文章摘要
飞机舱门密封系统的仿真分析与优化设计
Simulation Analysis and Optimization Design of Sealing System of Aircraft Cabin Door
投稿时间:2022-02-28  修订日期:2022-02-28
DOI:10.12136/j.issn.1000-890X.2023.08.0563
中文关键词: 舱门密封系统  密封带  截面圆角半径  增强织物  硅橡胶材料  密封性能
英文关键词: sealing system of cabin door  sealing strip  section fillet radius  reinforcement fabric  silicone rubber material  sealing performance
基金项目:辽宁省教育厅青年科技人才“育苗”项目(JYT19026);沈阳航空航天大学博士科研启动项目(18YB32)
作者单位E-mail
姚文心 沈阳航空航天大学 民用航空学院 1415510014@qq. com 
徐鸣遥 沈阳航空航天大学 民用航空学院 xumingyao@sau.edu.cn 
袁永平 沈阳航空航天大学 民用航空学院  
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中文摘要:
      对飞机舱门(简称舱门)密封系统进行仿真分析,通过正交试验对密封带的结构和材料进行优化设计。结果表 明:密封带的截面圆角半径对舱门密封系统的应力产生影响,密封带的截面圆角半径为3.5 mm时舱门密封系统的压缩应 力最小,最大接触应力最大;密封带的内部增强织物能同时提高舱门密封系统的压缩应力与最大接触应力,但对压缩应力 的影响较小;密封带采用35U硅橡胶材料时舱门密封系统的压缩应力与最大接触应力最小,密封带采用75U硅橡胶材料时 舱门密封系统的压缩应力与最大接触应力最大;舱门密封系统的压缩应力与最大接触应力随着密封带的硅橡胶材料邵尔 A型硬度的增大而增大。当密封带的截面圆角半径为3.5 mm、采用邵尔A型硬度为50度的55U硅橡胶材料、内部有增强织 物时,舱门密封系统的密封性能最优。
英文摘要:
      The sealing system of aircraft cabin door(referred to as cabin door) was simulated and analyzed,and the optimization design of the structure and material of the sealing strip was carried out through orthogonal experiments.The results showed that the section fillet radius of the sealing strip had a significant impact on the stress of the sealing system of cabin door.When the section fillet radius was 3.5 mm,the maximum contact stress of the sealing system was the highest,and the compression stress was the lowest.The internal reinforcement fabric of the sealing strip could simultaneously increase the compression stress and maximum contact stress of the sealing system of cabin door,but had little effect on the compression stress.When the sealing strip was made of 35U silicone rubber material,the compression stress and maximum contact stress of the sealing system of cabin door were the smallest,and when the sealing strip was made of 75U silicone rubber material,the compression stress and maximum contact stress were the largest.Moreover,the compression stress and maximum contact stress increased with the increase of Shore A hardness of the silicone rubber material.When the section fillet radius of the sealing strip was 3.5 mm,55U silicone rubber material with a shore A hardness of 50 degree was used,and a layer of reinforcement fabric was applied,the sealing performance of the sealing system of cabin door was the best.
Author NameAffiliationE-mail
YAO Wenxin Shenyang Aerospace University 1415510014@qq. com 
XU Mingyao Shenyang Aerospace University xumingyao@sau.edu.cn 
YUAN Yongping Shenyang Aerospace University  
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