主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
水陆两栖飞行器汲水系统结构改进设计与仿真验证
作者:
作者单位:

庆安集团有限公司 航空设备研究所

中图分类号:

TP182


Improved design and simulation verification of water pumping system structure for amphibious aircraft
Author:
Affiliation:

1.Aviation Equipment Research Institute,QINAN GROUP CO.,LTD,Xi’an 710077;2.China

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    摘要:

    汲水系统是飞行器灭火系统实现汲水功能的主要系统,改进汲水系统的设计可以缩短汲水时间,提高灭火效率。对某型两栖飞行器的原始汲水系统进行基于计算流体力学的仿真分析,发现其出口位置设置不合理,导致两个出口流量差别过大,汲水时间过长,不满足汲水要求。为了缩短汲水时间,提出两种不同出口位置的汲水结构形式,并通过仿真分析得到出口流量差别较小的出口位置模型,在该模型基础上增加挡板并提出三种不同挡板位置模型。结果表明:当挡板距离管道中线10 mm 时,两个出水口流量大致相同,汲水时间较原始汲水系统构型缩短了50%,上述结构改进对后续该型两栖飞行器汲水管路设计具有重要意义。

    Abstract:

    The water scooping system is the main part of the extinguishing aircraft system for realizing the water scooping function. Improving the design of water scooping system can shorten the time of water scooping and improve fire extinguishing efficiency as soon as possible. In this paper,CFD-based simulation analysis is performed on the original water scooping system of a certain type of amphibious aircraft.The results show that the unreasonable position of the outlets of the original water scooping system makes the volume flow difference between the two outlets are too large,and the water scooping time is to long, which is not conform to the water scooping requirements.In order to reduce the scooping time, two structural forms of water scooping system at different outlet positions are designed,and obtain the outlet position model with small volume flow difference by simulation analysis,and design the battle model with three different position base on the outlet model with small volume flow difference.when the baffle is 10mm from the center line of the water scooping pipe, the flow rate of the two outlets is roughly the same,and the water scooping time is 50% shorter than that of the original configuration of water scooping system, which is great significance to the subsequent design of the water scooping pipeline of amphibious aircraft.

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引用本文

叶庆龙,杜秀军,李文源.水陆两栖飞行器汲水系统结构改进设计与仿真验证[J].航空工程进展,2022,13(6):160-165,183

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历史
  • 收稿日期:2021-07-29
  • 最后修改日期:2022-03-31
  • 录用日期:2022-04-06
  • 在线发布日期: 2022-06-23