本文選題：氣囊 + 緩沖　； 參考：《包裝工程》2017年11期

【摘要】：目的總結(jié)當(dāng)前著陸緩沖氣囊的國(guó)內(nèi)外研究現(xiàn)狀。方法介紹不同緩沖氣囊的工作原理與優(yōu)缺點(diǎn),總結(jié)解析與有限元2種氣囊性能的計(jì)算方法與性能參數(shù)優(yōu)化方法的研究現(xiàn)狀,以及氣囊技術(shù)研究的發(fā)展方向。結(jié)果分析了各類(lèi)緩沖氣囊與性能參數(shù)計(jì)算方法的優(yōu)缺點(diǎn),總結(jié)了氣囊技術(shù)待解決的問(wèn)題。結(jié)論提高緩沖氣囊的氣壓主動(dòng)控制技術(shù)與著陸姿態(tài)控制技術(shù)可進(jìn)一步提高氣囊性能。
[Abstract]:Objective to summarize the current research status of landing cushion airbag at home and abroad. Methods the working principle, advantages and disadvantages of different cushioning airbags were introduced, and the current research status of the analytical and finite element methods for calculating the performance of airbags and the optimization methods of performance parameters were summarized, as well as the development trend of airbag technology. Results the advantages and disadvantages of various cushioning airbags and performance parameters were analyzed, and the problems to be solved were summarized. Conclusion the air pressure active control technology and landing attitude control technology can further improve the performance of the airbag.
【作者單位】： 軍械工程學(xué)院;軍械技術(shù)研究所;
【分類(lèi)號(hào)】：TB485.1
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本文編號(hào)：1822718