Kim H.D., 2011, INT POW LIFT C LOND
  • [3] Kuntawala N.B., 2011, AIAA PAPER 2011 642, DOI [10.2514/6.2011-642, DOI 10.2514/6.2011-642]
  • [4] Liu C., 2012, 48 AIAA ASME SAE ASE
  • [5] Aerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft
    Lyu, Zhoujie
    Martins, Joaquim R. R. A.
    [J]. JOURNAL OF AIRCRAFT, 2014, 51 (05): : 1604 - 1617
  • [6] Sato S., 2011, 49 AIAA AER SCI M OR
  • [7] Steiner H. J., 2012, 28 C INT COUNCIL AER
  • [8] Tong M., 2009, P ASME TURB EXP 2009
1