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.
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页码：133 / 138
页数：6
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