solidworks机载弹舱结构设计+文献综述
由于现代战场的不同需求，以往的内埋式弹舱的结构已经不能完全满足。本文基于中型战略导弹在战场中的统治地位，对内埋式弹舱的结构进行了新的设计。新型内埋式弹舱将采取把导弹从飞行器尾部弹射而出的发射方式。解决了以往内埋式弹舱舱门设计难度太高的问题。
本文采用solidworks三文实体模型软件来对新型内埋式弹舱进行结构设计，并对发射筒的强度进行了校核。本文所做的研究将可以辅助未来内埋式弹舱的结构设计，为未来内埋式弹舱的结构提供了新的思路。
关键词 内埋式弹舱， 结构设计，压力传递
毕业论文设计说明书外文摘要
Title An airborne missile cabin structure design
Abstract
With the Modern Warfare Strategy, the air battlefield has played an important role in controlling the overall situation.. Due to the stealth capability and speed cruising capability of the modern fighter, the embedded missile weapon has become the mainstream.. The internal buried type missile chamber is the important structural basis of the embedded weapon, and the structural design of the missile cabin will have the important significance for the lifting of the embedded weapon..
Due to the different needs of the modern battlefield, the structure of the embedded missile cabin can not be fully satisfied in the past.. Based on the dominant position of mid sized strategic missile in the battlefield, the structure of the embedded missile cabin is designed.. The new type of embedded missile cabin will take the missile from the tail of the aircraft and out of the launch mode. To solve the buried bomb bay door design difficult problem.
In this paper, the SolidWorks 3D solid model is used to design the structure of the new type of embedded missile.And the intensity of the launching cylinder was checked. The research done in this paper will help the structure design of the embedded bomb cabin in the future, and provide a new way for the structure of the embedded missile in the future..
Keywords embedded missile weapon, structure design, pressure transfer
目 录
1 引言 1
1.1 概述 1
1.2 研究背景 2
1.3 内埋式弹舱的研究现状 3
1.4 本论文的主要工作 10
1.5 小结 10
2 内埋式弹舱设计结构的选择 11
2.1 当代内埋式弹舱结构及发射方式 11
2.2 新型内埋式弹舱结构及发射方式 12
2.3 两种结构的对比与选择 14
3 本课题新型内埋式弹舱的基本结构及强度校核 16
3.1 弹的基本模型 16
3.2 新型内埋式弹舱的设计理念 18
3.3 新型内埋式弹舱的设计思路 19
3.4 发射筒的强度校核 20
3.5 小结 25
4 新型内埋式弹舱几个重要结构 26
4.1 胶座 26
4.2 钢座 27
4.3 燃气发生器 28
4.4 小结 28
5 简述飞行器上的装配情况 29
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