EXPERIMENT AND SIMULATION RESEARCH OF THE OPTIMUM INTERFERENCE OF HI-LOCK ASSEMBLY

At present, the high lock bolt assembly standard of our country are come from abroad, lack of relevant theoretical and experimental research. Fatigue gain mechanism of high lock bolt interference on the base of different layer thickness is researched,through the method of combining the fatigue test...

Full description

Saved in:
Bibliographic Details
Main Authors: XIE JieDong, CHEN Guo, ZENG XinLiang, SHU MaoSheng, LUO Yun, GAO Hong, ZHENG QiHui
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2018-01-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2018.06.009
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1841535668598079488
author XIE JieDong
CHEN Guo
ZENG XinLiang
SHU MaoSheng
LUO Yun
GAO Hong
ZHENG QiHui
author_facet XIE JieDong
CHEN Guo
ZENG XinLiang
SHU MaoSheng
LUO Yun
GAO Hong
ZHENG QiHui
author_sort XIE JieDong
collection DOAJ
description At present, the high lock bolt assembly standard of our country are come from abroad, lack of relevant theoretical and experimental research. Fatigue gain mechanism of high lock bolt interference on the base of different layer thickness is researched,through the method of combining the fatigue test and finite element simulation in a certain type of aircraft aluminum alloy structure. First, the fatigue test was designed and tested, and the results were analyzed by S-N curve, detail fatigue rating(DFR) and fracture location. Then, the finite element modeling and simulation are used to explain the experimental phenomena, and the mechanism of the interference fit to the fatigue gain is studied. Finally, the comprehensive detail fatigue rating results and the finite element simulation results are obtained, which are the standard recommended values of the high lock bolt assembly,and verified existing installation specifications, ensure the assembly quality of a certain type of aircraft.
format Article
id doaj-art-fe447266e75e4e36a384058a51a2935c
institution Kabale University
issn 1001-9669
language zho
publishDate 2018-01-01
publisher Editorial Office of Journal of Mechanical Strength
record_format Article
series Jixie qiangdu
spelling doaj-art-fe447266e75e4e36a384058a51a2935c2025-01-15T02:30:53ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692018-01-01401321132930603218EXPERIMENT AND SIMULATION RESEARCH OF THE OPTIMUM INTERFERENCE OF HI-LOCK ASSEMBLYXIE JieDongCHEN GuoZENG XinLiangSHU MaoShengLUO YunGAO HongZHENG QiHuiAt present, the high lock bolt assembly standard of our country are come from abroad, lack of relevant theoretical and experimental research. Fatigue gain mechanism of high lock bolt interference on the base of different layer thickness is researched,through the method of combining the fatigue test and finite element simulation in a certain type of aircraft aluminum alloy structure. First, the fatigue test was designed and tested, and the results were analyzed by S-N curve, detail fatigue rating(DFR) and fracture location. Then, the finite element modeling and simulation are used to explain the experimental phenomena, and the mechanism of the interference fit to the fatigue gain is studied. Finally, the comprehensive detail fatigue rating results and the finite element simulation results are obtained, which are the standard recommended values of the high lock bolt assembly,and verified existing installation specifications, ensure the assembly quality of a certain type of aircraft.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2018.06.009Interference fitHi-lock boltFatigue strengthFinite element methodDetail fatigue rating
spellingShingle XIE JieDong
CHEN Guo
ZENG XinLiang
SHU MaoSheng
LUO Yun
GAO Hong
ZHENG QiHui
EXPERIMENT AND SIMULATION RESEARCH OF THE OPTIMUM INTERFERENCE OF HI-LOCK ASSEMBLY
Jixie qiangdu
Interference fit
Hi-lock bolt
Fatigue strength
Finite element method
Detail fatigue rating
title EXPERIMENT AND SIMULATION RESEARCH OF THE OPTIMUM INTERFERENCE OF HI-LOCK ASSEMBLY
title_full EXPERIMENT AND SIMULATION RESEARCH OF THE OPTIMUM INTERFERENCE OF HI-LOCK ASSEMBLY
title_fullStr EXPERIMENT AND SIMULATION RESEARCH OF THE OPTIMUM INTERFERENCE OF HI-LOCK ASSEMBLY
title_full_unstemmed EXPERIMENT AND SIMULATION RESEARCH OF THE OPTIMUM INTERFERENCE OF HI-LOCK ASSEMBLY
title_short EXPERIMENT AND SIMULATION RESEARCH OF THE OPTIMUM INTERFERENCE OF HI-LOCK ASSEMBLY
title_sort experiment and simulation research of the optimum interference of hi lock assembly
topic Interference fit
Hi-lock bolt
Fatigue strength
Finite element method
Detail fatigue rating
url http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2018.06.009
work_keys_str_mv AT xiejiedong experimentandsimulationresearchoftheoptimuminterferenceofhilockassembly
AT chenguo experimentandsimulationresearchoftheoptimuminterferenceofhilockassembly
AT zengxinliang experimentandsimulationresearchoftheoptimuminterferenceofhilockassembly
AT shumaosheng experimentandsimulationresearchoftheoptimuminterferenceofhilockassembly
AT luoyun experimentandsimulationresearchoftheoptimuminterferenceofhilockassembly
AT gaohong experimentandsimulationresearchoftheoptimuminterferenceofhilockassembly
AT zhengqihui experimentandsimulationresearchoftheoptimuminterferenceofhilockassembly