Frame Structure Design of a Combined Helicopter-borne Missile Launcher

ZHANG Dazhi; XUE Hairui; QIN Gang; YU Jiangxia

doi:10.15892/j.cnki.djzdxb.2019.05.038

Journal of Projectiles, Rockets, Missiles and Guidance >

2019 , Vol. 39 >Issue 5: 163 - 165

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2019.05.038

Frame Structure Design of a Combined Helicopter-borne Missile Launcher

ZHANG Dazhi ,
XUE Hairui ,
QIN Gang ,
YU Jiangxia

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Xi’an Modern Control Technology Research Institute, Xi’an 710065, China

Received date: 2018-10-22

Online published: 2025-05-12

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Abstract

In order to solve the problems such as poor consistency of weight,low yield of cast products and limited quantity of foundry manufacturers who meet the requirements of the casting frame of the launcher,it is put forward that the frame of the launcher is designed into six parts,which are added and formed by machine.The modular and combinational design of the frame is realized.Through finite element analysis and test verification,it is shown that the combined design scheme of the frame of this type launcher is feasible and meets the requirements of structural performance.

Key words： helicopter load; missile launcher; launcher frame design

Cite this article

ZHANG Dazhi , XUE Hairui , QIN Gang , YU Jiangxia . Frame Structure Design of a Combined Helicopter-borne Missile Launcher[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(5) : 163 -165 . DOI: 10.15892/j.cnki.djzdxb.2019.05.038

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References

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