某型飞机弹射座椅穿盖弹射试验与数值模拟

V215.2; 通过某型飞机弹射座椅穿盖弹射火箭滑车试验,研究了舱盖在穿盖弹射中的破裂形式.在试验研究的基础上,进行了数值模拟,利用PCL语言对MSC.PATRAN进行二次开发,实现参数化建模.采用非线性有限元方法,通过瞬态动力学软件MSC.Dytran仿真得到了人椅系统在穿盖出舱过程中的过载及舱盖的破裂效果,与试验数据对比吻合较好,验证了模型的准确性.在此基础上,以VC及OpenCASCADE为工具,开发了通用性的飞机座椅弹射仿真平台,该平台具有一定的工程应用价值....

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Published in南京航空航天大学学报 Vol. 45; no. 3; pp. 336 - 340
Main Authors 王一丁, 童明波, 闫家益, 潘雄
Format Journal Article
LanguageChinese
Published 南京航空航天大学飞行器先进设计技术国防重点学科实验室,南京,210016 2013
Subjects
参数化建模
二次开发
parametric modeling
动力学分析
through canopy ejection
dynamics analysis
穿盖弹射
secondary development
Online AccessGet full text
ISSN1005-2615

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Abstract V215.2; 通过某型飞机弹射座椅穿盖弹射火箭滑车试验,研究了舱盖在穿盖弹射中的破裂形式.在试验研究的基础上,进行了数值模拟,利用PCL语言对MSC.PATRAN进行二次开发,实现参数化建模.采用非线性有限元方法,通过瞬态动力学软件MSC.Dytran仿真得到了人椅系统在穿盖出舱过程中的过载及舱盖的破裂效果,与试验数据对比吻合较好,验证了模型的准确性.在此基础上,以VC及OpenCASCADE为工具,开发了通用性的飞机座椅弹射仿真平台,该平台具有一定的工程应用价值.
AbstractList V215.2; 通过某型飞机弹射座椅穿盖弹射火箭滑车试验,研究了舱盖在穿盖弹射中的破裂形式.在试验研究的基础上,进行了数值模拟,利用PCL语言对MSC.PATRAN进行二次开发,实现参数化建模.采用非线性有限元方法,通过瞬态动力学软件MSC.Dytran仿真得到了人椅系统在穿盖出舱过程中的过载及舱盖的破裂效果,与试验数据对比吻合较好,验证了模型的准确性.在此基础上,以VC及OpenCASCADE为工具,开发了通用性的飞机座椅弹射仿真平台,该平台具有一定的工程应用价值.
Author 闫家益
潘雄
童明波
王一丁
AuthorAffiliation 南京航空航天大学飞行器先进设计技术国防重点学科实验室,南京,210016
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Yan Jiayi
Pan Xiong
Tong Mingbo
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Keywords 参数化建模
二次开发
parametric modeling
动力学分析
through canopy ejection
dynamics analysis
穿盖弹射
secondary development
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Snippet V215.2; 通过某型飞机弹射座椅穿盖弹射火箭滑车试验,研究了舱盖在穿盖弹射中的破裂形式.在试验研究的基础上,进行了数值模拟,利用PCL语言对MSC.PATRAN进行二次开发,实现参...
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Title 某型飞机弹射座椅穿盖弹射试验与数值模拟
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