Analysis of the Hydraulic System of a Long-Haul Aircraft

被引：0
|
作者：
Grachev, S., V [1 ]
Smagin, D., I [1 ]
Vasilyev, N. G. [1 ]
Savelev, R. S. [1 ]
Zinina, A., I [1 ]
机构：
[1] Natl Res Univ, Moscow Aviat Inst, Dept Aircraft Design & Certificat, Moscow, Russia
来源：
2021 12TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE) | 2021年
关键词：
hydraulic system; hydraulic system structure; hydraulic system reliability; hydraulic system analysis;
D O I：
10.1109/ICMAE52228.2021.9522518
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
At the moment, the design of various aircraft systems is a complex process in which you have to choose from a large number of competing versions of the developed system. Decisions that were made during development can affect various key factors, including system reliability. In this article a comparative analysis of two variants of hydraulic system power unit design for a heavy twin-engine aircraft with passenger capacity up to 300 people was carried out. For the analysis was taken a number of basic technical solutions, which were applied in such aircraft as A-350, B-787, IL-96, SSJ-100, and several others. As a result of the analysis, the most suitable version of the hydraulic system in terms of reliability and the possibility of implementing this version of the system was selected.
引用
收藏
页码：133 / 138
页数：6
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